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| Document ID | 1313888 |
| Application ID | qSDcHpOrLko7i/mvw1kz+g== |
| Document Description | SD-720 Manual Part 3 |
| Short Term Confidential | No |
| Permanent Confidential | No |
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| Document Type | User Manual |
| Display Format | Adobe Acrobat PDF - pdf |
| Filesize | 130.25kB (1628135 bits) |
| Date Submitted | 2010-07-19 00:00:00 |
| Date Available | 2010-07-19 00:00:00 |
| Creation Date | 2017-11-08 17:48:52 |
| Producing Software | GPL Ghostscript 9.18 |
| Document Lastmod | 2017-11-08 17:48:52 |
| Document Title | SDIM:Multi-Channel SATCOM System:A15-5111-010 |
| Document Author: | ATR |
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
INSERT PAGE 44 OF 53 FACING PAGE 6-100.
Reason:
To add a new failure code, 0B, to Table 6-19 between failure codes 0A and 0D.
Failure code 0B is added as follows:
Table 6-19.
Failure
Code
0B
Airbus Level I (SDU No. 1) Failure Messages and ATA No.
SDU/SDU No. 1 – CFDS Normal and Interactive Modes
HDM
ATA Number
232832
23-20-35
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 44 of 53
28 Sep 2009
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
1A
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
[IGA]
232813
HI GAIN ANTENNA--TOP(16RV1)
[Top Mount]
232813
HI GAIN ANTENNA--L(17RV)
[Conformal]
232812
1C
HI GAIN ANTENNA--R(18RV)
[Conformal]
232812
1F
LO GAIN ANTENNA(13RV)
21
MCDU1(2CA1)
[A330/A340]
228212
MCDU1(3CA1)
[A320]
228212
MCDU2(2CA2)
[A330/A340]
228212
MCDU2(3CA2)
[A320]
228212
MCDU3(2CA3)
[A330/A340]
228212
MCDU3(3CA3)
[A320]
228212
ATSU1(1TX1)
[ATSU]
462134
[A320 ACARS]
232434
[A330/A340 ACARS]
232434
[ATSU]
462134
[A320 ACARS]
232434
[A330/A340 ACARS]
232434
22
23
33
ANTENNA1(116RV1)
ATA Number
ACARS MU(1RB)
ACARS MU1(1RB1)
34
232811
ATSU2 (1TX2)
ACARS MU2
ACARS MU2(1RB2)
35
ADIRU1(1FP1)
341234
36
ADIRU2(1FP2)
341234
37
RESERVED
N/A
38
RESERVED
N/A
39
RESERVED
N/A
3D
FMGC1(1CA1)
FMGEC1(1CA1)
3E
228334
[A330/A340]
228334
[A320]
228334
[A330/A340]
228334
FMGC2(1CA2)
FMGEC2(1CA2)
40
[A320]
ARINC 429 ICAO
N/A
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--101
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-19.
Failure
Code
42
43
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
ATA Number
CTU--CU CEPT--E1 BUS/SDU1 (105RV1)
[IGA A320]
233500
CTU--CU CEPT--E1 BUS/SDU1 (105RV1)
[IGA A330/A340]
239200
CTU--CU CEPT--E1 BUS/SDU1 (5RV1)
[HGA A320]
233500
CTU--CU CEPT--E1 BUS/SDU1 (5RV1)
[HGA A330/A340]
239200
IFE 429 BUS/SDU1 (5RV1)
[A330/A340 HGA]
233000
IFE 429 BUS/SDU1 (105RV1)
[A330/A340 HGA]
IFE 429 BUS/SDU1 (105RV1)
[A320 IGA]
IFE 429 BUS/SDU1 (5RV1)
[A320 HGA]
50
HSDU1 (63RV1)/SDU1 (5RV1)
52
IFE 429 BUS/SDU1 (5RV1)
[A330/A340 HGA]
IFE 429 BUS/SDU1 (105RV1)
[A330/A340 HGA]
IFE 429 BUS/SDU1 (105RV1)
[A320 IGA]
53
233000
ATSU1 (1TX1)/SDU1(105RV1)
[IGA ATSU]
462134
[HGA ATSU]
462134
[IGA A320 ACARS]
232434
[IGA A330/A340 ACARS]
232434
[HGA A320 ACARS]
232434
[HGA A330/A340 ACARS]
232434
CTU--CU CEPT--E1 BUS/SDU1(105RV1)
[IGA A320]
233500
CTU--CU CEPT--E1 BUS/SDU1(105RV1)
[IGA A330/A340]
239200
CTU--CU CEPT--E1 BUS/SDU1(5RV1)
[HGA A320]
233500
CTU--CU CEPT--E1 BUS/SDU1(5RV1)
[HGA A330/A340]
239200
[IGA A330/A340]
228212
[HGA A330/A340]
228212
[IGA A320]
228212
[HGA A320]
228212
[IGA A330/A340]
228212
[HGA A330/A340]
228212
IGA A320
228212
HGA A320
228212
ACARS MU1 (1RB1)/SDU1(105RV1)
ACARS MU (1RB)/SDU1(5RV1)
ACARS MU1 (1RB1)/SDU1(5RV1)
MCDU1(2CA1)/SDU1(105RV1)
MCDU1(2CA1)/SDU1(5RV1)
MCDU1(3CA1)/SDU1(105RV1)
MCDU(3CA1)/SDU1(5RV1)
56
233000
[A320 HGA]
ACARS MU (1RB)/SDU1(105RV1)
55
232839
IFE 429 BUS/SDU1 (5RV1)
ATSU1 (1TX1)/SDU1(5RV1)
54
233000
MCDU2(2CA2)/SDU1(105RV1)
MCDU2(2CA2)/SDU1(5RV1)
MCDU2(3CA2)/SDU1(105RV1)
MCDU2(3CA2)/SDU1(5RV1)
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--102
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
57
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
ATSU2 (1TX2)/SDU1(105RV1)
ATA Number
[IGA ATSU]
462134
[HGA ATSU]
462134
[IGA A320 ACARS]
232434
[IGA A330/A340 ACARS]
232434
[HGA A320 ACARS]
232434
[HGA A330/A340 ACARS]
232434
CFDIU(1TW)/SDU1(105RV1)
[IGA A320]
313234
CMC1(1TM1)/SDU1(105RV1)
[IGA A330/A340]
451334
CFDIU(1TW)/SDU1(5RV1)
[HGA A320]
313234
CMC1(1TM1)/SDU1(5RV1)
[HGA A330/A340]
451334
[IGA]
341234
[HGA]
341234
[IGA]
341234
[HGA]
341234
[IGA]
232831
HPA--HI GAIN(7RV1)/SDU1(5RV1)
[HGA]
232831
HPA--LO GAIN(9RV)/SDU1(5RV1)
[HGA + LGA]
232835
HPA--LO GAIN(9RV)/SDU1(105RV1)
[IGA + LGA]
232835
BSU(8RV1)/SDU1(5RV1)
[Top Mount]
232846
BSU--L(15RV1)/SDU1(5RV1)
[Conformal]
232844
64
BSU--R(15RV2)/SDU1(5RV1)
[Conformal]
232844
66
MCDU3(2CA3)/SDU1(105RV1)
[IGA A330/A340]
228212
[HGA A330/A340]
228212
[IGA A320]
228212
[HGA A320]
228212
ATSU2 (1TX2)/SDU1(5RV1)
ACARS MU2/SDU1(105RV1)
ACARS MU2 (1RB2)/SDU1(105RV1)
ACARS MU2/SDU1(5RV1)
ACARS MU2 (1RB2)/SDU1(5RV1)
59
5A
ADIRU1(1FP1)/SDU1(105RV1)
ADIRU1(1FP1)/SDU1(5RV1)
5B
ADIRU2(1FP2)/SDU1(105RV1)
ADIRU2(1FP2)/SDU1(5RV1)
5C
5F
62
HPA1 (110RV1)/SDU1(105RV1)
MCDU3(2CA3)/SDU1(5RV1)
MCDU3(3CA3)/SDU1(105RV1)
MCDU3(CA3)/SDU1(5RV1)
67
RESERVED
68
RESERVED
6A
RESERVED
6C
RESERVED
6D
RESERVED
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--103
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
6E
RESERVED
6F
RESERVED
71
SDU2(105RV2)CROSSTALK BUS/SDU1
(105RV1)
ATA Number
[IGA]
232834
[HGA]
232834
[IGA A320]
228334
[IGA A330/A340]
228334
[HGA A320]
228334
[HGA A330/A340]
228334
[IGA A320]
228334
[IGA A330/A340]
228334
[HGA A320]
228334
[HGA A330/A340]
228334
[IGA]
232834
[HGA]
232834
SDU1(5RV1) BUS M--CTRL/HPA--LO
GAIN(9RV)
[HGA+LGA]
232834
SDU1(105RV1) BUS M--CTRL/HPA--LO
GAIN(9RV)
[IGA+LGA]
232834
SDU1(5RV1) BUS M--CTRL/BSU(8RV1)
[Top Mount]
232834
SDU1(5RV1) BUS M--CTRL/BSU--L(15RV1)
[Conformal]
232834
9A
BSU--R (15RV2) XTALK BUS/BSU--L(15RV1)
[Conformal]
232844
9C
SDU1(5RV1) BUS M--CTRL/BSU--R(15RV2)
[Conformal]
232834
9D
BSU--L (15RV1) XTALK BUS/BSU--R(15RV2)
[Conformal]
232844
9E
SDU1 (5RV1) /HSDU1 (63RV1)
9F
Not applicable for package 6.0 and beyond
SDU2(5RV2)CROSSTALK BUS/SDU1
5RV1)
73
FMGC1(1CA1)/SDU1(105RV1)
FMGEC1(1CA1)/SDU1(105RV1)
FMGC1(1CA1)/SDU1(5RV1)
FMGEC1(1CA1)/SDU1(5RV1)
74
FMGC2(1CA2)/SDU1(105RV1)
FMGEC2(1CA2)/SDU1(105RV1)
FMGC2(1CA2)/SDU1(5RV1)
FMGEC2(1CA2)/SDU1(5RV1)
80
RESERVED
82
RESERVED
88
RESERVED
90
SDU1(105RV1) BUS M--CTRL/HPA1(110RV1)
SDU1(5RV1) BUS M--CTRL/HPA--HI
GAIN(7RV1)
96
98
232834
N/A
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--104
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-19.
Failure
Code
A1
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
SDU1(105RV1)/MCDU1(2CA1)
SDU1(5RV1)/MCDU1(2CA1)
A2
SDU1(105RV1).MCDU2(2CA2)
SDU1(5RV1)/MCDU2(2CA2)
A3
SDU1(105RV1)/MCDU3(2CA3)
SDU1(5RV1)/MCDU3(2CA3)
ATA Number
[IGA]
228212
[HGA]
228212
[IGA]
228212
[HGA]
228212
[IGA]
228212
[HGA]
228212
A6
ESU(101RF) ETHERNET 1/HSDU1(63RV1)
464131
A7
ESU(101RF) ETHERNET 2/HSDU1(63RV1)
464131
A8
ESU(101RF) ISDN 1/HSDU1(63RV1)
464131
A9
ESU(101RF) ISDN 2/HSDU1(63RV1)
464131
C0
WRG:CONFIG PIN PROG/SDU1(105RV1)
[IGA]
232800
[HGA]
232800
[IGA]
323171
[HGA]
323171
[IGA]
232834
SDU1(5RV1) SEL--DISABLE
DISCRETE/SDU2(5RV2)
[HGA]
232834
WRG:ICAO ADDRESS PIN
PROG/SDU1(105RV1)
[IGA]
232800
WRG:ICAO ADDRESS PIN
PROG/SDU1(5RV1)
[HGA]
232800
[IGA]
232831
[HGA]
232831
[IGA]
232800
[HGA]
232800
WRG:CONFIG PIN PROG/SDU1(5RV1)
C1
LGCIU1(5GA1)/LGCIU2(5GA2)/SDU1(105RV1)
LGCIU1(5GA1)/LGCIU2(5GA2)/SDU1(5RV1)
C2
C3
C4
SDU1(105RV1) SEL--DISABLE
DISCRETE/SDU2(105RV2)
HPA1 (110RV1)/VSWR
HPA--HI GAIN(7RV1)/VSWR
C5
WRG:CONFIG PIN PROG/SDU1(105RV1)
OWNER REQS DB
WRG:CONFIG PIN PROG/SDU1(5RV1)
OWNER REQS DB
C6
HPA--LO GAIN(9RV)/VSWR
C7
HPA(110RV1)/OVER TEMPERATURE
232835
HPA--HI GAIN(7RV1)/OVER TEMPERATURE
[IGA]
232831
[HGA]
232831
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--105
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
C8
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
ATA Number
SDU1(105RV1)/BAD DATA FROM GROUND
STATION
SDU1(5RV1)/BAD DATA FROM GROUND
EARTH STATION
C9
HPA--LO GAIN(9RV)/OVER TEMPERATURE
CA
SDU1(5RV1)CTRL DISCRETE/DLNA--LO
GAIN(14RV)
SDU1(105RV1)CTRL DISCRETE/DLNA--LO
GAIN(14RV)
CB
[IGA]
232834
[HGA]
232834
232835
[HGA+LGA]
232834
[IGA+LGA]
232834
[IGA]
232800
[HGA]
232800
WRG:SDI PIN PROG/HPA1(110RV1)
WRG:SDI PIN PROG/HPA--HI GAIN(7RV1)
CC
WRG:SDI PIN PROG/HPA--LO GAIN(9RV)
232800
CD
N/A
CE
RESERVED
CF
N/A
N/A
D0
N/A
N/A
D1
WRG:SDI PIN PROG/HPA1(110RV1)
232800
WRG:SDI PIN PROG/HPA--HI GAIN(7RV1)
232800
D2
WRG:SDI PIN PROG/HPA--LO GAIN(9RV)
232800
D3
WRG:SDI PIN PROG/BSU(8RV1)
[Top Mount]
232800
WRG:SDI PIN PROG/BSU--L(15RV1)
[Conformal]
232800
D4
WRG:SDI PIN PROG/BSU--R(15RV2)
[Conformal]
232800
D5
SDU1(105RV1)/TXCOAX
[IGA]
232834
[HGA]
232834
[IGA+LGA]
232834
[HGA+LGA]
232834
[IGA]
232834
[HGA]
232834
N/A
SDU1(5RV1)/TXCOAX
D6
SDU1 (105RV1)/TXCOAX
SDU1(5RV1)/TXCOAX
D7
RESERVED
D8
SDU1(105RV1)/RXCOAX
SDU1(5RV1)/RXCOAX
D9
SDU2(5RV1)/RXCOAX
DA
SDU1(105RV1)/RXCOAX
232834
[IGA+LGA]
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
232834
Page 6--106
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
SDU1(5RV1)/RXCOAX
DB
LO GAIN ANTENNA(13RV)
LOG ON FAILURE
DC
N/A
DD
SDU1(105RV1) OWNER REQS DB SECURED
PARTITION
ATA Number
[HGA+LGA]
232811
N/A to Airbus
[IGA]
232834
[HGA]
232834
[IGA]
232834
[HGA]
232834
SDU1(105RV1)
LOG ON FAILURE
[IGA]
232834
SDU1(5RV1)
LOG ON FAILURE
[HGA]
232834
SDU1(5RV1) OWNER REQS DB SECURED
PARTITION
DE
SDU1(105RV1) OWNER REQS DB USER
PARTITION
SDU1(5RV1) OWNER REQS DB USER
PARTITION
DF
232834
E0
RESERVED
E1
SDU1(5RV1) DISCRETE/HSDU1(63RV1)
E2
N/A
N/A
E3
N/A
N/A to Airbus
E4
SDU1(5RV1)/HSDU1(63RV1)
E5
N/A
E6
HSDU1(63RV1)/TXCOAX
E7
N/A
E8
HSDU1(63RV1)/RXCOAX
E9
N/A
N/A
EA
N/A
N/A to Airbus
EB
MCDU1(2CA1)+MCDU2(2CA2)+MCDU3(2CA3)
INACTIVE
EC
WRG:CONFIG PIN PROG/HSDU1(63RV1)
232800
ED
WRG:CONFIG PIN PROG/HSDU1(63RV1)
SDU ORT
232800
232834
232834
N/A to Airbus
232839
N/A
232839
[RMP only]
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
228212
Page 6--107
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 1) Failure Messages and ATA No. (cont)
Table 6-19.
Failure
Code
SDU/SDU No. 1 -- CFDS Normal and Interactive Modes
ATA Number
EE
WRG:FWD ID1 ADDRESS PIN
PROG/HSDU1(63RV1)
232800
FE
POWER SUPPLY INTERRUPT
240000
Table 6-20.
Failure
Code
01
Airbus Level I (SDU No. 2) Failure Messages and ATA No.
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
SDU2(105RV2)
SDU2(5RV2)
02
SDU1(105RV1) INCOMPATIBILITY
SDU1(5RV1) INCOMPATIBILITY
03
HSDU2(63RV2)
04
HPA2(110RV2)
ATA Number
[IGA]
232834
[HGA]
232834
[IGA]
232834
[HGA]
232834
232839
HPA--HI GAIN(7RV2)
[IGA]
232831
[HGA]
232831
07
HPA--LO GAIN(9RV)
232835
0A
HI POWER RELAY(21RV)
232842
0D
DLNA2 (119RV2)
[IGA]
232838
DLNA--TOP(19RV2)
[Top Mount]
232838
DLNA--L(20RV3)
[Conformal]
232837
0F
DLNA--R(20RV4)
[Conformal]
232837
10
DLNA--LO GAIN(14RV)
13
BSU(8RV2)
[Top Mount]
232846
BSU--L(15RV3)
[Conformal]
232844
15
BSU--R(15RV4)
[Conformal]
232844
1A
ANTENNA2(116RV2)
[IGA]
232813
HI GAIN ANTENNA--TOP(16RV1)
[Top Mount]
232813
HI GAIN ANTENNA--L(17RV)
[Conformal]
232812
1C
HI GAIN ANTENNA--R(18RV)
[Conformal]
232812
1F
LO GAIN ANTENNA(13RV)
21
MCDU1(2CA1)
[A330/A340]
228212
MCDU1(3CA1)
[A320]
228212
232836
232811
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 6--108
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
INSERT PAGE 45 OF 53 FACING PAGE 6-108.
Reason:
To add a new failure code, 0B, to Table 6-20 between failure codes 0A and 0D.
Failure code 0B is added as follows:
Table 6-20.
Failure
Code
0B
Airbus Level I (SDU No. 2) Failure Messages and ATA No.
SDU/SDU No. 2 – CFDS Normal and Interactive Modes
HDM
ATA Number
232832
23-20-35
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 45 of 53
28 Sep 2009
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
Table 6-20.
Failure
Code
22
23
33
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
MCDU2(2CA2)
[A330/A340]
228212
MCDU2(3CA2)
[A320]
228212
MCDU3(2CA3)
[A330/A340]
228212
MCDU3(3CA3)
[A320]
228212
ATSU1(1TX1)
[ATSU]
462134
[A320 ACARS]
232434
[A330/A340 ACARS]
232434
[ATSU]
462134
[A320 ACARS]
232434
[A320/A340 ACARS]
232434
ACARS MU(1RB)
ACARS MU1(1RB1)
34
ATA Number
ATSU2 (1TX2)
ACARS MU(1RB)
ACARS MU2(1RB2)
35
ADIRU1(1FP1)
341234
36
ADIRU2(1FP2)
341234
37
RESERVED
N/A
38
RESERVED
N/A
39
RESERVED
N/A
3D
FMGC1(1CA1)
FMGEC1(1CA1)
3E
[A320]
228334
[A330/A340]
228334
[A320]
228334
[A330/A340]
228334
FMGC2(1CA2)
FMGEC2(1CA2)
40
ARINC 429 ICAO
42
CTU -- CU CEPT--E1 BUS/SDU2(105RV2)
[IGA A320]
233500
CTU -- CU CEPT--E1 BUS/SDU2(105RV2)
[IGA A330/A340]
239200
CTU -- CU CEPT--E1 BUS/SDU2(5RV2)
[HGA A320]
233500
CTU -- CU CEPT--E1 BUS/SDU2(5RV2)
[HGA A330/A340]
239200
IFE 429 BUS/SDU2(5RV2)
[A330/A340 HGA]
233000
43
232800
IFE 429 BUS/SDU2(105RV2)
[A330/A340 IGA]
IFE 429 BUS/SDU2(105RV2)
[A320 IGA]
IFE 429 BUS/SDU2(5RV2)
50
HSDU2(63RV2)/SDU2(5RV2)
51
RESERVED
233000
[A320 HGA]
232839
23--20--35
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Page 6--109
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-20.
Failure
Code
52
53
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
IFE 429 BUS/SDU2(5RV2)
55
[A330/A340 IGA]
IFE 429 BUS/SDU2(105RV2)
[A320 IGA]
233000
[A320 HGA]
ATSU1 (1TX1)/SDU2(105RV2)
[IGA ATSU]
462134
[HGA ATSU]
462134
ACARS MU(1RB1)/SDU2(105RV2)
[IGA ACARS A330/A340]
232434
ACARS MU1(1RB1)/SDU2(5RV2)
[HGA ACARS A330/A340]
232434
ACARS MU(1RB)/SDU2(105RV2)
[IGA ACARS A320]
232434
ACARS MU1(1RB)/SDU2(5RV2)
[HGA ACARS A320]
232434
CTU -- CU CEPT--E1 BUS/SDU2(105RV2)
[IGA A320]
233500
CTU -- CU CEPT--E1 BUS/SDU2(105RV2)
[IGA A330/A340]
239200
CTU -- CU CEPT--E1 BUS/SDU2(5RV2)
[HGA A320]
233500
CTU -- CU CEPT--E1 BUS/SDU2(5RV2)
[HGA A330/A340]
239200
[IGA A330/A340]
228212
[HGA A330/A340]
228212
[IGA A320]
228212
[HGA A320]
228212
[IGA]
228212
[HGA]
228212
[IGA A320]
228212
MCDU2(3CA2)/SDU2(5RV2)
[HGA A320]
228212
ATSU2 (1TX2)/SDU2(105RV2)
[IGA ATSU]
462134
[HGA ATSU]
462134
[IGA A320 ACARS]
232434
[IGA A330/A340 ACARS]
232434
[HGA A320 ACARS]
232434
[HGA A330/A340 ACARS]
232434
MCDU1(2CA1)/SDU2(105RV2)
MCDU1(3CA1)/SDU2(105RV2)
MCDU1(3CA1)/SDU2(5RV2)
MCDU2(2CA2)/SDU2(105RV2)
MCDU2(2CA2)/SDU2(5RV2)
MCDU2(3CA2)/SDU2(105RV2)
57
233000
IFE 429 BUS/SDU2(5RV2)
MCDU1(2CA1)/SDU2(5RV2)
56
[A330/A340 HGA]
IFE 429 BUS/SDU2(105RV2)
ATSU1 (1TX1)/SDU2(5RV2)
54
ATA Number
ATSU2 (1TX2)/SDU2(5RV2)
ACARS MU2/SDU2(105RV2)
ACARS MU2 (1RB2)/SDU2(105RV2)
ACARS MU2/SDU2(5RV2)
ACARS MU2(1RB2)/SDU2(5RV2)
23--20--35
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Page 6--110
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
Table 6-20.
Failure
Code
59
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
ATA Number
CFDIU(1TW)/SDU2(105RV2)
[IGA A320]
313234
CMC1(1TM1)/SDU2(105RV2)
[IGA A330/A340]
451334
CFDIU(1TW)/SDU2(5RV2)
[HGA A320]
313234
CMC1(1TM1)/SDU2(5RV2)
[HGA A330/A340]
451334
[IGA]
341234
[HGA]
341234
[IGA]
341234
[HGA]
341234
[IGA]
232831
HPA--HI GAIN(7RV2)/SDU2(5RV2)
[HGA]
232831
HPA--LO GAIN(9RV)/SDU2(5RV2)
HGA+LGA
232835
IGA+LGA
232835
BSU(8RV2)/SDU2(5RV2)
[Top Mount]
232846
BSU--L(15RV3)/SDU2(5RV2)
[Conformal]
232844
64
BSU--R(15RV4)/SDU2(5RV2)
[Conformal]
232844
66
MCDU3(2CA3)/SDU2(105RV2)
[IGA A330/A340]
228212
[HGA A330/A340]
228212
[IGA A320]
228212
[HGA A320]
228212
[IGA]
232834
[HGA]
232834
5A
ADIRU1(1FP1)/SDU2(105RV2)
ADIRU1(1FP1)/SDU2(5RV2)
5B
ADIRU2(1FP2)/SDU2(105RV2)
ADIRU2(1FP2)/SDU2(5RV2)
5C
5F
HPA2(110RV2)/SDU2(105RV2)
HPA--LO GAIN(9RV)/SDU2(105RV2)
62
MCDU3(2CA3)/SDU2(5RV2)
MCDU3(3CA3)/SDU2(105RV2)
MCDU3(3CA3)/SDU2(5RV2)
67
RESERVED
68
RESERVED
6A
RESERVED
6C
RESERVED
6D
RESERVED
6E
RESERVED
6F
RESERVED
71
SDU1(105RV1)CROSSTALK
BUS/SDU2(105RV2)
SDU1(5RV1)CROSSTALK BUS/SDU2(5RV2)
23--20--35
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Page 6--111
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
Table 6-20.
Failure
Code
73
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
FMGC1(1CA1)/SDU2(105RV2)
ATA Number
[IGA A320]
228334
[IGA A330/A340]
228334
[HGA A320]
228334
[HGA A330/A340]
228334
[IGA A320]
228334
[IGA A330/A340]
228334
[HGA A320]
228334
[HGA A330/A340]
228334
[IGA]
232834
[HGA]
232834
HGA+LGA
232834
SDU2(105RV2) BUS M--CTRL/HPA--LO
GAIN(9RV)
IGA+LGA
232834
SDU2(5RV2) BUS M--CTRL/BSU(8RV2)
[Top Mount]
232834
SDU2(5RV2) BUS M--CTRL/BSU--L(15RV3)
[Conformal]
232834
9A
BSU--R(15RV4) XTALK/BSU--L(15RV3)
[Conformal]
232844
9C
SDU2(5RV2) BUS M--CTRL/BSU--R(15RV4)
[Conformal]
232834
9D
BSU--L(15RV3) XTALK BUS/BSU--R(15RV4)
[Conformal]
232844
9E
SDU2(5RV2)/HSDU2(63RV2)
9F
Not applicable for package 6.0 and beyond
A1
SDU2(105RV2)/MCDU1(2CA1)
FMGEC1(1CA1)/SDU2(105RV2)
FMGC1(1CA1)/SDU2(5RV2)
FMGEC1(1CA1)/SDU2(5RV2)
74
FMGC2(1CA2)/SDU2(105RV2)
FMGEC2(1CA2)/SDU2(105RV2)
FMGC2(1CA2)/SDU2(5RV2)
FMGEC2(1CA2)/SDU2(5RV2)
80
RESERVED
82
RESERVED
88
RESERVED
90
SDU2(105RV2) BUS M--CTRL/HPA2(110RV2)
SDU2(5RV2) BUS M--CTRL/HPA--HI
GAIN(7RV2)
96
98
SDU2(5RV2) BUS M--CTRL/HPA--LO
GAIN(9RV)
232834
N/A
SDU2(5RV2)/MCDU1(2CA1)
A2
SDU2(105RV2)/MCDU2(2CA2)
SDU2(RV2)/MCDU2(2CA2)
[IGA]
228212
[HGA]
228212
[IGA]
228212
[HGA]
228212
23--20--35
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Page 6--112
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-20.
Failure
Code
A3
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
SDU2(105RV2)/MCDU3(2CA3)
SDU2(5RV2)/MCDU3(2CA3)
ATA Number
[IGA]
228212
[HGA]
228212
A6
ESU(101RF) ETHERNET 1/HSDU2(63RV2)
464131
A7
ESU(101RF) ETHERNET 2/HSDU2(63RV2)
464131
A8
ESU(101RF) ISDN 1/HSDU2(63RV2)
464131
A9
ESU(101RF) ISDN 2/HSDU2(63RV2)
464131
C0
WRG:CONFIG PIN PROG/SDU2(105RV2)
[IGA]
232800
[HGA]
232800
[IGA]
323171
[HGA]
323171
[IGA]
232834
[HGA]
232834
WRG:ICAO ADDRESS PIN PROG/
SDU2(105RV2)
[IGA]
232800
WRG:ICAO ADDRESS PIN PROG/
SDU2(5RV2)
[HGA]
232800
[IGA]
232831
[HGA]
232831
[IGA]
232800
[HGA]
232800
WRG:CONFIG PIN PROG/SDU2(5RV2)
C1
LGCIU1(5GA1)/LGCIU2(5GA2)/SDU2(105RV2)
LGCIU1(5GA1)/LGCIU2(5GA2)/SDU2(5RV2)
C2
SDU2(105RV2) SEL--DISABLE
DISCRETE/SDU1(105RV1)
SDU2(5RV2) SELECT--DISABLE
DISCRETE/SDU1(5RV1)
C3
C4
HPA2(110RV2)/COAX
HPA--HI GAIN(7RV1)/COAX
C5
WRG:CONFIG PIN PROG/SDU2(105RV2)
OWNER REQS DB
WRG:CONFIG PIN PROG/SDU2(5RV2)
OWNER REQS DB
C6
LPA--LO GAIN(9RV)/COAX
C7
HPA2(110RV2)/OVER TEMPERATURE
C8
232835
[IGA]
232831
HPA--HI GAIN(7RV2)/OVER TEMPERATURE
[HGA]
232831
SDU2(105RV2)/BAD DATA FROM GROUND
STATION
[IGA]
232834
[HGA]
232834
SDU2(5RV2)/BAD DATA FROM GROUND
EARTH STATION
C9
HPA--LO GAIN(9RV)/OVER TEMPERATURE
232835
23--20--35
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Page 6--113
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
Table 6-20.
Failure
Code
CA
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
SDU2(5RV2)CTRL DISCRETE/DLNA--LO
GAIN(14RV)
SDU2(105RV2)CTRL DISCRETE/DLNA--LO
GAIN(14RV)
CB
ATA Number
[HGA+LGA]
232834
[IGA+LGA]
232834
[IGA]
232800
[HGA]
232800
WRG:SDI PIN PROG/HPA2(110RV1)
WRG:SDI PIN PROG/HPA--HI GAIN(7RV2)
CC
WRG:SDI PIN PROG/HPA--LO GAIN(9RV)
232800
CD
N/A
CE
RESERVED
CF
N/A
N/A
D0
N/A
N/A
D1
WRG:SDI PIN PROG/HPA2(110RV1)
N/A
WRG:SDI PIN PROG/HPA--HI GAIN(7RV2)
[IGA]
232800
[HGA]
232800
D2
WRG:SDI PIN PROG/HPA--LO GAIN(9RV)
D3
WRG:SDI PIN PROG/BSU(8RV2)
[Top Mount]
232800
WRG:SDI PIN PROG/BSU--L(15RV3)
[Conformal]
232800
D4
WRG:SDI PIN PROG/BSU--R(15RV4)
[Conformal]
232800
D5
SDU2(105RV2)/TXCOAX
[IGA]
232834
SDU2(5RV2)/TXCOAX
[HGA]
232834
SDU2(105RV2)/TXCOAX
[LGA]
232834
[HGA or IGA]
232834
[IGA]
232834
SDU2(5RV2)/RXCOAX
[HGA]
232834
D9
SDU2(5RV2)/RXCOAX
[HGA]
232834
DA
SDU2(105RV2)/RXCOAX
LGA+(HGA or IGA)
232834
SDU2(5RV2)/RXCOAX
LGA+(HGA or IGA)
232834
D6
SDU2(5RV2)/TXCOAX
D7
RESERVED
D8
SDU2(105RV2)/RXCOAX
DB
LO GAIN ANTENNA(13RV) LOG ON FAILURE
DC
N/A
232800
232811
N/A
23--20--35
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Page 6--114
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Airbus Level I (SDU No. 2) Failure Messages and ATA No. (cont)
Table 6-20.
Failure
Code
DD
SDU/SDU No. 2 -- CFDS Normal and Interactive Modes
ATA Number
SDU2 (105RV2) OWNER REQS DB SECURED
PARTITION
SDU2 (5RV2) OWNER REQS DB SECURED
PARTITION
DE
SDU2 (105RV2) OWNER REQS DB USER
PARTITION
SDU2 (5RV2) OWNER REQS DB USER
PARTITION
DF
SDU2 (105RV2) LOG ON FAILURE
SDU2 (5RV2) LOG ON FAILURE
[IGA]
232834
[HGA]
232834
[IGA]
232834
[HGA]
232834
[IGA]
232834
[HGA]
232834
E0
RESERVED
E1
SDU2(5RV2) DISCRETE/HSDU2(63RV2)
E2
N/A
N/A
E3
N/A
N/A
E4
SDU2(5RV2)/HSDU2(63RV2)
E5
N/A
E6
HSDU2(63RV2)/TXCOAX
E7
N/A
E8
HSDU2(63RV2)/RXCOAX
E9
N/A
N/A
EA
N/A
N/A
EB
MCDU1(2CA1)+MCDU2(2CA2)+MCDU3(2CA3)
INACTIVE
EC
WRG:CONFIG PIN PROG/HSDU2(63RV2)
232800
ED
WRG:CONFIG PIN PROG/HSDU2(63RV2)
SDU ORT
232800
EE
WRG:FWD ID1 ADDRESS PIN
PROG/HSDU2(63RV2)
232800
FE
POWER SUPPLY INTERRUPT
240000
232834
232834
N/A
232839
N/A
232839
[RMP only]
23--20--35
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228212
Page 6--115
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-21.
Failure
Code
McDonnell Douglas Level I Failures Messages and
ATA Reference Numbers
CFDS Normal and Interactive Modes
ATA Number
01
SDU
232610
02
OTHER SDU INCOMPATIBILITY
232611
03
HSU
232664
04
HPA--IN GAIN
[IGA]
232600
HPA--HI GAIN
[HGA]
232613
07
HPA--LO GAIN
232614
0A
HI POWER RELAY
232615
0D
DLNA--(TOP/L)
232616
0F
DLNA--R
232618
10
DLNA--LO GAIN
232619
13
BSU--(TOP/L)
23261B
15
BSU--R
23261C
1A
IN GAIN ANTENNA--TOP
[IGA]
232600
HI GAIN ANTENNA--(TOP/L)
[HGA]
23261D
1C
HI GAIN ANTENNA--R
23261F
1F
LO GAIN ANTENNA
232620
21
MCDU1
232635
22
MCDU2
232636
23
MCDU3
232637
33
(ACARS MU/CMU)
23243C
34
(ACARS MU/CMU)2
N/A
35
(IRS/ADIRU)--PRI
23263E
36
(IRS/ADIRU)--SEC
23263F
37
RESERVED
38
RESERVED
39
RESERVED
3D
(FMC/VIA)1
232642
3E
(FMC/VIA)2
232643
23--20--35
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Page 6--116
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
INSERT PAGE 46 OF 53 FACING PAGE 6-116.
Reason:
To add a new failure code, 0B, to Table 6-21 between failure codes 0A and 0D.
Failure code 0B is added as follows:
Table 6-21.
Failure
Code
0B
McDonnell Douglas Level I Failure Messages and
ATA Reference Numbers
CFDS Normal and Interactive Modes
HDM
ATA Number
232664
23-20-35
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 46 of 53
28 Sep 2009
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-21.
Failure
Code
McDonnell Douglas Level I Failures Messages and
ATA Reference Numbers (cont)
CFDS Normal and Interactive Modes
ATA Number
40
ARINC 429 ICAO ADDRESS
N/A
42
CTU
43
(CFS/CPDF)
50
HSU/SDU
52
(CFS/CPDF)/SDU
53
(ACARS MU/CMU)/SDU
23263C
54
CTU/SDU
232644
55
MCDU1/SDU
232635
56
MCDU2/SDU
232636
57
(ACARS MU/CMU)2/SDU
59
CFDIU/SDU
232641
5A
(IRS/ADIRU)--PRI/SDU
23263E
5B
(IRS/ADIRU)--SEC/SDU
23263F
5C
HPA--IN GAIN/SDU
[IGA]
232600
HPA--HI GAIN/SDU
[HGA]
232600
232644
TBD
232664
TBD
N/A
5F
HPA--LO GAIN/SDU
232623
62
BSU--(TOP/L)/SDU
232626
64
BSU--R/SDU
232627
66
MCDU3/SDU
232637
67
RESERVED
68
RESERVED
6A
RESERVED
6C
RESERVED
6D
RESERVED
6E
RESERVED
6F
RESERVED
71
OTHER SDU/THIS SDU
232600
73
(FMC/VIA)1/SDU
232642
23--20--35
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Page 6--117
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-21.
Failure
Code
McDonnell Douglas Level I Failures Messages and
ATA Reference Numbers (cont)
CFDS Normal and Interactive Modes
ATA Number
74
(FMC/VIA)2/SDU
232643
80
RESERVED
82
RESERVED
88
RESERVED
90
SDU M--CTRL/HPA--IN GAIN
[IGA]
232600
SDU M--CTRL/HPA--HI GAIN
[HGA]
232600
96
SDU M--CTRL/HPA--LO GAIN
23262D
98
SDU M--CTRL/BSU--(TOP/L)
232600
9A
BSU--R XTALK/BSU--L
232600
9C
SDU M--CTRL/BSU--R
232630
9D
BSU--L XTALK/BSU--R
232600
9E
SDU/HSU
232664
9F
RESERVED
232664
A6
HSU ETHERNET PORT 1
232664
A7
HSU ETHERNET PORT 2
232664
A8
HSU ISDN PORT 1
232664
A9
HSU ISDN PORT 2
232664
C0
WRG:CONFIG PIN PROG/SDU
232600
C1
SDU WOW MISCOMPARE
C2
SDU/OTHER SDU SELECT--DISABLE DISCRETE
232600
C3
WRG:ICAO ADDRESS PIN PROG/SDU
232631
C4
TX PATH VSWR--IN GAIN
[IGA]
232600
TX PATH VSWR--HI GAIN
[HGA]
232600
N/A
C5
WRG:CONFIG PIN PROG/SDU OWNER REQS
232600
C6
TX PATH VSWR--LO GAIN
232600
C7
HPA--IN GAIN/OVER TEMPERATURE
[IGA]
232600
HPA--HI GAIN/OVER TEMPERATURE
[HGA]
23262C
C8
BAD DATA FROM GROUND EARTH STATION
C9
HPA--LO GAIN/OVER TEMPERATURE
None
232634
23--20--35
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Page 6--118
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-21.
Failure
Code
McDonnell Douglas Level I Failures Messages and
ATA Reference Numbers (cont)
CFDS Normal and Interactive Modes
ATA Number
CA
SDU/DLNA--LO GAIN
232619
CB
WRG:SDI PIN PROG/HPA--IN GAIN
[IGA]
232600
WRG:SDI PIN PROG/HPA--HI GAIN
[HGA]
232600
CC
WRG:SDI PIN PROG/HPA--LO GAIN
232600
CD
SDU (POC/TOTC) DATA RESET
CE
RESERVED
CF
HPA--IN GAIN (POC/TOTC) DATA RESET
[IGA]
None
HPA--HI GAIN (POC/TOTC) DATA RESET
[HGA]
None
None
D0
HPA--LO GAIN (POC/TOTC)
None
D1
WRG:SDI PIN PROG/HPA--IN GAIN
[IGA]
232600
WRG:SDI PIN PROG/HPA--HI GAIN
[HGA]
232600
D2
WRG:SDI PIN PROG/HPA--LO GAIN
232600
D3
WRG:SDI PIN PROG/BSU--(TOP/L)
232600
D4
WRG:SDI PIN PROG/BSU--R
232600
D5
SDU COAX/HPA--IN GAIN
[IGA]
232600
SDU COAX/HPA--HI GAIN
[HGA]
232600
D6
SDU COAX/HPA--LO GAIN
D7
RESERVED
D8
DLNA/(SDU)--(TOP/L)
232600
D9
DLNA/(SDU)--R
232600
DA
DLNA/(SDU)--LO GAIN
232600
DB
LO GAIN SUBSYSTEM
232600
DC
NO ACTIVE ACARS MU/CMU
232400
DD
SDU OWNER REQS -- SECURED
None
DE
SDU OWNER REQS -- USER
None
DF
IN GAIN SUBSYSTEM
[IGA]
232600
HI GAIN SUBSYSTEM
[HGA]
232600
E0
RESERVED
E1
BAD HSU DISABLE DISCRETE
232600
232664
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-21.
Failure
Code
McDonnell Douglas Level I Failures Messages and
ATA Reference Numbers (cont)
CFDS Normal and Interactive Modes
ATA Number
E2
RESERVED
E3
RESERVED
E4
HSU/SDU INTERFACE VER INCOMPATIBILITY
E5
RESERVED
E6
HSU/HPA TX RF PATH
E7
RESERVED
E8
DLNA/HSU RX RF PATH
E9
RESERVED
EA
RESERVED
EC
WRG:CONFIG PIN PROG/HSU
232664
ED
WRG:CONFIG PIN PROG/HSU SDU OWNER REQS
232664
EE
WRG:FWD ID PIN PROG/HSU
232664
FE
POWER SUPPLY INTERRUPT
None
232664
232664
232664
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
4. SCDU for Dual SATCOM
A. General
(1) The SDU supports SCDU page displays for dual systems. All pages are as specified
in paragraph 2.D. (SCDU pages) with the following exceptions.
B. SATCOM Logical Channels
(1) The SATCOM channels for HEADSET calls in a dual system can be supplied by
several combinations of physical channels within both SDUs. These combinations are
determined by the configuration strap settings for cockpit wiring and ORT items
regarding the use of SDU channel resources (items vi, vii, and xlviii). The display of
channel status and selections as reported on menus MAIN, DIRECTORY, and
CATEGORY-n reflect the logical channel status.
C. SATCOM (Cross-Talk Bus Failed)
(1) The SDU designated as the slave unit in a dual system must receive most of the
system status information from the master over the SDU cross-talk bus. If full
communication is not established, the slave unit cannot receive the necessary data
for the display pages. The default SATCOM MAIN MENU display page THIS UNIT
UNAVAILABLE is displayed in this case.
D. SATCOM
(1) The channel status page reflects the physical channels within the SDU that is
providing the display page.
E.
SATCOM Menus
(1) The maintenance menus reflect the maintenance data for the SATCOM system that
is providing the display page.
5. Maintenance Panel Assembly
A. General
(1) The maintenance panel assembly interface diagram (Figure 5-17) supplies remote
monitoring of MCS system operation. The maintenance panel assembly is made up
of two parts: the cabin telecommunications (CTM) panel and the Commissioning and
Maintenance Terminal (CMT) panel. The CTM panel is used for monitoring the cabin
telecommunications equipment. The panel contains six lamps to indicate the
availability of the telephone handsets. A keyed on/off switch arms the system when
the key is turned to the ON position.
(2) The CMT panel is used primarily to debug, detect, isolate software and/or hardware
integration, LRU and system integration, formal testing, and system access approval,
as well as general performance analysis. The CMT data connector supplies an
access port for a commissioning and maintenance terminal that can be a personal
computer, a dumb terminal, or a modem. The SDU interface connector on the panel
supplies a remote access port for testing the SDU. The panel also contains lamps to
indicate the status of the MCS system. These lamps are defined in Table 6-22.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table 6-22.
Commissioning and Maintenance Terminal Panel Lamps
Definition
Lamp
IN USE CH--1
(SDU pin TPH1) This lamp lights to show channel 1 is in use.
IN USE CH--2
(SDU pin TPK1) This lamp lights to show channel 2 is in use.
PILOT VCE NOT AVAIL
(SDU pin TP3A) This lamp lights to show no additional voice channels can be
established. This can be because no resources are available, or all available
resources being allocated to existing calls.
LOG OFF
(SDU pin TPC3) This lamp lights to show no packet mode data service
capability exists at any data rate; system not logged on.
CABIN VCE NOT AVAIL
(SDU pin TPB3) This lamp lights to show no additional channels can be
established for analog or digital cabin voice, or circuit--mode data. This can be
because no resources are available, or all available resources being allocated
to existing calls.
MCS FAIL
(SDU pin TPG1) This lamp lights to show a total loss of all SATCOM voice and
data services, and at least one cause can be attributable to the MCS system
LRUs themselves. Replacement of the appropriate LRU (SDU, HPA) is
necessary to restore partial or complete service. It is possible for this indicator
and the MCS inoperable indicator (NON-MCS FAIL) to be active
simultaneously, indicating failure in both the MCS system LRUs and nonsystem
LRUs.
NON-MCS FAIL
(SDU pin TPE3) This lamp lights to show total loss of all SATCOM voice and
data services, and at least one cause is attributable to the non-MCS system
LRUs, or interfaces to those LRUs. Replacement of the appropriate non MCS
LRU(s), or correction of the interface failure is necessary to restore partial or
complete service. It is possible for this indicator and the SATCOM fail indicator
(MCS FAIL) to be active simultaneously, indicating failure in both the MCS
system LRUs and the nonsystem LRUs or interfaces.
NO SAT LINK
(SDU pin TPJ1) This lamp lights to show no SATCOM voice or data services
are available because of the AES not being successfully logged-on, and the
cause is definitely not due to reported failures (MCS or non-MCS). If there is a
MCS or non-MCS failure, the NO SAT LINK lamp will not light.
HGA FAIL
(SDU pin TPD3) This lamp lights to show packet-mode data service capability
exists, but only at the lowest channel rates (600 and 1200 bps). This indicator
is assumed to only be present in high gain antennas installations that have a
low gain antenna backup system. The lamp indicates an HGA failure due to the
reduction from normal high speed capability.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
SECTION 7
MAINTENANCE PRACTICES
1. Overview
A. General
(1) This section supplies instructions for removing, reinstalling, and adjusting each LRU
of the MCS that has been installed by the aircraft manufacturer or completion center.
Where applicable, instructions for replacing lamps, knobs, and set screws are
included. Adjustment information is called out as required.
CAUTION: SHOULD ANY INSTALLATION CRITICAL CASES ARISE WITH THE
REINSTALLATION OF ANY UNIT, YOU MUST COMPLY 100 PERCENT
WITH THE INSTRUCTION.
CAUTION: TO PREVENT DAMAGE TO EQUIPMENT, TURN AIRCRAFT POWER OFF
WHEN REMOVING OR INSTALLING LRUS.
2. Equipment and Materials
A. General
CAUTION: DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO
MATERIALS SPECIFIED BY HONEYWELL. MATERIALS NOT
EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN
MAKE THE WARRANTY NOT APPLICABLE.
(1) Maintenance materials identified with a Honeywell Material Number (HMN) are given
in Table 7-1.
(2) No additional special equipment or materials other than those commonly used in the
shop are required to install the units in existing trays and clamps, and to adjust the
system. Do not over tighten mounting screws. Where torque values are not given, it
is acceptable to finger tighten the mounting screws.
Table 7-1.
Item
Materials
Description
Source
HMN 97P5778
RTV silicone, No. 3145,
translucent, per MIL--A--46146,
Group II, Type I military
designation M4614621XTN.
Dow Corning Corp, Midland, MI
(05AJ8)
HMN 98C0978
Sealant, corrosion inhibitive
(MIL--S--81733, Type II--1/2 -- for
extrusion application in the time of
1/2 hour) — Pro--Seal 870B--1/2
Courtaulds Aerospace, Glendale,
CA (83574)
NOTES: NOTES:
1.
Equivalent alternatives are permitted for materials in this list.
2.
The HMN codes in the list of materials identify the Honeywell Material Number (HMN) given to each material.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
3. Procedure for Antennas
A. General
(1) The following paragraphs describe general information when removing or installing
antennas.
NOTE: For all antennas not supplied by Honeywell, removal and installation should
be done according to installation instructions from the manufacturer.
B. Antenna Weather Protection
(1) Some antennas require gaskets and others have O--rings. When reinstalling
antennas, new gaskets or O--rings should be used.
(2) A weather sealant should be applied around the periphery of the antenna base to
prevent seepage of water and condensation and preclude corrosion. If a sealant or
aerodynamic smoother is used around the periphery of the antenna base, it should
be applied after the antenna has been bolted down. The sealant used should be
nonadhering so the antenna can be removed at a later time, if necessary. Chromatic
tape is recommended.
NOTE: When mounting antennas on a pressurized fuselage, a leveling and sealing
compound like Pro-Seal 870B--1/2 should be used between the entire
mounting surface of the antenna and the fuselage. Use of this compound, in
addition to the installation gasket, compensates for surface irregularities and
voids between the antenna and the fuselage. A mold releasing agent can be
used on the fuselage prior to installation to prevent the leveling compound
from adhering to the fuselage.
(3) To prevent water seepage on top mounted antennas, it can be necessary to apply
Silastic sealant (RTV--3145 or equivalent) to the mounting screw heads.
C. Antenna Hardware
(1) Clean the airframe at the antenna mounting area to remove any foreign material.
(2) Because of the insulation qualities of gaskets and leveling compounds, the mounting
screws are required to supply the electrical bonding between the antennas and the
aircraft (typically 15 milliohms or less is required). The technician doing the
reinstallation must be sure any hardware being reused is clean and free of corrosion.
If in doubt, use new hardware.
(3) Gaskets and O--rings deform during initial installation. While it is possible to reuse
gaskets and O--rings, it is highly recommended new gaskets or O--rings be used.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
D. General Antenna Removal Instructions
NOTE: These procedures apply to all antennas. To prevent damage to the
antennas, do not apply pressure to the plastic housings or pry on plastic
housings.
(1) Pull the appropriate circuit breakers.
(2) After removing and saving the hardware, cut the bond line of any installer--applied
sealant between the antenna and the aircraft skin.
(3) Pull the antenna away from the aircraft skin far enough to disconnect the cable
connector(s).
4. Procedure for the LRUs
CAUTION: BEFORE AN LRU IS INSTALLED OR REMOVED, PULL THE CIRCUIT
BREAKERS THAT SUPPLY POWER TO THE LRU TO REMOVE POWER.
CAUTION: MOISTURE AND DIRT CAUSE DAMAGE TO LRUs.
CAUTION: LRU FAILURE RATES INCREASE WITH A RISE IN TEMPERATURE. INSTALL
THE LRUs WITH CLEARANCE; LET THE AIR FLOW ON TOP AND BOTTOM
OF LRUS TO PREVENT OVERHEATING.
A. LRU Removal
(1) Remove an LRU as follows:
(a) Disconnect the circuit breakers that supply power to the LRU.
(b) Tag the circuit breakers with DO-NOT-OPERATE identifiers.
(c) Loosen the clamp knobs and let them drop out of the way.
(d) Pull the LRU forward a minimum of 1/2 inch to clear the rear connector pins.
(e) Lift the LRU free of the cooling air-duct gasket on the mounting rack.
B. LRU Installation
(1) Install an LRU as follows:
(a) Determine the location of each LRU in the aircraft.
(b) Check the LRU to be installed and make sure all connector pins are straight and
ready for connection.
(c) Make sure the index pin coding on the rear connector is correct for the mating
connector.
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MCS--4200/7200 Multi--Channel SATCOM System
(d) Place the LRU in the appropriate mounting rack and align the connectors. Push
the LRU back to make contact with the connector pins. Push the LRU into place
and rock the LRU sideways slightly.
CAUTION: DO NOT OVER TIGHTEN THE CLAMP. EXCESSIVE TORQUE CAN
CAUSE BRACKETS AND CONNECTORS TO WARP AND BEND.
(e) Put the hold-down clamps in place and tighten the knobs finger-tight.
5. Owner Requirements Table Uploading
A. General
(1) When the SDU is replaced, the ORT needs to be uploaded before normal operation
can begin. Refer to SYSTEM OPERATION, for the ORT uploading procedure.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
6. Instructions for Continued Airworthiness, FAR 25.1529
A. General
(1) Maintenance requirements and instructions for continued airworthiness of the MCS
components are contained in the paragraphs that follow.
(2) Installation of the MCS on an aircraft by supplemental type certificate or Form 337
obligates the aircraft operator to include the maintenance information supplied by this
manual in the operator’s Aircraft Maintenance Manual and the operator’s Aircraft
Scheduled Maintenance Program.
(a) Maintenance information for the MCS (system description, removal, installation,
testing, etc.) is contained in this manual.
(b) LRU part numbers and other necessary part numbers contained in this manual
should be placed into the aircraft operator’s appropriate aircraft illustrated parts
catalog (IPC).
(c) Wiring diagram information contained in this manual should be placed into the
aircraft operator’s appropriate aircraft Wiring Diagram Manuals.
(d) The MCS system components are considered on--condition units and no
additional maintenance is required other than a check for security and operation
at normal inspection intervals.
(e) If a system component is inoperative, remove unit, secure cables and wiring,
collar applicable switches and circuit breakers, and placard them inoperative.
Revise equipment list and weight and balance as applicable prior to flight and
make a log book entry that unit was removed (refer to section 91.213 of the FAR
or the aircraft’s minimum equipment list (MEL).
(f)
The MCS components can be repaired at a factory authorized repair center or an
appropriately rated FAA Part 145 repair station.
(g) Once repaired, reinstall the LRU in the aircraft in accordance with the original
Form 337 approved data or instructions in this manual. Do a Return to Service
test of the system and approve it for return to service with a log book entry
required by section 43.9.
(h) Scheduled maintenance program tasks to be added to the aircraft operator’s
appropriate aircraft maintenance program are as follows:
Recommended periodic scheduled servicing tasks: None required.
Recommended periodic inspections: None required.
NOTE: The (applicable LRUs) used with this system have test and
inspections that are required by FAR 91.413 to be completed every
24 calender months.
Recommended periodic scheduled preventative maintenance tests (Tests to
determine system condition and/or latent failures): None required.
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MCS--4200/7200 Multi--Channel SATCOM System
Blank Page
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX A
VENDOR EQUIPMENT
1. Overview
A. General
(1) Appendix A contains information on vendor-manufactured equipment that can be
installed on an aircraft configured for MCS system. Installation of this equipment
depends on the specific requirements of the operator. Therefore, information in this
section is supplied as a courtesy to the MCS equipment operators.
2. Electronic Cable Specialists
A. General
(1) This paragraph contains information on how to select installation provisions offered
by ECS for the Honeywell MCS--4200/7200 system. ECS designs and manufactures
the installation provisions described here and can supply either individual
components or complete installation kits. The address for Electronic Cable
Specialists is as follows:
Electronic Cable Specialists
5300 W. Franklin Drive
Franklin, WI 53132
U.S.A.
Telephone: (414) 421--5300
FAX: (414) 421--5301
B. Radio Frequency Components
(1) All RF components (cable, connectors, and attenuators) supplied to interface the
SATCOM Avionics and Antenna Subsystems have been designed to meet the strict
usage and attenuation requirements of the Honeywell MCS--4200/7200 system and
ARINC 741/761. A selected list of RF components offered by ECS for SATCOM
installations is shown in Table A--1 and Table A--2.
C. Cable Assembly Fabrication
(1) ECS fabricates cable assemblies guaranteed to meet SATCOM system requirements
and ARINC 741 specifications.
• Each cable assembly is fabricated with an individual part number, which is
permanently affixed to each end of the assembly.
• Each set of cable assemblies is assigned a serial number, which is printed on the
part number label. Serialization makes sure each cable assembly is traceable and
repeatable.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--1.
ECS Cables and Connectors
310801
310201
311501
311601
311901
3C142B*
4.7
6.9
8.7
10.7
15.5
18.4
0.45 in.
0.32 in.
0.245 in.
0.23 in.
0.195 in.
0.195 in.
15.0
8.6
5.2
5.0
4.3
5.0
Male TNC 180°
CTS022
CTS122
CTS922
CTS922
CTS722
CTS722
Male TNC 90°
CTR022
CTR122
CTR922
CTR922
CTR722
CTR722
Male N 180°
CNS022
CNS122
CNS922
CNS922
CNS722
CNS722
Male N 90°
CNR022
CNR122
CNR922
CNR922
CNR722
CNR722
Female N 180°
FNS022
FNS122
FNS922
FNS922
FNS722
FNS722
ARINC 600 Size 1
L0122
L1122
L9122
L9122
L7122
L7122
ARINC 600 Size 5
N/A
N/A
A650922
A650922
ECS Cable Part No.
Nominal Attenuation
@ 1.6 GHz (dB/100 ft)
Overall Diameter
Pounds/100 ft
Table A--2.
225791--2 225791--2
ECS Attenuators
Attenuator (Transmit Path)
Attenuator (Receive Path)
Fixed or Variable
Fixed or Variable
D. Cable Assembly Testing
(1) Testing is done on Hewlett-Packard 8753 network analyzers to verify insertion loss
and VSWR. The results become part of a test database and are shipped with each
cable assembly. Each cable assembly is tested across the SATCOM system
frequency bandwidth (1530 MHz to 1660.5 MHz). Received path cable assemblies
are test swept from 1530 MHz to 1559 MHz. Customers have the option of having
cable assemblies tested with or without attenuators.
E.
ARINC 600 Connectors
(1) ECS supplies ARINC 600 connectors for ARINC 741 style avionic electrical
interfaces. The SATCOM rack-side connectors (Figure A--1) are described in this
paragraph. Connector part numbers are:
(2) ECS supplies ARINC 600 Size 1 coaxial connectors with the requisite termination kit
and assembly instructions (Figure A--2).
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Figure A--1.
Figure A--2.
ARINC Connectors
ARINC Assembly
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
F.
SATCOM Avionics Unit Mounting Hardware
(1) SATCOM avionics mounting hardware is made up of the HPA, SDU, and SCU and
will be mounted in ARINC 600 style tray assemblies. The HPA and SDU each require
forced air cooling during normal operation, whereas the SCU can function properly
with convection cooling alone. Refer to MECHANICAL INSTALLATION, for LRU
cooling requirements.
G. SATCOM Hardware Component Kits
(1) This paragraph contains information on how to select SATCOM hardware component
kits offered by ECS for the Honeywell MCS--4200/7200 avionic units in Table A--3
thru Table A--8. ECS supplies several options for each kit to accommodate the variety
of mounting requirements specific to each aircraft installation. ECS tray assemblies
come with and without independent cooling systems to ensure installation flexibility.
(2) The tray assemblies have been specially designed to meet Honeywell and ARINC
600 LRU cooling requirements. Tray assemblies are supplied with insertion/extraction
front hold-downs as standard, but are available with other front hold-down options.
For tray assembly dimensions refer to Figure A--3.
(3) The hardware component kits for the HPA, HSU, and SDU are listed in Table A--3
thru Table A--8, respectively.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Figure A--3.
Dimensions for ECS Tray Assemblies
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--3.
SD--720 (120--10141--1XX) Pressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER, FLAT
NSXN2P201S01
SD--720 ARINC CONNECTOR W/PINS AND
SOCKETS (NOTE 1 AND 2)
--
--
--
--
--
--
--
--
--
--
6028--101
6 MCU TRAY SHORT, RIGHT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
6068--101
6 MCU TRAY, SHORT, LEFT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
6413--101
6 MCU TRAY, LONG, REAR DC FAN
--
--
--
--
--
--
--
--
--
--
6013--102
6 MCU TRAY, SHORT, BOTTOM DC FAN
--
--
--
--
--
--
--
--
--
--
6218--101
6 MCU TRAY, LONG, RIGHT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6217--101
6 MCU TRAY, LONG, LEFT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6080--101
6 MCU TRAY, LONG, NO FAN
--
--
--
--
--
--
--
--
--
--
6110--101
6 MCU TRAY, SHORT, RIGHT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6216--101
6 MCU TRAY, SHORT, LEFT SIDE AC FAN
--
--
--
--
--
--
--
--
--
6013--106
6 MCU TRAY, SHORT, BOTTOM AC FAN
--
--
--
--
--
--
--
--
--
--
6035--101
6 MCU TRAY, SHORT, NO FAN
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: AD2--313--3AA00, NIC66H21A00AA0.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 300; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS. QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
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COMPONENTS
PART NO.
NO
OR
IDENTIFYING NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--4.
SD--720 (120--10142--1XX) Unpressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER, FLAT
NSXN2P201S01
SD--720 ARINC CONNECTOR W/PINS
AND SOCKETS (NOTE 1 AND 2)
--
--
--
--
--
--
--
--
--
--
200--10276--101
6 MCU TRAY SHORT, RIGHT SIDE DC FAN
(NOTE 3)
--
--
--
--
--
--
--
--
--
--
200--85743--101
6 MCU TRAY, SHORT, LEFT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
200--93955--101
6 MCU TRAY, LONG, REAR DC FAN
--
--
--
--
--
--
--
--
--
--
200--93112--101
6 MCU TRAY, SHORT, BOTTOM DC FAN
--
--
--
--
--
--
--
--
--
--
6281--101
6 MCU TRAY, LONG, RIGHT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6045--109
6 MCU TRAY, LONG, LEFT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6080--101
6 MCU TRAY, LONG, NO FAN
--
--
--
--
--
--
--
--
--
--
6282--101
6 MCU TRAY, SHORT, RIGHT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6232--101
6 MCU TRAY, SHORT, LEFT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6283--101
6 MCU TRAY, SHORT, BOTTOM AC FAN
--
--
--
--
--
--
--
--
--
--
6035--101
6 MCU TRAY, SHORT, NO FAN
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: AD2--313--3AA00, NIC66H21A00AA0.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 300; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
3.
200--10276--101 TRAY NOT CURRENTLY DESIGNED. APPROVED FAN ASSEMBLIES ARE: S0085--125, --134, --135, --138, AND --142.
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15 Jul 2006
COMPONENTS
PART NO.
OR
IDENTIFYING
NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--5.
HS--720 (120--10267--1XX) Pressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER, FLAT
NSXN2P221S01
HS--720 ARINC CONNECTOR W/PINS AND
SOCKETS (NOTE 1 AND 2)
--
--
--
--
--
--
--
--
--
--
200--10510--101
4 MCU TRAY SHORT, RIGHT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
200--92609--101
4 MCU TRAY, SHORT, LEFT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
200--92893--101
4 MCU TRAY, LONG, REAR DC FAN
--
--
--
--
--
--
--
--
--
--
200--84977--101
4 MCU TRAY, SHORT, BOTTOM DC FAN
--
--
--
--
--
--
--
--
--
6083--102
4 MCU TRAY, LONG, REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6026--101
4 MCU TRAY, LONG, NO FAN
--
--
--
--
--
--
--
--
--
--
6049--102
4 MCU TRAY, SHORT, RIGHT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6049--101
4 MCU TRAY, SHORT, LEFT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6050--101
4 MCU TRAY, SHORT, BOTTOM AC FAN
--
--
--
--
--
--
--
--
--
--
6034--101
4 MCU TRAY, SHORT, NO FAN
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: AD2--155C--3AA00, AD2--155C--30000, NIC66H20A00A00.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 140; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
23--20--35
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15 Jul 2006
COMPONENTS
PART NO.
OR
IDENTIFYING
NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--6.
HS--720 (120--10268--1XX) Unpressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER, FLAT
NSXN2P221S01
HS--720 ARINC CONNECTOR W/PINS AND
SOCKETS (NOTE 1 AND 2)
--
--
--
--
--
--
--
--
--
--
200--10684--101
4 MCU TRAY SHORT, RIGHT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
200--10683--101
4 MCU TRAY, SHORT, LEFT SIDE DC FAN
--
--
--
--
--
--
--
--
--
--
200--85588--101
4 MCU TRAY, LONG, REAR DC FAN
--
--
--
--
--
--
--
--
--
--
200--10682--101
4 MCU TRAY, SHORT, BOTTOM DC FAN
--
--
--
--
--
--
--
--
--
6137--101
4 MCU TRAY, LONG, REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6026--101
4 MCU TRAY, LONG, NO FAN
--
--
--
--
--
--
--
--
--
--
200--87190--101
4 MCU TRAY, SHORT, RIGHT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
200--84496--101
4 MCU TRAY, SHORT, LEFT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6376--101
4 MCU TRAY, SHORT, BOTTOM AC FAN
--
--
--
--
--
--
--
--
--
--
6034--101
4 MCU TRAY, SHORT, NO FAN
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: AD2--155C--3AA00, AD2--155C--30000, NIC66H20A00A00.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 140; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
23--20--35
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Page A--13/A--14
15 Jul 2006
COMPONENTS
PART NO.
OR
IDENTIFYING
NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--7.
HP--720 (120--99510--1XX) Pressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER, FLAT
NSXN2P221S01
HSD--128 ARINC CONNECTOR W/CONTACTS
(NOTE 1 AND 2)
MS25083--2BB8
6 INCH GROUNDING STRAP
--
--
--
--
--
--
--
--
--
--
200--96981--101
8 MCU S/S W/RIGHT MOUNTED DC FAN
--
--
--
--
--
--
--
--
--
--
200--91171--101
8 MCU S/S TRAY W/LEFT MOUNTED DC FAN
--
--
--
--
--
--
--
--
--
--
200--90568--101
8 MCU S/L W/REAR MOUNTED DC FAN
--
--
--
--
--
--
--
--
--
--
200--88654--101
8 MCU S/S TRAY W/BOTTOM MOUNTED DC
FAN
--
--
--
--
--
--
--
--
--
--
6117--103
8 MCU S/L TRAY W/RIGHT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6117--101
8 MCU S/L TRAY W/LEFT REAR AC FAN
--
--
--
--
--
--
--
--
--
--
6096--101
8 MCU S/L STANDARD TRAY
--
--
--
--
--
--
--
--
--
--
6101--101
8 MCU S/S TRAY W/RIGHT SIDE AC FAN
--
--
--
--
--
--
--
--
--
--
6100--101
8 MCU S/S TRAY W/LEFT SIDE AC FAN
--
--
--
--
--
--
--
--
--
6093--103
8 MCU S/S TRAY W/BOTTOM AC FAN
--
--
--
--
--
--
--
--
--
--
6072--102
8 MCU S/S STANDARD TRAY
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: 4D2--155C--3AA00, AD2--155C--30000, 4D2--155C--38900, BKAD2--V155M--301, NIC66H20A00AA0.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 140; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
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Page A--15/A--16
15 Jul 2006
COMPONENTS
PART NO.
NO
OR
IDENTIFYING NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--8.
HP--720 (120--99509--1XX) Unpressurized Hardware Kit
MS51957--29
6--32 X 7/16 IN. PAN HEAD
NAS1149DN616J
WASHER
NSXN2P221S01
HSD--128 ARINC CONNECTOR
W/CONTACTS (NOTE 1 AND 2)
MS25083--2BB8
6 INCH GROUNDING STRAP
--
--
--
--
--
--
--
--
--
--
--
200--90568--101
8 MCU S/L W REAR DC FAN
--
--
--
--
--
--
--
--
--
--
--
200--91171--102
8 MCU S/S W LEFT DC FAN &
FINGER GUARD
--
--
--
--
--
--
--
--
--
--
--
200--91171--101
8 MCU S/S TRAY W/LEFT SIDE DC
FAN
--
--
--
--
--
--
--
--
--
--
--
6--08S1C1C0
8 MCU S/S TRAY W/O COOLING AND
#10 MOUNTING HOLES
--
--
--
--
--
--
--
--
--
--
--
200--91165--101
8 MCU S/S TRAY W/BOTTOM DC FAN
--
--
--
--
--
--
--
--
--
--
--
6288--101
8 MCU S/S TRAY W/LEFT SIDE AC
FAN
--
--
--
--
--
--
--
--
--
--
--
6269--101
8 MCU S/S TRAY W/BOTTOM AC
MOUNTED
--
--
--
--
--
--
--
--
--
--
--
6286--101
8 MCU S/L TRAY W/RIGHT AC REAR
FAN
--
--
--
--
--
--
--
--
--
--
--
6284--101
8 MCU S/L TRAY W/LEFT AC REAR
FAN
--
--
--
--
--
--
--
--
--
--
--
6290--101
8 MCU S/S TRAY W/RIGHT AC SIDE
FAN
--
--
--
--
--
--
--
--
--
--
200--90202--101
8 MCU S/S TRAY W/LEFT SIDE AC
FAN/FILTER
--
--
--
--
--
--
--
--
--
--
--
6292--101
8 MCU S/S TRAY W/BOTTOM FAN
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
QTY
REQ’D
--112
--111
--110
--109
--108
--107
--106
--105
--104
--103
--102
--101
ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY ASSEMBLY
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
P/N
NOTES:
1.
ALTERNATE P/N: 4D2--155C--3AA00, AD2--155C--30000, 4D2--155C--38900, BKAD2--V155M--301, NIC66H20A00AA0.
2.
CONTACTS ARE: 22 AWG PINS, QTY OF 140; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.
23--20--35
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Page A--17/A--18
15 Jul 2006
COMPONENTS
PART NO.
OR
IDENTIFYING
NO.
NOMENCLATURE
OR
DESCRIPTION
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
H. Air Filtration Assemblies
(1) ECS can supply air filtration assemblies for the HPA, SDU, and BSU tray assemblies
described in Table A--9. These filter assemblies offer protection against airborne
contaminants, such as dust and cigarette smoke. System
mean--time--between--failures (MTBF) can be significantly increased. Appendix B
supplies installation procedures for air filtration hardware.
I.
SATCOM Shelf Assemblies
(1) ECS supplies customized and standard turnkey plenum shelf assemblies to
accommodate either single or dual SATCOM installations. A shelf assembly can
incorporate equipment trays, racking, and additional support structures, such as
disconnect panels, cover plates, and mounting brackets. ECS can supply
components that are compatible with all types of air transport aircraft.
NOTE: Some SATCOM system installation locations render the aircraft cooling
system inadequate. ECS has designed a self-contained cooling system for
the SATCOM shelf assembly that can be used in this type of installation.
J.
Additional Avionics Installation Components
(1) ECS supplies a variety of additional components to support a SATCOM installation.
These include RF splitters, combiners, high power relays, maintenance panels,
placards, circuit breakers, and control annunciator panels.
K. Antenna System Provisions
(1) SATCOM antenna systems are available in numerous configurations. ECS supplies
installation provisions for each of these configurations.
• Some high-gain top-mounted antenna systems require a 2-MCU tray assembly
and an ARINC 600 connector for the BSU. Others require mounting bracketry for
the BSU. ECS supplies both BSU 2-MCU tray assembly, and connector and
mounting bracketry as required.
• ECS supplies trays and ARINC connectors for various SCUs in the market place.
• ECS supplies other antenna mounting hardware, such as mounting brackets for
the diplexer/low noise amplifier (D/LNA) and high- and low-gain antenna doublers.
L.
Cabin Communications System Provisions
(1) ECS supplies ARINC 746 compliant air-to-ground communication systems installation
provisions. These provisions include mounting hardware and connectors, shelves,
racks, brackets, placards, cover plates, RF cable, connectors, cable assemblies, and
wire harness assemblies.
M. Wire Harnesses
(1) ECS can supply wire harness provisions that interface the SATCOM avionics with the
cabin communication units, the cabin communications units with the cabin phones,
and both the SATCOM avionics and cabin communication units with other aircraft
systems.
23--20--35
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Page A--19
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
(2) ECS wire harness assemblies can be custom designed and fabricated to meet
system installation requirements.
N. Complete Integrated SATCOM Installation Kits
(1) Complete system integration packages are available for ECS for virtually any given
installation requirements. These integration packages can include any of the
installation provisions discussed in this section, along with other customer-specified
components. ECS can also support Honeywell’s customers with systems installation
design engineering and certification design data packaging.
3. Hollingsead International
A. General
(1) This information aids you in selecting the engineering services and installation
provisions offered by Hollingsead International for the various MCS systems.
Hollingsead International is rapidly transforming into a world-class avionics and
aircraft systems integration leader, providing the capability to perform any or all of the
following:
• Design and manufacturing of the structural mounting for the MCS and all
associated avionics.
• Design and manufacturing of all wire and cable harness assembly interface
connections between the MCS and all associated avionics.
• Development of all engineering design substantiation, documentation, and testing
in support of FAA approval.
• Complete on-site support of a full installation team for the entire MCS installation
kit.
(2) You can contact them at the following address regarding your specific MCS program
requirements:
Hollingsead International
13701 Excelsior Drive
Santa Fe Springs, CA 90670
U.S.A.
Telephone: (310) 921-3438
FAX: (310) 921-6313
Telex: 691-462
B. Engineering Services
(1) As addressed in the previous paragraph, Hollingsead International supplies any level
of engineering support from minimal consultation to full turn-key. Full turn-key support
is defined as Hollingsead International undertaking the entire systems integration
from initial design through procurement and manufacture of parts to final installation
and certification on behalf on the customer.
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Page A--20
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
C. LRU Mounting Requirements
(1) MCS avionics are made up of the HPA, SDU, and BSU, which are mounted in ARINC
600 style tray assemblies. The HPA and SDU each require forced air cooling during
normal operation. The BSU and CMU, which are mounted in an ARINC 404 tray,
function properly with convection cooling alone.
D. Installation Kit Components
(1) General
(a) Complete system installation kits are available from Hollingsead International for
virtually any given installation requirement. These installation kits can include any
of the installation provisions discussed herein along with other
customer-specified components.
(2) Coaxial Cables
(a) All coaxial cables, connectors, and attenuators have been designed to fulfill the
MCS system and the ARINC 741 usage and attenuation requirements.
Hollingsead International supplies immediate access to several types and
manufacturers of coaxial cable, appropriate N or TNC connectors, and
attenuators to make sure the specific attenuation profiles for each aircraft
installation is achieved. These cables range in nominal attenuation from 1.27 to
16.3 dB per 100 feet at 1.6 GHz. The cable outer diameter range is from 0.206
inch to 1.55 inches. Each cable assembly is fabricated with an individual part
number and, where necessary, is assigned a serial number, which is
permanently affixed to each end. Serialization insures traceability and
reproducibility.
(b) Testing of each cable assembly is performed to verify insertion loss and VSWR.
The results become part of a test database and are shipped with each cable
assembly. Each cable assembly is tested across the MCS system frequency
bandwidth. Transmit path cable assemblies are test swept from 1626.5 MHz to
1660.5 MHz and receive path cable assemblies are test swept from 1530 MHz to
1559 MHz. Customers have the option of having cable assemblies tested with or
without attenuators.
(3) Connectors
(a) Hollingsead International supplies the appropriate ARINC connectors for ARINC
Characteristic 741 style avionics electrical interfaces. The SATCOM rack-side
connector blocks are appropriately mounted on each tray assembly. Hollingsead
International supplies ARINC 600 Size 1 coaxial connectors with the necessary
termination kit assembly instructions.
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Page A--21
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
(b) The connector part numbers are as follows:
• SDU -- C--06B3--0204--0100
• HPA -- C--06B3--0708--0100
• HSU -- C--06B3--0708--0100
• BSU -- C--06B1--0101--0100
• CMU -- DPX2MA--A106PA106P--33B--0001.
(4) Tray Assemblies
(a) Hollingsead International manufactures several tray assemblies for the MCS
avionics. These tray assemblies come with or without independent cooling
systems to ensure installation flexibility. Where forced air cooling is required,
these tray assemblies have been specially designed to meet the cooling
requirements of each LRU using a single fan. Tray assemblies are supplied with
insertion/extraction front hold-downs as standard, but are available with other
front hold-down options. Table A--9 identifies the various tray options and
Figure A--3 identifies the dimensions for each tray assembly.
Table A--9.
Type
Standard
Ta
Tray
Assembly
Tray Assembly Part Numbers
Assembly Fan Location
Bottom
Left Side
Right Side
Left Rear
Right Rear
N/A
N/A
8 MCU S/S
1708006--101 1708007--101 1708008--101 1708008--102
8 MCU S/L
1708006--201 1708007--201 1708008--201 1708008--202 1708009--101 1708009--102
6 MCU S/S
1706007--101 1706008--101 1706009--101 1706009--102
6 MCU S/L
1706007--201 1706008--201 1706009--201 1706009--202 1706010--101 1706010--102
4 MCU S/S
1704008--101 1704009--101 1704010--101 1704010--102
4 MCU S/L
1704008--201 1704009--201 1704010--201 1704010--202 1704011--101 1704011--102
2 MCU S/S
1702002--101 1702003--101
2 MCU S/L
1702002--201 1702003--201
N/A
N/A
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Honeywell International Inc. Do not copy without express permission of Honeywell.
N/A
N/A
Page A--22
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Figure A--4.
Dimensions for Hollingsead Tray Assemblies
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15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
(5) Plenum Shelf Assemblies
(a) Hollingsead International supplies customized and standard turnkey plenum
shelf assemblies to accommodate either single or dual MCS system installations.
A shelf assembly can incorporate equipment trays, racking, and additional
support structures such as disconnect panels, cover plates, and mounting
brackets. Hollingsead International can supply components that are compatible
with all types of air transport aircraft.
(6) Additional Components
(a) Hollingsead International supplies a variety of additional components to support
an MCS installation, including RF splitters, combiners, high power relays,
maintenance panels, placards, circuit breakers, and control enunciator panels.
(7) Antenna System Provisions
(a) The antenna subsystems for the MCS system are available in numerous
configurations. Hollingsead International supplies installation provisions for each
of these configurations. Some high-gain, top-mounted antenna systems use a
2-MCU tray assembly and ARINC 600 connector for the BSU. Others use
mounting bracket hardware for the BSU. Hollingsead International supplies both
BSU 2-MCU tray assemblies and mounting bracket hardware as necessary.
Hollingsead International supplies other antenna mounting hardware such as
mounting brackets for the diplexer/LNA and high-gain and low-gain antenna
doublers.
(8) Cabin Communications System Provisions
(a) Hollingsead International supplies ARINC 746 compliant air-to-ground
communications system installation provisions. These provisions include
mounting hardware and connectors, shelves, racks, brackets, placards, cover
plates, RF cable, connectors, cable assemblies, and wire harness assemblies.
(9) Wire Harness Assemblies
(a) Hollingsead International wire harness assemblies are custom designed and
fabricated to meet each customer’s specific system installation requirements.
Hollingsead International supplies wire harness assemblies for the following
interfaces:
• MCS avionics and cabin communication units
• MCS avionics and flight deck data and voice communication sources
• Cabin communications units and cabin telephones
• Both the SATCOM avionics and cabin communication units with other aircraft
systems.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
4. Signal Conditioning Unit
A. General
(1) The SCU (Part No. 56047--010XX) is manufactured by ATS USA Inc. in the U.S.A.
Contact the project manager at the following address for additional information not
supplied in this section:
ATS USA Inc.
11410 Isaac Newton Square
Suite 210
Reston, VA 20190
U.S.A.
Telephone: (800) 709--0172
FAX: (888) 325--5808
(2) The MCS system requires ARINC 429 data for antenna pointing, antenna
stabilization, and Doppler frequency correction. These requirements are defined in
Table A--10. If the aircraft does not have an IRS that supplies this ARINC data, the
SCU can be used to supply the data.
(3) The SCU is packaged as an ARINC 600 2 MCU and weighs a maximum of 5.95
pounds (2.70 kilograms). The outer case of the SCU is constructed from two
half-shells identical in dimensions, which are made of an aluminum alloy 1.6
millimeters thick. The front and rear panels are made of the same alloy 3.3
millimeters thick. Both panels attach to the outer half-shells with corner brackets. Two
divider plates mount between the half-shells of the outer case to supply additional
rigidity and electrical shielding.
(4) The SCU translates and consolidates various input data formats into a two-wire
differential ARINC 429 high speed output for latitude and longitude position, true
heading, track angle, ground speed, and pitch and roll attitude. Program pins define
the particular type of data being received. These pins are interrogated at power on by
the software to determine the required configuration.
(5) The SCU operates from a nominal 115 V ac, 400 Hz single phase supply and/or from
28 V dc primary power. Input pins are supplied for both power sources in the ARINC
600 connector, and both power inputs can be connected to the aircraft power.
Current consumption depends on the input voltage and temperature, but is typically
0.25 amperes at 115 V ac or 0.40 amperes at 28 V dc.
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--10.
Label
ARINC 429 Data Requirements
Definition
Minimum
Rate (MS)
Maximum
Rate (ms)
310
Latitude of present position
334
67
311
Longitude of present position
334
67
312
Ground speed
125
22
313
Track angle
55
22
314
True heading
55
22
324
Pitch
40
325
Roll
40
B. Operator Functions
(1) The front panel contains six LED indicators to allow monitoring of the SCU status.
However, these indicators are intended for use during repair by maintenance
personnel rather than by the operator during normal flight operation. Discrete outputs
representing the state of each LED indicator are also supplied for remote monitoring.
The functions of these discretes are defined in Table A--11.
Table A--11.
Color
Nomenclature
SCU Discrete Functions
Function
Green
Power
Indicates SCU is on and all voltages are correct when lit.
Green
SCU Valid
Indicates correct operation of the SCU logic and processing
circuits when lit.
Red
BIT Fail
• Indicates normal operation when off.
• Indicates BIT is running repetitively when flashing slowly.
Indicates the SCU has failed BIT when steadily lit.
• Indicates the SCU has failed BIT when steadily lit.
Amber
Signal 1
Indicates selection of input channel 1 when lit.
Amber
Signal 2
Indicates selection of input channel 2 when lit.
Amber
Signal 3
Indicates selection of input channel 3 when lit.
(2) Three amber LED indicators supply an error code that is displayed when the SCU
fails in the BIT mode. The red indicator lights and a three-bit code is continuously
displayed on the amber LEDs as indicated in Table A--12. BIT is interruptive and all
normal operation ceases during the time when the SCU is in the BIT mode.
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--12.
SCU Error Code
Code
LED 1
LED 2
LED 3
ARINC 429 translator not programmed
ON
OFF
OFF
RAM read/write failed
OFF
ON
OFF
ARINC 561 translator failed
ON
ON
OFF
PROM checksum failed
OFF
OFF
ON
ARINC 561 translator not programmed
ON
OFF
ON
Discrete input failed
OFF
ON
ON
ARINC 429 translator failed
ON
ON
ON
Failure
C. Control Functions
(1) Normal operation of the SCU is fully automatic and does not require operator
intervention. Some control functions are supplied through the main ARINC 600
connector. These functions include:
• Remote SCU on/off control
• BIT initiate control
• Signal select A
• Signal select B
• Program pin A
• Program pin B
• Program pin C.
(2) The remote SCU on/off control line enables the operation of the SCU power supply.
The control line is active low and must be connected to ground to enable operation of
the SCU. An open circuit or 28 V dc on this line shuts down operation of the SCU.
(3) The BIT initiate control line is an active low input used to enable BIT in the SCU. The
BIT mode is an optional function that supplies a pre/post-flight confidence check and
is intended for use by maintenance personnel as a diagnostic tool. The SCU remains
in the BIT mode as long as the BIT initiate control line is grounded. An open circuit or
28 V dc on this control causes the SCU to return to normal operation.
(4) Signal selection is normally an automatic function under control of the internal SCU
program and is based on the validity of the received data. The signal select control
lines supply an override of this automatic function to allow manual selection of one
input from three available sources. The signal select control lines are active low and
are internally pulled high. Manual selection is accomplished by applying a ground to
the control lines as given in Table A--13.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--13.
SCU Manual Signal Selection
Signal Select Control Lines
Automatic Selection
High
High
Select Input No. 1
Low
High
Select Input No. 2
High
Low
Select Input No. 3
Low
Low
Function
D. System Functions
(1) Initialization
(a) Operation begins with BIT when the SCU is activated by applying aircraft power
and grounding the on/off control line. Testing normally takes approximately 0.5
second and when BIT passes normal operation begins. If the SCU fails the initial
BIT check, the unit latches in the BIT mode and displays an error code with the
amber LED indicators.
(2) Automatic Input Selection Mode
(a) There are three available data input channels. Unless a channel is manually
selected, the input to be used by the SCU is selected automatically. After initially
selecting Channel 1, the SCU checks for the presence of the required valid
words in the input data stream and the status of the attitude warning discrete
from the selected synchro channel. If all validity conditions are met within 1.6
seconds from the initial channel selection, the SCU locks on to the current
channel and continues to operate from that data source. The appropriate amber
LED indicator lights to indicate the selected channel to operator. If any of the
required data is invalid, the SCU cycles to the next input channel until a channel
providing a complete frame of valid data is received.
(3) Valid Channel Condition
(a) Conditions that must exist to let the SCU accept the current input channel
include:
• At least one new data word for each of the required labels is received within
the specified time period.
• The sign/status matrix (SSM) of all words for all required labels must be valid.
• The primary attitude warning input discrete must be in a valid state to indicate
the synchro inputs for attitude are usable.
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MCS--4200/7200 Multi--Channel SATCOM System
(4) Channel Switching Timing
(a) The SCU allows 1.6 seconds for the selected input channel to receive a valid
data frame. However, if 1.6 seconds has passed and the valid channel
conditions have not been satisfied, the input channel cycles to the next
sequential channel. If all three input channels have been checked and none are
valid, the SCU prevents further cycling of the input channel selection for 1
minute. This prevents the SCU from continuously cycling when the inertial
navigation units or other sources of navigation data have not been initialized.
After the 1-minute delay, the SCU again initiates the checking cycle.
(5) Data Input
(a) A data subset made up of present latitude and longitude, true heading, track
angle, and ground speed is received through either the ARINC 561--6 wire inputs
or the ARINC 571--2 wire inputs as defined by the program pin selections. When
used as a selector of ARINC 404 data inputs, pitch and roll labels are also
included. The words are selected from the data stream by their octal labels while
other words are ignored. Program pin selections and associated data formats
and labels are defined in Table A--14 thru Table A--18.
Table A--14.
ARINC 561 Binary Data
Program Pin
Octal Label
Coded
310
Binary
Latitude of present position
311
Binary
Longitude of present position
212
Binary
Ground speed
213
Binary
Track angle
214
Binary
True heading
Table A--15.
Definition
ARINC 561 BCD Data
Program Pin
Octal Label
Coded
010
BCD
Latitude of present position
011
BCD
Longitude of present position
012
BCD
Ground speed
013
BCD
Track angle
014
BCD
True heading
Definition
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--16.
ARINC 571 Data, ARINC 429 Format
Program Pin
Octal Label
310
Latitude of present position
311
Longitude of present position
212
Ground speed
213
Track angle
214
True heading
Table A--17.
Definition
ARINC 571 Data, ARINC 419 Format
Program Pin
Octal Label
210
Latitude of present position
211
Longitude of present position
212
Ground speed
213
Track angle
214
True heading
Table A--18.
Definition
ARINC 404 Data, ARINC 429 Format
Program Pin
Octal Label
310
Latitude of present position
311
Longitude of present position
312
Ground speed
313
Track angle
314
True heading
324
Pitch
325
Roll
Definition
(b) The SSM of each received data word is checked. Valid words are converted to
ARINC 429 data. Invalid words are discarded.
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MCS--4200/7200 Multi--Channel SATCOM System
(c) With exception of the ARINC 404 input, the SCU also receives attitude data from
an associated attitude source. The attitude data is in the form of ARINC 407
pitch and roll synchro channels and an attitude warning flag. Attitude data is
selected from a source associated with the source selected for digital data. The
attitude inputs used are given in Table A--19.
Table A--19.
SCU Attitude Data Inputs
Data
Line Function
Roll
Synchro X
Roll
Synchro Y
Roll
Synchro Z
Pitch
Synchro X
Pitch
Synchro Y
Pitch
Synchro Z
Roll/Pitch
Reference HI
Roll/Pitch
Reference LO
Warning Flag
HI Flag (HI = Good)
(d) The pitch and roll synchro inputs are read every 20 milliseconds. The attitude
warning flag is sampled before each computation to check the validity of the
input data before the data is accepted.
(6) Data Output
(a) The SCU transmits ARINC 429 serial words at a rate of one complete
seven-word message every 20 milliseconds. The SSMs in the navigation data
words are based on those supplied by the digital input words. The SSM data for
the attitude words is derived from computations and from the primary warning
flag.
(b) The data output is in accordance with ARINC 429 high speed data (100 kHz
clock speed). The SCU outputs ARINC 429 data on two separate ports operating
in parallel. Data from both ports is identical, but independent output buffers are
used to supply redundancy.
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MCS--4200/7200 Multi--Channel SATCOM System
E.
ARINC 600 Connector Pin Assignments
(1) The rear connector (ARINC Part No. NIC66F11A00AA0) of the SCU complies with
ARINC Characteristic 600 as specified in the following:
• ARINC 600 -- Size MCU 2 no. 2 shell
• Type 0X top insert
• Type 0X middle insert
• Type 0X bottom insert
• Index pin code 0X.
(2) The contact arrangements for the connector are specified in Table A--20. An example
pin designation of BC12 for the table is given below.
Pin Designation Example: Pin BC12
B -- C -- 12
Connector Cavity Identifier
Top Cavity = A
Middle Cavity = B
Bottom Cavity = C
Column Identifier
(A, B, C, or D)
Row Identifier
(1 thru 15)
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--20.
Contact Arrangements for SCU ARINC 600 Connector
Function
Pin
Remarks
AC1
ARINC 561 Data No. 1 (HI)
Note 1.
AD1
ARINC 561 Data No. 1 (LO)
Note 1.
AC2
ARINC 561 Clock No. 1 (HI)
Note 1.
AD2
ARINC 561 Clock No. 1 (LO)
Note 1.
AC3
ARINC 561 Strobe No. 1 (HI) or ARINC 429/419 Data No. 1 (HI)
Note 1.
AD3
ARINC 561 Strobe No. 1 (LO) or ARINC 429/419 Data No. 1 (LO)
Note 1.
AC4
Spare
AD4
Spare
AC5
Spare
AD5
Spare
AC6
Spare
AD6
Spare
AC7
Spare
AD7
Spare
AC8
Spare
AD8
Spare
AC9
ARINC 561 Data No. 3 (HI)
Note 1.
AD9
ARINC 561 Data No. 3 (LO)
Note 1.
AC10
ARINC 561 Clock No. 3 (HI)
Note 1.
AD10
ARINC 561 Clock No. 3 (LO)
Note 1.
AC11
ARINC 561 Strobe No. 3 (HI) or ARINC 429/419 Data No. 3 (HI)
Note 1.
AD11
ARINC 561 Strobe No. 3 (LO) or ARINC 429/419 Data No. 3 (LO)
Note 1.
AC12
Spare
AD12
Spare
AC13
ARINC 407 Pitch No. 1 X
Note 2.
AD13
ARINC 407 Pitch No. 1 Y
Note 2.
AC14
ARINC 407 Pitch No. 1 Z
Note 2.
AD14
ARINC 407 Heading X
Reserved
AC15
ARINC 407 Heading Y
Reserved
AD15
ARINC 407 Heading Z
Reserved
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--20.
Contact Arrangements for SCU ARINC 600 Connector (cont)
Pin
Function
Remarks
AA1
ARINC 407 Pitch No. 3 X
Note 2.
AB1
ARINC 407 Pitch No. 3 Y
Note 2.
AA2
ARINC 407 Pitch No. 3 Z
Note 2.
AB2
Attitude Warning No. 1 (From Attitude Source)
Note 2.
AA3
ARINC 407 Reference No. 1 (HI)
AB3
ARINC 407 Reference No. 1 (LO)
AA4
ARINC 407 Heading Reference (HI)
Reserved
AB4
ARINC 407 Heading Reference (LO)
Reserved
AA5
ARINC 407 Reference No. 3 (HI)
AB5
ARINC 407 Reference No. 3 (LO)
AA6
Attitude Warning No. 3 (From Attitude Source)
AB6
Spare
AA7
ARINC 407 Roll No. 1 X
Note 2.
AB7
ARINC 407 Roll No. 1 Y
Note 2.
AA8
ARINC 407 Roll No. 1 Z
Note 2.
AB8
Spare
AA9
Spare
AB9
Spare
AA10
Spare
AB10
Spare
AA11
ARINC 407 Roll No. 3 X
Note 2.
AB11
ARINC 407 Roll No. 3 Y
Note 2.
AA12
ARINC 407 Roll No. 3 Z
Note 2.
AB12
Spare
AA13
ARINC 404 Echo (HI)
Note 3.
AB13
ARINC 404 Echo (LO)
Note 3.
AA14
Spare
AB14
Spare
AA15
Spare
AB15
Spare
Note 2.
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--20.
Contact Arrangements for SCU ARINC 600 Connector (cont)
Pin
Function
Remarks
BC1
ARINC 407 Pitch No. 2 X
Note 2.
BD1
ARINC 407 Pitch No. 2 Y
Note 2.
BC2
ARINC 407 Pitch No. 2 Z
Note 2.
BD2
Spare
BC3
ARINC 407 Roll No. 2 X
Note 2.
BD3
ARINC 407 Roll No. 2 Y
Note 2.
BC4
Spare
BD4
ARINC 407 Roll No. 2 Z
BC5
Spare
BD5
Attitude Warning No. 2 (From Attitude Source)
BC6
ARINC 407 Reference No. 2 (HI)
BD6
ARINC 407 Reference No. 2 (LO)
BC7
Signal Source Select A (Input No. 1)
Note 4.
BD7
Signal Source Select (Input No. 2)
Note 4.
BC8
BIT initiate (Input No. 3)
Note 5.
BD8
Spare
BC9
BIT Failed (Output No. 2)
Reserved
BD9
SCU Valid
Reserved
BC10
Superflag (+28 V dc = Output Valid)
Note 6.
BD10
/Superflag (<1 V dc = Output Valid)
Note 6.
BC11
Program Pin A (Input No. 5)
Note 7.
BD11
Program Pin B (Input No. 6)
Note 7.
BC12
Program Pin C (Input No. 7)
Note 7.
BD12
Spare
BC13
Spare
BD13
Spare
BC14
Spare
BD14
Spare
BC15
ARINC 429 Out No. 1 (HI)
BD15
ARINC 429 Out No. 1 (LO)
Note 2.
Note 2.
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--20.
Contact Arrangements for SCU ARINC 600 Connector (cont)
Pin
Function
Remarks
BA1
Spare
BB1
Spare
BA2
ARINC 429 Out No. 2 (HI)
BB2
ARINC 429 Out No. 2 (LO)
BA3
Spare
BB3
Spare
BA4
Discrete Out No. 3 (Select No. 2 LED)
Reserved
BB4
Discrete Out No. 4 (Select No. 3 LED)
Reserved
BA5
Discrete Out No. 5 (Select No. 1 LED)
Reserved
BB5
Discrete Out No. 6
Reserved
BA6
Discrete Out No. 7
Reserved
BB6
Discrete Out No. 8
Reserved
BA7
ARINC 561 Data No. 2 (HI)
Note 1.
BB7
ARINC 561 Data No. 2 (LO)
Note 1.
BA8
ARINC 561 Clock No. 2 (HI)
Note 1.
BB8
ARINC 561 Clock No. 2 (LO)
Note 1.
BA9
ARINC 561 Strobe No. 2 (HI) or ARINC 429/419 Data No. 2 (HI)
Note 1.
BB9
ARINC 561 Strobe No. 2 (LO) or ARINC 429/419 Data No. 2 (LO)
Note 1.
BA10
+28 V dc Power
Aircraft Power (Note 8.)
BB10
+28 V dc Power
Aircraft Power (Note 8.)
BA11
0 V dc Power Return
Aircraft Power (Note 8.)
BB11
0 V dc Power Return
Aircraft Power (Note 8.)
BA12
Chassis Ground
BB12
Remote SCU On/Off Control
Note 9.
BA13
Shield return
Connected to Chassis
BB13
Shield Return
Connected to Chassis
BA14
115 V ac Power 400 Hz (HI)
Aircraft Power (Note 8.)
BB14
Chassis Ground
BA15
115 V ac Power 400 Hz (LO)
Aircraft Power (Note 8.)
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table A--20.
Contact Arrangements for SCU ARINC 600 Connector (cont)
Pin
BB15
Function
Remarks
Chassis Ground
NOTES:
1.
The 6-wire ARINC 561 or 2-wire ARINC 429/419 (ARINC 571/404) data can be routed from up to three sources.
However, if a single input is supplied, it should be connected to the No. 1 inputs as indicated. Inputs No. 2 and 3
should be left open. The type of data being used, either ARINC 561 or ARINC 571/404, must be indicated by
selecting the proper program pins as specified in NOTE 7. Also, refer to NOTE 4. for more information on selecting
a specific input as the data source.
2.
The synchro pitch and roll data can be routed from up to three sources. However, sources of attitude data must be
paired with sources of ARINC 561 or ARINC 571 data. Thus, if only one source of ARINC 561 or ARINC 571 data
is available, then only one source of attitude data can be used. An attitude warning flag for each source of attitude
that is active must be supplied. +28 V dc = valid. Ground or open = invalid.
3.
When the SCU is used as a selector/controller of multiple ARINC 404 compatible data sources, the receiving
equipment should be connected to the ARINC 404 echo outputs. In this configuration, the input as valid by the
SCU is routed back out of the unit on these pins. Since attitude data is embedded in the ARINC 404 data stream,
no attitude inputs are used.
4.
When multiple sources of data are available and routed to the SCU, it automatically searches for an input with valid
attitude data and ARINC 561/571 data. If only one source of ARINC 561/571 data and attitude data is available, the
SCU should be connected to only one input and the signal source select lines should be linked as applicable for
the selected input as given in Table A--21.
5.
Grounding the BIT initiate input forces the SCU to enter the interruptive BIT mode and repetitively do its BIT
routines until ground is removed. BIT is automatically done at each power-up cycle. This input should be an open, if
not used.
6.
The superflag output is +28 V dc whenever the SCU is operating normally and the output data is valid. If a portion
of the input data is invalid or the SCU detects an internal fault, then the superflag output is 0 V dc. The /superflag
output is the inverse of the superflag output.
7.
The data format and characteristics accepted by the SCU are programmable through pins A, B, and C. The
combinations supported by the SCU are specified in Table A--22.
8.
The SCU operates from either +28 V dc or 115 V ac, 400 Hz power. The power source not used should remain
unconnected.
9.
The remote SCU on/off control can be used to power down the SCU from a remote location. A ground activates the
unit and an open switches the unit off. If remote control is not required, this pin should be permanently grounded at
the connector.
Table A--21.
Signal Source Select Lines
Signal Source Select
Auto
Open
Open
Input No.1
Ground
Open
Input No. 2
Open
Ground
Input No. 3
Ground
Ground
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MCS--4200/7200 Multi--Channel SATCOM System
Table A--22.
SCU Program Pin Combinations
Program Pins
ARINC 561 data, binary labels, synchro attitude
ARINC 561 data, BCD labels, synchro attitude
ARINC 571 data with ARINC 429 format, synchro attitude
ARINC 571 data with ARINC 419 format, synchro attitude
Input Description
NOTE: Ground = 1; open = 0.
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MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX B
INSTALLATION PROCEDURES FOR SATCOM AIR FILTRATION
SYSTEMS
1. Introduction
A. General
(1) Appendix B contains information on the different air filtration systems available for the
SATCOM installations. Procedures for installing these air filtration systems are also
supplied. After you have determined the proper air filtration system for your needs,
follow the appropriate procedures in paragraph 4.
(2) The SATCOM system (SDU and HPA) is designed to ARINC 600 standards including
ARINC 600 cooling requirements. ARINC 600 calls for the cooling air to contain no
contamination particles in excess of 400 microns. Several installation designs do not
supply cooling air in accordance with ARINC 600. The OEM installation design for the
B747, B767, and B777 supply unfiltered cooling air (cabin air) to the SATCOM LRUs.
As a result, contaminants in the air tend to accumulate on and inside the LRUs
sometimes blocking off the cooling air passages. This leads to units operating at a
higher temperature, which can result in decreasing the MTBF of the units.
(3) Filter assemblies have been designed that attach to the SATCOM LRUs or to the
LRU trays. These filter assemblies contain filter media that filter out contaminants
before entering the LRUs. This design is for installations where the cooling air is
drawn through the LRU top to bottom, and where there is at least 1 inch of clearance
above the LRUs to allow for the assembly itself. Thus, the air filtration units included
in this appendix are acceptable for installation on the B747 and B777 aircraft, but
because of clearance problems, are not acceptable for installation on the
OEM-provisioned B767 aircraft.
2. Continued Airworthiness
A. General
CAUTION: THE FILTER MEDIA MUST BE REPLACED (OR CLEANED) APPROXIMATELY
EVERY 4000 FLIGHT HOURS OR EVERY C CHECK, WHICHEVER COMES
FIRST, OR THE EFFECTIVENESS OF THE AIR FILTRATION ASSEMBLY CAN
BE DEGRADED.
(1) The selection of the type of filter media cartridge is based on the following:
• Effectiveness of the filter media in removing contaminants from the cooling air
before entering the SATCOM LRUs.
• Impact of the filter media on the cooling air mass flow rate through the units.
• Time between removals.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
3. Equipment and Materials
A. General
CAUTION: DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO
MATERIALS SPECIFIED BY HONEYWELL. MATERIALS NOT
EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN
MAKE THE WARRANTY NOT APPLICABLE.
(1) Refer to Table B--1 for a list of materials.
Table B--1.
Materials
Description
Item
Source
HMN 9730178
Retaining compound
Loctite Corp, Rocky Hill, CT
(MIL--S--22473, grade A) — Grade (05972)
HMN 9731178
Primer for retaining compound,
ready--to--use, quick
(MIL--S--22473, grade T, form R)
— Locquic Grade T
NOTES: NOTES:
1.
Equivalent alternatives are permitted for equipment and materials in this list.
2.
The HMN codes in the list of materials identify the Honeywell Material Number (HMN) given to each material.
(2) The equipment listed in Table B--2, Table B--3, and Table B--4 supplies the necessary
hardware to install air filtration systems on the aircraft. Find the air filtration system
and filter that best fits your needs and contact the company that manufacturers that
particular equipment.
Table B--2.
Equipment
Air Filtration Systems from ECS for a Top Mount Assembly
Quantity
LRU
Part No.
SATCOM System
SATCOM Filter Assembly
SDU
10919--101
6--MCU assembly
SATCOM Filter Assembly
HPA (20W)
10968--101
4--MCU assembly
SATCOM Filter Assembly
HPA (40W)
10923--101
8--MCU assembly
Filter Cartridge Assembly
SDU
10907--105
6--MCU assembly
Filter Cartridge Assembly
HPA (20W)
10907--104
4--MCU assembly
Filter Cartridge Assembly
HPA (40W)
10907--106
8--MCU assembly
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table B--3.
Air Filtration Systems from ECS for a Body--Mounted Design
Equipment
Quantity
LRU
Part No.
SATCOM System
SATCOM Filter Assembly
SDU
P0329--106
6--MCU assembly
SATCOM Filter Assembly
HPA (20W)
P0329--104
4--MCU assembly
SATCOM Filter Assembly
HPA (40W)
P0329--108
8--MCU assembly
Filter Cartridge Assembly
SDU
20008--05
6--MCU assembly
Filter Cartridge Assembly
HPA (20W)
20008--04
4--MCU assembly
Filter Cartridge Assembly
HPA (40W)
20008--06
8--MCU assembly
Table B--4.
Air Filtration Systems from ECS for a Tray--Mounted Design
Equipment
Quantity
LRU
Part No.
SATCOM System
SATCOM Filter Assembly
SDU
20005--103
6--MCU assembly
SATCOM Filter Assembly
HPA (20W)
20005--102
4--MCU assembly
SATCOM Filter Assembly
HPA (40W)
20005--104
8--MCU assembly
Filter Cartridge Assembly
SDU
20008--05
6--MCU assembly
Filter Cartridge Assembly
HPA (20W)
20008--04
4--MCU assembly
Filter Cartridge Assembly
HPA (40W)
20008--06
8--MCU assembly
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
4. Installation Instructions
A. Top Mount Assembly
(1) The ECS top mount air filtration assembly is designed to clamp to the top of the
SATCOM LRUs so it does not come off the LRU. Once attached to the top of the
LRU, it forms a seal letting only filtered air enter the LRU. The assembly is held to the
top of the LRU by friction from the sides of the assembly and by the clamps that
supply friction to the front and rear panels of the unit. Figure B--1 shows the location
of the components for the following procedures.
(2) Install the filter assembly to an SDU or HPA using the following steps.
(a) Make sure the correct size assembly is selected for the given LRU (refer to
Table B--2).
(b) OPTIONAL — Remove the SATCOM LRU from its tray and set it on a secure
surface. (The assembly can be installed while the unit is in the rack.)
(c) Install the air filtration media inside the air filtration assembly in the rectangular
filter frame.
(d) Place the filter assembly over the top of the LRU with the clamps in the up
(thumb lever over the top of the filter assembly) position and pointing toward you.
(e) Push down on the air filtration unit until it fits over the top of the SATCOM LRU.
The sides of the air filtration assembly may need to be spread open slightly prior
to sliding over the sides of the LRU.
(f)
Once the air filtration unit is firmly seated to the top of the LRU, clamp the
assembly to the unit by pushing down on the two thumb levers until they lock into
position. The thumb levers pass through approximately 180 degrees of rotation
for the clamping process.
(g) Make sure the air filtration assembly remains seated firmly against the top of the
LRU to maintain the air seal.
(h) Make sure the air filtration assembly is held tightly to the unit by gently lifting up
on the assembly; making sure the assembly does not pull off of the LRU.
(i)
OPTIONAL -- Install the SATCOM LRU back into its tray if removed in step
4.A.(2)(b).
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Figure B--1.
ECS Top Mount Air Filtration Assembly
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
(3) Replace the filter media according to the following steps.
(a) Gain access to the SATCOM LRUs.
(b) Lift up on the two thumb levers (approximately 180 degrees).
(c) Pull up on the air filtration unit until it lifts off the top of the SATCOM LRU. The
sides of the air filtration assembly may need to be spread open slightly prior to
sliding up the sides of the LRU.
(d) Remove the air filtration media from the air filtration assembly in the rectangular
filter frame.
(e) Once the assembly is removed, pull the filter assembly out of its retaining fixture
and discard the filter appropriately.
(f)
Obtain a new filter.
(g) Make sure the correct size filter assembly is selected for the given LRU (refer to
Table B--2).
(h) Install the new filter media into the filter assembly retaining fixture.
(i)
OPTIONAL — Remove the SATCOM LRU from its tray and set on a secure
surface. (The assembly can be installed while the unit is in the rack.)
(j)
Install the air filtration media inside the air filtration assembly in the rectangular
filter frame.
(k) Place the filter assembly over the top of the LRU with the clamps in the up
(thumb lever over the top of the filter assembly) position and pointing toward you.
(l)
Push down on the air filtration unit until it fits over the top of the SATCOM LRU.
The sides of the air filtration assembly may need to be spread open slightly prior
to sliding over the sides of the LRU.
(m) Once the air filtration unit is firmly seated to the top of the LRU, clamp the
assembly to the unit by pushing down on the two thumb levers until they lock into
position. The thumb levers will pass through approximately 180 degrees of
rotation for the clamping process.
(n) Make sure the air filtration assembly remains seated firmly against the top of the
LRU to maintain the air seal.
(o) Make sure the air filtration assembly is held tightly to the unit by gently lifting up
on the assembly to verify the assembly does not pull off the LRU.
(p) OPTIONAL -- Install the SATCOM LRU back into its tray if removed in step
4.A.(3)(i).
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
B. Body--Mounted Assembly
(1) The ECS body-mounted air filtration assembly is designed to strap around the body
of the SATCOM LRUs in a way that it will not come off the LRU. Once attached to the
LRU, it forms a seal allowing only filtered air to enter the LRU. The assembly is held
to the top of the LRU with a strap that fits securely around the body of the unit. The
filtration unit sits on top of the SATCOM LRU. The strap runs down the side,
underneath, and up the other side of the LRU. By way of a clamping system on top of
the LRU, the strap is pulled tight, which firmly secures the filter assembly to the top of
the unit.
(2) Install the filter assembly to an SDU or HPA according to the following steps.
(a) Make sure the correct size assembly is selected for the given LRU
(refer to Table B--3).
(b) Remove the SATCOM LRU from its tray and set it on a secure surface.
(c) Slide the filter strap around the front of the LRU so the strap is underneath and
coming up each side of the LRU.
(d) Place the filter assembly on top of the LRU so the back lip of the assembly unit
fits over the back of the LRU.
(e) Pull the strap around the top of the filter assembly unit so the two ends of the
strap overlap. The strap should come over the top of the filter assembly on the
front end of the assembly (dog-house end of the LRU). A channel is built into the
filter assembly for the strap.
(f)
With the strap in place, latch the strap together by inserting the lips of the strap
ends together so they latch together. With the LRU facing you, the strap on the
left-hand side should latch over the top of the strap on the right-hand side.
(g) Once the strap is latched, make sure the lip on the rear of the filter assembly is
seated firmly just over the rear of the LRU.
(h) Make sure the filter retainer mechanism is latched closed.
(3) Replace the filter media according to the following steps. Figure B--2 shows the
location of the components used.
(a) Gain access to the SATCOM LRUs.
(b) Locate the filter retaining clips located on the forward end of the filter assembly
mechanism.
(c) Slide the retainer clips (one on the left and one on the right) out to disengage the
clips from the latching pins.
(d) Lift the filter retaining tray up, (hinged on the rear side) remove the filter media
cartridge and discard the filter appropriately.
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MCS--4200/7200 Multi--Channel SATCOM System
(e) Install the new filter media by placing a new filter media cartridge in the filter
retaining tray chamber.
(f)
Lower the filter retaining tray down until the locating pins protrude through the
clearance holes on the filter retaining tray.
(g) Slide the retaining clips (left and right) in until they latch around the latching pins.
C. Tray--Mounted Assembly
(1) The ECS tray-mounted air filtration assembly is designed as an integral part of the
equipment tray and does not attach to the LRU itself. The SATCOM LRU slides into
the tray, sandwiched between the tray and plenum below, and the air filtration
assembly above. Since the air filtration assembly is an integral part of the equipment
tray, in order to install this type of assembly, a modified equipment tray must be
purchased for each LRU.
(2) Replace the filter media according to the following steps. Figure B--2 shows the
location of the components used.
(a) Gain access to the SATCOM LRUs.
(b) Locate the filter retaining clips located on the forward end of the filter assembly
mechanism.
(c) Slide the retainer clips (one on the left and one on the right) out to disengage the
clips from the latching pins.
(d) Lift the filter retaining tray up (hinged on the rear side) and remove the filter
media cartridge. Discard the filter media cartridge appropriately.
(e) Install the new filter media by placing a new filter media cartridge in the filter
retaining tray chamber.
(f)
Make sure the filter cartridge is supported on the air plenum seals. The direction
of airflow through the filter is not important.
(g) Lower the filter retaining tray until the locating pins protrude through the
clearance holes on the filter retaining tray.
(h) Slide the retaining clips (left and right) in until they latch around the latching pins.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Figure B--2.
Front and Side Views Showing Filter Removal
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX C
OWNER REQUIREMENTS TABLE
1. Overview
A. General
(1) Appendix C contains information on the ORT and is stored in non--volatile memory in
the SDU. The ORT contains information relating to different areas of functionality,
such as log-on and telephony. The ORT does not lose its contents because of the
loss of SDU primary power or as a result of PAST. All ORT contents are set to default
values by a factory settings restart. The ORT contains all pilot and aircraft operator
entered information preserved when the SDU is powered-down. The characteristics
of the ORT are specified in Table C--1.
NOTE: Honeywell supplies Windows--based software (ORT editor) that is used to
generate the ORT files for upload. Contact your Honeywell representative for
a copy of this software.
Table C--1.
ORT Item
Characteristic
Attributes
ORT Characteristics
Description
Log-On Policy
Secured,
common
This item defines the log-on procedure. When the SDU has
power applied, the SDU either starts the automatic log-on
procedure at the earliest opportunity (automatic), or the SDU
goes to an inert standby state, even if the SDU is entirely
failure free, where the SDU then waits for user stimulus to
start logging-on (commanded).
ii
Satellite/GES
Names
User,
common
This item defines associated names for the satellites and
GESs. Satellite names are up to five characters long. GES
names are up to 14 characters long. Names made up of
upper case letters, decimal digits, hyphens, and spaces are
allowed. A GES name can include satellite and service
identifying strings; e.g., GOON A--E SKY takes 12 characters
and identifies Goonhilly, the United Kingdom GES servicing
the Skyphone consortium and using the Atlantic ocean region
east satellite.
iii
GES Preference
Values
User,
common
This item defines the automatic log-on preference values for
GESs from 0 to 9, where 9 corresponds to the most preferred
GES. The interpretation of preference value 0 is determined
by item lvi, 0 is either the least preferred GES or it is not used
for automatic log-on. GESs with preference level 0 can still be
used for a constrained log-on. When all GESs on a particular
satellite have a preference level of 0 and this satellite
becomes the candidate for logon, the logon processing
considers all of these GESs to have a preference level of 1 to
facilitate continued SATCOM operation.
iv
Maintenance
Page Access
User,
common
This item defines whether the SCDU maintenance pages are
accessible as: a) never; b) always; or c) only when the aircraft
is on the ground.
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MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
Cockpit
Telephone
Numbers
Attributes
User,
common
ORT Characteristics (cont)
Description
This item defines up to 100 telephone numbers as follows:
• Each made up of up to 18 numeric characters (including
optional spaces and/or trailing network ID preceded by a
slash)
• Each number having an associated priority value
(i.e., 1 thru 4), protection (i.e., protected or unprotected),
and a mnemonic of up to 14 characters
• All are located in four user-definable categories of no more
than 25 telephone numbers each.
If configuration pin TP13A is set to the zero state, every entry
with a priority 4 is modified to a priority 3 following an ORT
upload or following a POST/PAST where priority 4 numbers
existed prior to TP13A being set to the zero state. In a dual
system, this modification takes place only if strap TP13A is in
the zero state on both SDU systems. This item includes
manually entered telephones from the SCDU CATEGORY
NUMBERS pages.
vi
Deleted
vii
Resources
Reserved for
Headset
User,
common
When enabled, this item reserves the following resources for
cockpit headset use at all times: one codec, one modem, and
sufficient HPA power to support an extra C--channel in all
prevailing circumstances. These resources are capable of
being reserved for either of the cockpit audio channels. In a
dual system, channel refers to logical channel.
viii
Response
Capability to
Log-On
Interrogation
N/A
This item is not considered part of the MCS ORT, since the
AES always supports log-on interrogation. There is always
one SDU modem dedicated to P--channel reception and
capable of R--channel and T--channel transmission.
ix
Use and Value of
Flight
Identification
N/A
This item is not considered part of the MCS ORT since the
value is dynamic and is obtained from the CFDS/CMC/OMS
or SCDU (along with item xxxiv).
Ground-to-Air
Circuit-Mode
Data
User,
common
This item defines the allowing/disallowing of analog
interconnect circuit-mode data on ground-to-air calls. It lets
the AES identify itself to the GES as being data capable and
the owner/operator anticipates receiving ground-to-air calls
that need circuit-mode data service, thereby directing the
GES to assign data capable channels to all ground-to-air
calls.
xi
Deleted
xii
Deleted
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MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
Attributes
ORT Characteristics (cont)
Description
xiii
Ground-to-Air
Calls
User,
common
This item defines the allowing/disallowing and routing of
ground-to-air priority 4 calls. If calls are allowed and if two or
more of the AES voice user interfaces (i.e., digital phones,
analog handset, or headset) are fitted, this item specifies
which destination (digital phone, analog handset, or headset)
incoming priority 4 calls are routed. However, routing to the
headset is only possible if configuration pin TP13A is set to
the one state. If TP13A is set to the zero state, the ORT
setting is modified to Disallowed following a factory setting
restart, an ORT upload with headset selected, or a
POST/PAST if headset was selected prior to TP13A being set
to the zero state. In a dual system, ground-to-air priority 4
calls can be routed to an interface that is installed on at least
one of the SDU systems. Routing to HEADSET is only
possible if at least one SDU system has a codec wired to
AMS with TP13A strap in the one state (on this same SDU
system).
xiv
Call Camp-On
Duration
User,
common
This item defines the camp-on duration be either indefinite, or
a specified time-out period in the range of 1 to 15 minutes, or
a time--out period of zero minutes (immediate time--out).
xv
Camp-On
Time-out Action
User,
common
This item defines whether the camp-on time-out action is to
(a) preempt (if a candidate call exists) or to cancel camp-on
(if no candidate call exists), or (b) to cancel camp-on.
xvi
Stored APHONE
(WH--10)
Telephone
Numbers
User,
duplicated
This item defines up to 10 stored telephone numbers (9
numbers plus last number redial), with each telephone
number made up of up to 18 digits, for each of the two analog
(APHONE) WH--10 channels. All such telephone numbers are
priority 4 and the priority is not modifiable. These two sets of
stored telephone numbers can be separate (distinct) or
shared as specified in ORT item xxvi.
xvii
Deleted
xviii
Noise Insertion
Level
Secured,
common
This item defines whether to enable or disable noise insertion
on ground-to-air circuit-mode telephone calls. When noise
insertion is enabled, this item also defines the level, as
selected. Noise insertion minimizes annoying noise
modulation when the GES drops the carrier in the forward
(to--aircraft) direction during speech pauses.
xix
Ground-to-Air
Preemption
User,
common
This item defines whether or not incoming calls of priority 2
and/or 3 automatically preempt (as necessary) a candidate
call as specified in SYSTEM DESCRIPTION. Priority 1
ground-to-air calls unconditionally preempt other calls of lower
priority as necessary.
xx
Preferred Cockpit User,
Call Routing
common
This item defines the routing of ground-initiated cockpit voice
calls to a particular channel when two channels are available.
This item does not affect which channel should be preempted
if both channels are not available. In a dual system, channel
refers to logical channel.
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MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
ORT Characteristics (cont)
Attributes
Description
xxi
Preferred
APHONE Call
Routing
User,
duplicated
When allowed by item xiii, this item defines the routing of
ground-to-air priority 4 calls, when allowed in accordance with
item xiii, to a particular channel when two APHONE channels
are available. In a dual system, this item specifies the
preferred physical channel on each SDU system, or None
when there is no channel wired to APHONE on that system.
xxii
HGA Tx Gain
Threshold
Secured,
common
This item specifies the threshold on the reported HGA Tx gain
for stimulating log-on renewal at Class 1 or automatic
handover.
xxiii
Analog telephone Secured,
(APHONE)
duplicated
System
Management
Commands
This item defines the allowing/disallowing of system
management commands from the analog phone (APHONE)
interface (WH--10 or APBX).
xxiv
Analog telephone User,
(APHONE)
duplicated
Outgoing Call
Barring Level
This item defines one of three levels for analog phone call
barring. Level 0 allows all outgoing calls and the Store Phone
Number Memory command specified in SYSTEM
DESCRIPTION, but disallows six-digit numbers between
42XXXX and 47XXXX if accompanied by credit card data.
Level 1 allows only stored phone numbers, directly dialed
short-code phone numbers, and long dialed numbers from the
APBX accompanied with credit card data to initiate outgoing
calls. Level 1 disallows manually dialed full-length phone
numbers not accompanied with credit card data, six-digit
numbers between 42XXXX and 47XXXX if accompanied by
credit card data, and the Store Phone Number Memory
command. Level 2 disallows all outgoing calls, both manual
and stored numbers, and the Store Phone Number Memory
command.
NOTE: The six-digit numbers between 42XXXX and
47XXXX have been designated air traffic control
(ATC) destinations. These numbers may be dialed
at any priority and are assigned a network ID of 1.
In order to prevent unauthorized use of these
numbers once they become publicly available, the
AES filters these numbers appropriately. The
filtering specified prohibits these numbers from
being dialed with credit card data present based on
the assumption anyone making a call to one of
these numbers using a credit card is not an
authorized user (i.e., a passenger).
xxv
Call Barring
Security Code
This item defines a four-digit password that, if entered
through the analog phone (APHONE), allows call barring
commands (SYSTEM DESCRIPTION) to be accepted.
User,
duplicated
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MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Characteristics (cont)
ORT Item
Characteristic
Attributes
Description
xxvi
Shared Analog
Telephone
(WH--10)
(APHONE)
Number Storage
User,
duplicated
This item defines whether the 10 stored numbers (9 numbers
plus the last number redial) maintained for each of the analog
phone (APHONE) channels are separate or shared (i.e.,
whether a phone number stored on a channel is accessible
by the dial stored phone number command on the other
channel).
xxvii
Deleted
xxviii
Default HPA
Backoff Limits
Secured,
duplicated
This item defines the maximum backoff values for the linear
and class C HPAs. The working (volatile) values are
automatically updated by non zero values (i.e., other than
16 dB) received in the HPA backoff range fields of valid HPA
status words. The nonvolatile entries are not modified with
the received values.
xxix
HPA Minimum
Reportable
Actual Power
Output
Secured,
duplicated
This item defines the minimum values of actual power output
capable of being reported through the HPA status words by
the linear and class C HPAs. When this value or a lower value
is reported in the HPA status word, calibration is inhibited.
xxx
Default Assumed Secured,
Global Beam
common
Initial C--Channel
EIRP
This item defines the default assumed global beam initial
C--channel EIRP. This value is used to assess the power
availability for a C--channel call in the absence of any existing
C--channels.
xxxi
SCDU Telephone Secured,
Number
common
Preselect
This item defines whether selection of a phone number on
one of the CATEGORY NUMBERS pages preselects the
phone number or initiates a call using the phone number. If
this item is enabled, the selection of a phone number on one
of the CATEGORY NUMBERS pages or manual entry of a
phone number on the DIRECTORY page retrieves the
selected number to the SATCOM MAIN MENU page
(TESTING/FAULT ISOLATION), where the number can then
be dialed by selecting the MAKE CALL prompt or by any of
the call initiation methods triggered by activation of an input
discrete.
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MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
xxxii
Characteristic
ACP Call
Initiation
Attributes
Secured,
common
ORT Characteristics (cont)
Description
This item enables/disables ACP call initiation. This item can
only be enabled when item xxxi is enabled. If enabled, one of
the following two pairs of SDU discretes are capable of being
used for call initiation (when the associated cockpit voice call
light outputs are open), based on the state of program pin
TP13K:
• Cockpit voice mic on inputs — if the latched ACP
hookswitch signaling method is strapped.
• Place/End call discrete inputs — if the switched PTT
hookswitch signaling method is strapped.
In either case, this item specifies whether the number dialed
should come from the ATC phone number register rather than
the SCDU MAIN menu. If the MAIN menu is selected, the
phone number displayed on the SATCOM MAIN MENU (3L
label line for channel 1, or 5L label line for channel 2) is used
for call initiation. If the ATC menu is selected, the phone
number displayed on the ATC menu is used for call initiation
on either cockpit channel. In a dual system, this item is
enabled if the straps of both SDU systems are identical.
xxxiii
User (or
Composite)
Partition ORT
Description
User,
common
This item defines the 24-character field to describe the ORT.
The ORT description is a 24-character field that annotates a
particular set of options, in order to distinguish one set from
another (e.g., NORTH PACIFIC ROUTE, SOUTH ATLANTIC
ROUTE, 747--400 ASIAN ROUTE, 777 ASIAN ROUTE).
Alternatively, this item could contain a software identification
(e.g., a software part number for the ORT as a released
entity). If the ORT version is for a composite file, the
description field is for the entire ORT and item liii is not used.
See item liii also.
xxxiv
Airline Code
User,
common
This item defines an airline code made up of up to four ISO--5
characters to be used with a four-digit BCD flight number
received from a McDonnell Douglas CFDIU (SYSTEM
DESCRIPTION) in constructing a flight identifier for log-on.
This is only used if the CFDS/CMC/OMS does not supply the
airline code.
xxxv
Headset
Outgoing Call
Barring Level
User,
common
This item defines one of two levels for headset call barring.
Level 0 allows all outgoing calls. Level 1 allows only stored
phone numbers, manually dialed short-code numbers, and
manually dialed numbers with a network ID other than 1. For
Level 1 call barring, all cockpit stored numbers are treated as
protected (i.e., they cannot be modified from the SCDU).
xxxvi
Headset Transit
Call
User,
common
This item either enables or disables transit calls from the
headset for line select key 4L.
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Page C--6
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
Attributes
ORT Characteristics (cont)
Description
xxxvii
User ORT
User,
Partition Modified common
Flag
This item indicates whether any item in the nonvolatile copy
of the user partition of the ORT partition has been modified
since the ORT was created in a configured state by the
PC-based off-line ORT editing tool. When any user-partition
ORT item is modified in nonvolatile memory by the SDU
software, either directly or indirectly, this flag is set to
modified. This value is never set to unmodified by the SDU
software. Its value is displayed on the SCDU, on the CFDS,
on the front panel display of the SDU, and on the CMT.
xxxviii
Failure Masking
Data
Secured,
common
This item is made up of a list of up to 50 failures (Level I
code, SRU code, and failure code) whose operation is
masked or suppressed. A switch is stored with each specified
failure to indicate whether that failure should never be raised
(i.e., the failure annunciation and reversion should be
suppressed completely), or whether the failure should be
annunciated normally (i.e., recorded and reported as
specified in TESTING/FAULT ISOLATION) when declared,
but not indict the appropriate functional resource specified for
the failure (i.e., not take any other action in response to the
failure, such as reconfiguring redundant resources). Unused
entries in this table are represented by the Level I code, SRU
code, and failure code all set to zero.
xxxix
Elevation
Handover
Threshold
Secured,
common
This item, ranging in integer degrees between 0° and 90°, is
used in combination with calculated elevation of the highest
satellite to determine at what elevation to initiate a handover
from the current satellite. This item is also used to determine
when a satellite is not high enough in elevation to be
considered in view for acquisition purposes by the automatic
log-on process.
High Rate Data
User,
Transmit Support common
This item made up of two flags that specify (by being set to
enabled or disabled) whether the SDU indicates support for
10,500 bps R-- and T--channels in its log-on request of class
2, 3, and 4 (i.e., when using a high gain antenna), for the
global beam and spot beam log-on requests, respectively.
xl
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Page C--7
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
xli
Characteristic
Attributes
Automatic Transit Secured,
Call GES Table
common
ORT Characteristics (cont)
Description
This item indicates the transit GES ID to be specified in an
air-to-ground call setup request (SYSTEM DESCRIPTION) if
no transit GES ID has been explicitly specified through the
initiating user interface (APHONE, Headset, DPHONE). If the
GES ID in the table is 377 octal (indicating null), then the
log-on GES is used in the call setup request. For each
satellite ID of 0, 1, 2, and 3, the table stores a GES ID to be
used with the following types of calls:
• Any PSTN long number call (i.e., with network ID 1, with
between 7 and 18 digits, beginning with 00) with country
code beginning with 1 (i.e., North America)
• Any PSTN long number call with a country code beginning
with 2 (i.e., Africa)
• Any PSTN long number call with a country code beginning
with 3 (i.e., South and West Europe)
• Any PSTN long number call with a country code beginning
with a 4 (i.e., North and East Europe)
• Any PSTN long number call with a country code beginning
with a 5 (i.e., South America)
• Any PSTN long number call with a country code beginning
with a 6 (i.e., South East Asia and Australia)
• Any PSTN long number call with a country code beginning
with a 7 (i.e., Soviet Union)
• Any PSTN long number call with a country code beginning
with an 8 (i.e., Far East)
• Any PSTN long number call with a country code beginning
with a 9 (i.e., India and Middle East)
• Any PSTN short number call (i.e., network ID of 1, with
between 2 and 6 digits not beginning with 00)
• Any non-PSTN call (i.e., with network ID other than 1).
The geographical region associated with each zone is
approximate; refer to Figure 1--3 for details of individual
country codes.
xlii
Air-to-Ground
Chime
Secured,
common
This item defines one of three chime options. These options
only affect air-to-ground chime activation for call annunciation
and the setting of SDU-to-ACARS MU/CMU status word bits.
The first option is to always chime and always set the
appropriate bits. The second option is to chime and set the
appropriate bits only if the call was camped-on. The third
option is to never chime and never set the bits.
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Page C--8
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
Attributes
ORT Characteristics (cont)
Description
xliii
SCDU Call
Prompts
Secured,
common
This item defines one of three levels of SCDU call prompt
display. Level 0 causes all SCDU call prompts to be
displayed. Level 1 causes the ANSWER CALL, REJECT, and
END CALL prompts to not be displayed. Level 2 causes the
MAKE CALL prompt and the Level 1 prompts to not be
displayed. Level 2 is selectable only if ORT item xxxii is
enabled.
xliv
EIRP Overdraft
Checking Priority
Secured,
common
This item defines the call priority level where at least one call
must be in progress when considering if an EIRP overdraft is
allowed.
xlv
Analog
Telephone
(APHONE)
Called Terminal
ID Assignment
User,
duplicated
This item provides for the assignment of a three-digit called
terminal identification (CTid) code to each APHONE channel
routing ground-to-air priority 4 calls to the APHONE interface,
based on the called terminal field in the call announcement
signal unit. The CTid assigned can be any decimal value
between --1 and 999. A CTid value of --1 represents no
specific routing.
This item also specifies a CTid assignment type of exclusive
or nonexclusive for each channel. The assignment type
defaults to nonexclusive if no CTid is assigned. An
assignment type of exclusive with no CTid assigned is
undefined and is not selectable. With a CTid assigned, an
assignment type of exclusive inhibits all incoming calls from
being routed to the associated channel unless the call
announcement contains a CTid that matches the assigned
value. An assignment type of nonexclusive allows all
incoming calls to be routed to the associated channel unless
the call announcement contains a CTid that matches the
assigned value of the other channel. Regardless of the
assignment type, an incoming call with a matching CTid is
rejected if the associated channel is unavailable.
Modifications of this item through the APHONE or CMT are
checked for duplication with the other APHONE channel in
the SDU and, in a dual system, with the APHONE channels in
the other SDU.
The primary use of this ORT item is to let incoming facsimile
calls be routed to the channel connected to the facsimile
machine.
xlvi
Cockpit Audio
Level Settings
Secured,
common
This item defines the level settings for the cockpit
microphone, sidetone, and receive audio.
xlvii
HGA Retry
Period (ground
and air)
Secured,
common
This item defines the time interval for ground and airborne
cases after which SATCOM (when logged on through the
LGA) is to make attempts to logon through the HGA. A value
of 0 disables the periodic retry for each case. The time
interval is in integer minutes ranging from 0 to 255.
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Page C--9
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
xlviii
Characteristic
Attributes
Cockpit Channel Secured,
Interface Type for common
Dual
ORT Characteristics (cont)
Description
This item defines the functional mapping of the one to four
potentially available physical SDU cockpit voice channels in a
dual system to the one or two logical cockpit voice channels
(as viewed from the perspective of the ACP and SCDU). It is
used in combination with ORT item vi and system
configuration pins TP13F and TP13J to determine the
number of logical channels and which physical channel(s)
is/are potentially available for each logical channel.
This item is capable of taking on the states of fixed and
shared. Fixed interfacing is interfacing each ACP/SCDU
(logical) channel to one physical channel on one SDU only.
Shared interfacing is interfacing each ACP/SCDU logical
channel to one physical channel on each of the two SDUs.
The fixed or shared interfacing declaration refers to the
functional channel mapping, and not necessarily to the
physical interwiring, e.g., the interwiring can be independent
but the interface can be effectively shared by virtue of
splitting/combining/paralleling within the AMS (as in the
Boeing 777), or the interwiring can be literally paralleled,
forcing the interface type to shared.
In the case of two logical channels, it is assumed the single
value for this item applies to both channels (i.e., both fixed or
both shared). For the case of shared (for one or two logical
channels), it is assumed each logical channel shares the
same numbered physical channel on each SDU.
The state of this item is checked for compatibility with the
state of pins TP13F and TP13J of both SDUs and the state of
ORT item vi of both SDUs.
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Page C--10
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
il
Characteristic
Mastery
Handover
Algorithm
Weighting
Attributes
User,
common
ORT Characteristics (cont)
Description
This item stores the relative weighting factors for each of the
six functional capability items that form the criteria for
determining which system should automatically become the
master in a dual system. Each of the six weighting factors is a
non-negative integer ranging from 0 to 99. Higher factors
indicate more important criteria; however, only the relative
values of the factors is significant. Zero is used to indicate a
capability factor not installed, not used, or is a don’t care. The
functional capability items are as follows:
• CoV -- Cockpit voice (for any number of channels).
• CaV -- Cabin circuit-mode voice/fax/data
(any number of channels, any cabin interface).
• CoL -- Cockpit packet-mode data
(through [C]MU) at low-rate only.
• CoH -- Cockpit packet-mode data
(through [C]MU) at (potentially) high-rate.
• CaL -- Cabin packet-mode data
(through CPDF or CTU) at low rate only.
• CaH -- Cabin packet-mode data (through CPDF or CTU) at
(potentially) high-rate.
CoL and CoH are mutually exclusive, as are CaL and
CaH — i.e., regardless of the weighting factors assigned, no
more than one of the cockpit data (or cabin data) capabilities
can be true at a time.
The primary practical use of this ORT item is for determining
which SDU in a dual system should be the master when the
choice is down to one system which only has voice capability
vs one which only has data capability, or one with only cockpit
services capabilities vs one with only cabin services
capabilities.
Disable/Reenable Secured,
Other SATCOM
common
SCDU Prompts
This item determines if the disable other SATCOM and
re--enable other SATCOM toggling SCDU prompts are
presented or suppressed. The SCDU prompts are usually
suppressed if the optional external manual switch (that
controls the dual system select and disable discretes) is
supplied so there is only one means of performing any
function at a time and the possibility of inadvertently disabling
both systems is avoided.
li
SCDU SATCOM
Subsystem
Prompts
This item defines up to six ISO--5 characters used for the
SCDU main menu SATCOM subsystem selection LSK
prompts. The owner/operator is able to select any ISO--5
characters and any length up to six characters. Example
character strings would be SAT L and SAT R, or MPDS/BGAN > ISDN
1 C--P4 > ISDN > MPDS/BGAN
2 MPDS/BGAN > C--P4 > ISDN
3 MPDS/BGAN > ISDN > C--P4
4 ISDN > C--P4 > MPDS/BGAN
5 ISDN > MPDS/BGAN > C--P4
Ixii
Ongoing HSD
Call EIRP
user,
common
This item defines the minimum level of power that the
SDU reserves for an ongoing Swift64 M--ISDN HSD
call. If the HSU requested EIRP falls below this
reserved EIRP level, then power reserved for the HSU
will freeze at this level even though the actual power
will track the EIRP requested by the HSU. The defined
range of this item is 0.0 to 25.0 dBW.
Ixiii
WSC Manual
Dialing
user,
This item defines parameter options to be passed to
any connected and active Williamsburg SDU
controller(s) (WSCs), for the WSC’s own optional
usage. It has no other direct functionality within the
SDU. It shall be capable of taking on the values
“Disabled” and “Enabled”, and for the latter case, it
specifies the priority level (1 through 4, [for Manual
Dial Enable and Priority for Manual Dial] ) to be used
for such calls.
Ixiv
Minimum HSD
Call EIRP
user,
common
Ixv
HSD Registration user,
Preference
common
common
This item defines the minimum permissible level of
power that the SDU deems adequate for an ongoing
Swift64 M--ISDN HSD call. If the HSU requested EIRP
falls below this level, then the SDU terminates the
call. The defined range of this item is 0.0 to 30.0
dBW.
This item specifies the type of HSD service
(Swift64 or BGAN) which the HSU shall provide by way of the
chosen satellite when in a region of both Swift64 and
BGAN service coverage. The item defines the
registration preference to be either
a) automatic (i.e. BGAN when in BGAN coverage,
otherwise Swift64 if in Swift64 coverage)
b) Swift64 only
c) BGAN only.
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Page C--13
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
Attributes
ORT Characteristics (cont)
ORT Item
Characteristic
Description
Ixvi
Swift64 M--ISDN
LES Preference
Values
user,
common
This item defines automatic log--on preference values
for Swift64 M--ISDN LESs in the range of 0 to 9 for use
by the HSU, where 0 disallows use for automatic log
on and 9 corresponds to most preferred.
Ixvii
Swift64 MPDS
LES Preference
Values
user,
common
This item defines automatic log--on preference values
for Swift64 MPDS LESs in the range of 0 to 9 for use
by the HSU, where 0 disallows use for automatic log--on and
9 corresponds to most preferred.
Ixviii
Ethernet MAC
Address
Assignment
user,
common
This item defines the MAC addresses that will be used
to overwrite the globally unique, IEEE--allocated
addresses associated with the Ethernet chipsets for
HSU port 1 and 2. The defined range for each of the
two addresses is 00--00--00-- 00--00--00 (i.e., retain
chipset value) to FF--FF--FF--FF--FF--FF. If an ORT
upload attempts to set the MAC addresses for both
HSU ports to the same non--zero value, then both
addresses are set to their default values (as
specified in Section 3.3.3.1.4.3.2), the User ORT
Modified Flag is set and the associated range
check failure is declared.
Ixix
PPPoE Access-Concentrator
Name
user,
duplicated
This item defines the Access Concentrator (AC) name,
for use in the HSU’s PADO response to a PADI
received during PPPoE communications. The AC
name is up to 15 characters long.
Names consisting of upper case letters, decimal digits,
hyphens and spaces shall be allowed.
In a dual system, this item specifies the AC name
for each SDU system. If an ORT upload attempts to
set identical AC names for both SDU #1 and SDU #2,
then both names are set to their default values,
the User ORT Modified Flag is set and the
associated range check failure is declared.
lxx
Telnet Server
Access
user,
common
This item defines whether access to the HSU Telnet
client, by way of the HSU’s Ethernet port 1, is Disallowed or
Allowed.
Ixxi
DHCP Server
Access
user,
common
This item defines whether access to the HSU Dynamic
Host Configuration Protocol (DHCP) server, by way of the
HSU’s ethernet port 1, is Disallowed or Allowed.
Ixxii
Telnet IP Address user,
Assignment
duplicated
This item defines the base IP address to be used for
the HSU Telnet server on Ethernet port 1. The defined
range for this item is 0.0.0.0 to 255.255.255.255.
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Page C--14
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
INSERT PAGE 47 OF 53 THRU N OF N FACING PAGE C-15.
Reason:
To change the capitalization of INMARSAT to Inmarsat in the description of ORT Item lxxviii.
The description for Item lxxviii is changed as follows:
Table C-1.
ORT Item
lxxviii
Characteristic
Attributes
ORT Characteristics (cont)
Description
This item defines Psid frequencies that may be used when
attempting to acquire a satellite. The item specifies two
frequencies and associated system table revision number
for a maximum of 10 satellites. The frequencies are
specified as Inmarsat channel numbers, with 0000x
indicating no frequency stored.
23-20-35
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Page 47 of 53
28 Sep 2009
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table C--1.
ORT Item
Characteristic
Attributes
ORT Characteristics (cont)
Description
lxxiii
Telnet Subnet
Mask
Assignment
user,
duplicated
This item defines the subnet mask address to be used
for the HSU Telnet server on Ethernet port 1. The
defined range for this item is 0.0.0.0 to
255.255.255.255. In a dual system, this item
specifies the subnet mask address for each SDU
system.
lxxiv
Telnet Default
Gateway
Assignment
user,
duplicated
This item defines the default gateway address to be
used for the HSU Telnet server on Ethernet port 1. The
defined range for this item must be 0.0.0.0 to
255.255.255.255. In a dual system, this item
specifies the default gateway address for each SDU
system.
Ixxv
DHCP IP
Address
Assignment
user,
common
This item defines the base IP address to be used for
the HSU DHCP server on Ethernet port 1. The defined
range for this item is 0.0.0.0 to 255.255.255.255.
Ixxvi
DHCP IP
Address Pool
Allocation
user,
common
This item defines the number of IP addresses
allocated for use by the HSU DHCP server on Ethernet
port 1. The defined range for this item is 3 to
250.
lxxvii
BGAN PDP
Session
Parameters
user,
common
This item defines the default values to be used in
establishing a BGAN PDP session when no control
parameter information is passed from the user
terminal. The item specifies defaults for the following
parameters: Traffic Class, Maximum Downlink and
Uplink Bit Rates, Guaranteed Downlink and Uplink Bit
Rates. The item defines the traffic class to be
either
a) Conversational
b) Streaming
c) Interactive
d) Background
The defined range of all bit rate parameters is 0
to FFFFx kbit/s.
lxxviii
Psid
Supplementary
Frequencies
user,
common
This item defines Psid frequencies that may be used
when attempting to acquire a satellite. The item
specifies two frequencies and associated system table
revision number for a maximum of 10 satellites. The
frequencies are specified as INMARSAT channel
numbers, with 0000x indicating no frequency stored.
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Page C--15
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
INSERT PAGE 48 OF 53 THRU 51 OF 53 FACING PAGE C-16.
Reason:
To add Items lxxix thru cviii to Table C-1, ORT Characteristics.
Table C-1 is changed to add new data as follows:
Table C-1.
ORT Characteristics (cont)
ORT Item
Characteristic
Attributes
Description
lxxix
DHCP Client
Activated
Access Point
Name
User,
duplicated
User,
common
lxxxi
Telnet User
Name and
Password
User,
duplicated
lxxxii
Port Host
Name
User,
duplicated
lxxxiii
lxxxiv
Reserved
TFTP Software
Upload
Enabled
CHAP/PAP
User Name and
Password
User,
common
User ORT Part
Number
Secured ORT
Part Number
MIB Self-Test
User,
common
Secured,
common
User,
common
User,
duplicated
This item defines whether the DHCP client within the HSDU should be
enabled or disabled on the two HSDU Ethernet ports.
This item defines the Access Point Name (APN) of an external network
that can be accessed by the HSDU. The APN can be up to 40
characters long and can consist of upper case letters, decimal digits
and hyphens.
This item defines the user name and password to be used when
accessing Telnet sessions on the HSDU. The user name and
password can each be up to 15 characters long and consist of upper
case letters, decimal digits, hyphens and spaces. If the user name is
defined as a null string, the HSDU will impose no access restrictions on
a Telnet session.
This item defines the host names for Ethernet ports 1 and 2 for use by
the DHCP client in the HSDU for TCP/IP addressing. Each host name
can be up to 15 characters long and consist of upper case letters,
decimal digits, hyphens, underscores and spaces.
This item defines whether the TFTP server within the HSDU should be
enabled or disabled. If enabled, the upload of an HSDU software image
through Ethernet port 1 will be allowed.
This item defines the user name and password to be used when the IP
router function is enabled within the HSDU and CHAP/PAP
authentication is required. The user name and password can each be
up to 15 characters long and consist of upper case letters, decimal
digits, hyphens and spaces. If the user name is defined as a null string,
the HSDU will impose no access restrictions.
This item defines the 15-character (ISO-5) ARINC-665 User ORT part
number.
This item defines the 15-character (ISO-5) ARINC-665 Secured ORT
part number.
This item defines whether the HSDU can be reset via the SNMP
interface and can be set to either allowed or disallowed.
This item defines the philosophy used by the HSDU for assigning new
Primary contexts to available channel cards. The options available are:
a) Share new Primary contexts between channel cards
b) Fill channel card 1 before moving onto channel card 2 or
c) Fill channel card 2 before moving onto channel card 1.
lxxx
lxxxv
lxxxvi
lxxxvii
lxxxviii
lxxxix
Primary
Context
Loading
User,
duplicated
23-20-35
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Page 48 of 53
28 Sep 2009
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS-4200/7200
TEMPORARY REVISION NO. 23-1
Table C-1.
ORT Item
xcvii
Characteristic
Ciphering
Enabled
Attributes
User,
common
xcviii
Ethernet
Duplex Mode
User,
duplicated
ic
SwiftBroadband
Attachment
Mode
User,
common
HSD Channel
Preemption
Preference
User,
common
ci
LCP
Authentication
Enabled
User,
common
ORT Characteristics (cont)
Description
This item defines whether the data passed over the air should be
encrypted as per the 3G specifications. The value can be Enabled or
Disabled.
This item shall control the half/full duplex mode applicable to both HSU
Ethernet ports. The available options are:
a) Both Ethernet ports operate at half duplex,
b) Ethernet Port 1 operates at full duplex, Ethernet Port 2
operates at half duplex,
c) Ethernet Port 1 operates at half duplex, Ethernet Port operates
at full duplex or
d) Both Ethernet ports operate at full duplex.
This item shall control the mode of attachment the HSU will use when
in SwiftBroadband mode. The available options are:
a) No automatic attachment,
b) Automatic attachment for SwiftBroadband Circuit Switched
service,
c) Automatic attachment for SwiftBroadband Packet Switched
service or
d) Automatic attachment for SwiftBroadband Circuit Switched and
Packet Switched services.
This item defines the preferred HSD Channel to preempt when more
than one HSD channel is among the preemption candidates and the
HSU is in SwiftBroadband mode. The available options are:
a) Any Channel,
b) HSD Channel Card 1,
c) HSD Channel Card 2.
This item defines whether LCP Authentication (using the PAP protocol)
should be Enabled or Disabled.
The HSU shall only utilize the CHAP/PAP Username and Password if
the LCP Authentication Enabled flag indicates ‘Enabled’. If LCP
Authentication is enabled, the CHAP/PAP Username and Password
shall be compared against the Username and Password provided by
the PPPoE client, if they both match, then no authentication
parameters are sent in the PDP context activation request to the
network. If they do not match, the HSU shall pass the Username and
Password parameters provided by the PPPoE client in the PDP context
activation request for authentication with the network.
23-20-35
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MCS-4200/7200
TEMPORARY REVISION NO. 23-1
Table C-1.
ORT Characteristics (cont)
ORT Item
xc
Characteristic
BGAN Packet
Data Threshold
Attributes
User,
common
xci
Satellite
Preferences
User,
common
xcii
Service
Preferences
User,
common
xciii
Satellite
Handover
based on
Service
Preferences
HSD Service
Recovery
Timeout
User,
common
This item defines whether a satellite handover can be initiated due to a
higher preference service being available for selection.
User,
common
xcv
Satellite
Constellation
User,
common
xcvi
IP Header
Compression
User,
common
This item defines the number of minutes to wait before allowing HSDU
services to be available for selection again on a particular satellite after
being temporarily marked as unavailable (e.g. as a result of registration
rejection). The defined range for the timeout is 1 to 30 minutes.
This item contains satellite constellation information which includes the
satellite identity, satellite longitude and satellite service information.
This item can be used to provide data for use in automatic satellite and
service selection.
This item defines whether IP Header Compression of TCP and UDP
headers as per RFC 2507 should be disabled or enabled and the
amount of memory to reserve for use. The range of values are:
xciv
Description
This item defines the values to be used as a data threshold value in
determining if any active PDP context has sufficient data throughput to
deem SwiftBroadband service as being “in use”. This item contains two
values, the number of data packets that defines the threshold, and a
period value in milliseconds in which the designated number of packets
are to be transmitted / received.
This item defines the satellites to be used in the automatic satellite
selection algorithm. A satellite can be marked as either 0 (not
considered for selection) or 1 (considered for selection).
This item defines a preference level associated with a service or
combination of services that the system can provide. The preference
value ranges from 0 to 3, with 3 being the most preferred service(s) for
which to attempt registration and 0 indicating that registration should
not be attempted for the service(s).
0: IP header compression is disabled
1: IP header compression is enabled, with 512 bytes
2: 1024 bytes
3: 2048 bytes
4: 4096 bytes
5: 8192 bytes
6: 16384 bytes
7: 32768 bytes
8: 65536 bytes
9: 131072 bytes
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TEMPORARY REVISION NO. 23-1
Table C-1.
ORT Characteristics (cont)
ORT Item
Characteristic
Attributes
Description
cii
Maximum
SwiftBroadband
Streaming
Bandwidth
User,
common
ciii
PIMBIT Fault
Threshold
User,
common
Reserved.
civ
PIMBIT Fault
Threshold for
Antenna
Beams
User,
common
Reserved.
cv
PIMBIT Data
Invalid
Thresholds
User,
common
Reserved.
cvi
PIMBIT
Antenna Beam
Angles
User,
common
Reserved.
cvii
PIMBIT Sample
Discard Ratio
User,
common
Reserved.
cviii
Aero Satellite
Recovery Timer
User,
common
This item defines the number of minutes to wait before allowing a Aero
service to be available for selection again on a particular satellite after
being temporarily marked as unavailable (e.g. as a result of P-Channel
degradation or failure to acquire a P-Channel or HGA transmit gain
below threshold). The defined range for the timeout is 1 to 30 minutes.
This item defines the maximum streaming bandwidth permitted within
the HSU when using SwiftBroadband service.
The Maximum SwiftBroadband Streaming Bandwidth ORT Item will not
be used by the HSU to deny SwiftBroadband service at the interface
level. It will instead be used as a basis of populating the ARINC 781
MIB Service Availability Related Sub Branch for information purposes.
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX D
CALL EVENTS LOG (CEL)
1. Call Events Log
A. General
(1) A CEL is maintained in non--volatile storage for post--flight analysis of circuit--mode
call statistics. The CEL can store at least 300 events. In a dual system, each SDU
maintains its own CEL for the calls it provides through its own antenna subsystem.
The slave logs its own calls, and the master does not log calls provided by the slave,
even though the master is involved with the establishment of the slave’s calls. Events
and the associated parameters to be stored are listed in Table D--1.
Table D--1.
Event
Call Events Log
Parameters
Air to Ground Call Setup Request
Current Time/Date
Interface (Headset 1 or 2, WH--10 1 or 2, APBX 1 or
2, DPHONE)
Application Reference Number
Call Precedence (Q)
Initial 6 digits of B--Party Address
Credit Card Data Present Flag
Calling Terminal Number
GES Id
Modem Number
Satellite Relative Azimuth and Elevation
Voice Channel Characteristics
RFM Channel Id
Transcoder Number
Call Setup Failure
Current Time/Date
Application Reference Number
Call Precedence (Q)
SLCV and detailed code
GES Id
Ground to Air Call Announcement
Current Time/Date
Application Reference Number
Call Precedence (Q)
GES Id
Called Terminal Number
Modem Number
Transcoder Number
Satellite Relative Azimuth and Elevation
SLCV and detailed code (NULL if not rejected)
Voice Channel Characteristics
RFM Channel Id
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Table D--1.
Event
Call Events Log (cont)
Parameters
Ground to Air Call Answer
Current Time/Date
Application Reference Number
Call Precedence (Q)
Interface (Headset 1 or 2, WH--10 1 or 2, APBX 1 or
2, DPHONE)
GES Id
Call Termination
Current Time/Date
Application Reference Number
Call Precedence (Q)
Satellite Relative Azimuth and Elevation
Return EIRP at end of call
Clearing SLCV and detailed code
GES Id
Highest audio level reported during call
CTU Call Setup Failure
Current Time/Date
Call Reference Number
CTU Event Type
SLCV and Detailed Code
HSD Air to Ground Call Setup Request
HSD channel number
Current Time/Date
Call Reference Number
Service Address (dialed phone number)
Service Variant
Originating Terminal Id
LES Id
Spot Beam Id (package 6.0 and subsequent)
Satellite Relative Azimuth and Elevation
Latitude
Longitude
HSU Interface (package 6.0 and subsequent)
HSD Ground to Air Call Announcement
HSD channel number
Current Time/Date
Call Reference Number
Service Variant
Destination Terminal Id
LES Id
Spot Beam Id (package 6.0 and subsequent)
Satellite Relative Azimuth and Elevation
Latitude
Longitude
HSD Channel Assignment
HSD channel number
Current Time/Date
Call Reference Number
LES Id
Spot Beam Id (package 6.0 and subsequent)
Initial call EIRP
Forward and return channel Id
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MCS--4200/7200 Multi--Channel SATCOM System
Table D--1.
Event
Call Events Log (cont)
Parameters
HSD Call Termination
HSD channel number
Current Time/Date
Call Reference Number
LES Id
Spot Beam Id (package 6.0 and subsequent)
Satellite Relative Azimuth and Elevation
Latitude
Longitude
EIRP at end of call
SLCV and Detailed Termination Code
Carrier to Noise Density at end of call
Unique Word Error Count
BGAN Air to Ground Circuit
HSD channel number
Switched Setup Request
Current Time/Date
Call Reference Number
Radio Network Controller
Spot Beam Id
Service Address (dialed phone number)
Calling Terminal Id
Service Type
HSU Interface
Satellite Relative Azimuth and Elevation
Latitude
Longitude
BGAN Call Termination
HSD channel number
Current Time/Date
Call Reference Number
Radio Network Controller
Spot Beam Id
Clearing SLCV and detailed termination code
Satellite Relative Azimuth and Elevation
Latitude
Longitude
BGAN Ground to Air Circuit
HSD channel number
Switched Setup Request
Current Time/Date
Call Reference Number
Radio Network Controller
Spot Beam Id
Calling Terminal Id
Service Type
HSU Interface
Satellite Relative Azimuth and Elevation
Latitude
Longitude
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2. Commentary
A. Most Significant Digit
(1) The DSLCV may be used to determine the type of circuit--mode service in--use when
a call terminates. The coding for this digit is as follows:
• 0
Not Answered
• 1
Answered, Voice Call
• 2
2400 bps TIF Fax
• 3
4800 bps TIF Fax
• 4
9600 bps TIF Fax (reserved)
• 5
V.21 only TIF Fax
• 6
1200/2400 bps TIF V.22bis “PC” Data
• 7
4800 (reserved)
• 8
9600 (reserved)
• 9
(reserved)
• A (reserved)
• B 9600 bps CN11 Circuit Mode Data
• C Answered ISDN Call
B. SLCV And Detailed Code Definitions
(1) Table D--2 lists the SLCV and detailed code combinations and associated
descriptions.
Table D--2.
SCLV and Detailed Code Descriptions
Description
Code
0006 xBx
CTU, Chan Unacceptable
0010 x00
Gnd User, Normal Clear
0010 x01
Normal Clear from Handset
0010 x02
Normal Clear from MCDU
0010 x03
Normal Clear from ACP Mic
0010 x04
Normal Clear from Cockpit Disc
0010 xBx
CTU, Normal Clear
0012 x81
Incoming Call Not Answered
0012 xBx
CTU, No User Responding
0015 x00
Call Rejected from SCDU
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Table D--2.
SCLV and Detailed Code Descriptions (cont)
Code
Description
0015 xBx
CTU, Call Rejected
001d xBx
CTU, Req Facility Reject
001e xBx
CTU, Respnse to Enquiry
001f xBx
CTU, Unspecified Failure
0029 xBx
CTU, Temporary Failure
002c xBx
CTU, Chan Unavailable
0043 xBx
CTU, Incoming APC Barred
0051 xBx
CTU, Invalid Call Ref
0060 xBx
CTU, Info Elemts Missing
0061 xBx
CTU, Invalid Msg Type
0064 xBx
CTU, Invalid Info Ctnts
0065 xBx
CTU, Inappropriate Msg
0066 xBx
CTU, Protocl Timer Expry
006f xBx
CTU, Unspec Protocol Err
0106 xBx
931, Chan Unacceptable
0110 xBx
931, Normal Clear
0112 xBx
931, No User Responding
0115 xBx
931, Call Rejected
011d xBx
931, Req Facility Reject
011e xBx
931, Respnse to Enquiry
011f xBx
931, Unspecified Failure
0129 xBx
931, Temporary Failure
012c xBx
931, Chan Unavailable
0143 xBx
931, Incoming APC Barred
0151 xBx
931, Invalid Call Ref
0160 xBx
931, Info Elemts Missing
0161 xBx
931, Invalid Msg Type
0164 xBx
931, Invalid Info Ctnts
0165 xBx
931, Inappropriate Msg
0166 xBx
931, Protocl Timer Expry
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MCS--4200/7200 Multi--Channel SATCOM System
Table D--2.
SCLV and Detailed Code Descriptions (cont)
Code
Description
016f xBx
931, Unspec Protocol Err
0206 xBx
CTU, Chan Unacceptable
0210 xBx
CTU, Normal Clear
0212 xBx
CTU, No User Responding
0212 xC0
Timer 301, No User Responding
0215 xBx
CTU, Call Rejected
021C x40
Invalid B--Party Address
021d xBx
CTU, Req Facility Reject
021e xBx
CTU, Respnse to Enquiry
021f xBx
CTU, Unspecified Failure
0229 xBx
CTU, Temporary Failure
022c xBx
CTU, Chan Unavailable
0243 xBx
CTU, Incoming APC Barred
0251 xBx
CTU, Invalid Call Ref
0260 xBx
CTU, Info Elemts Missing
0261 xBx
CTU, Invalid Msg Type
0264 xBx
CTU, Invalid Info Ctnts
0265 xBx
CTU, Inappropriate Msg
0266 xBx
CTU, Protocl Timer Expry
026f xBx
CTU, Unspec Protocol Err
0401 x00
Pub Net, Unassigned Number
0403 x00
Pub Net, No Route to Dest
0411 x00
Pub Net, User Busy
0412 x00
Pub Net, No User Responding
0412 xC0
G-->A Call Not Answered by User
041B x00
Pub Net, Dest Out of Service
041C x00
Pub Net, Invalid Number Format
0422 x00
Pub Net, No Circuit Avail
0426 x00
Pub Net, Network Out of Order
042A x00
Pub Net, Equip Congestion
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Table D--2.
SCLV and Detailed Code Descriptions (cont)
Code
Description
0442 x00
Pub Net, Chan Type not Implnt’d
046f xC0
Pub Net -- Q.931 Error State I1
046f xC1
Pub Net -- Q.931 Error State I3
046f xC2
Pub Net -- Q.931 Error State I4
046f xC3
Pub Net -- Q.931 Error State I6
046f xC4
Pub Net -- Q.931 Error State I7
046f xC5
Pub Net -- Q.931 Error State I9
046f xC6
Pub Net -- Q.931 Error State I10
0501 x00
Priv Net, Unassigned Number
071F x00
Intn’l, Busy Flash (Unspec’d)
1111 x11
Preempt by Higher Priority
1121 xC0
B--Channel Not Available
1131 xC0
Invalid CCD, No Track 2 Data
1132 xC0
Invalid Address/Call’Party Num
1132 xC1
Number not preselected for cockpit
1141 xC0
Dest Out of Service, Chan Abort
1141 xC1
Dest Out of Service, I/F Abort
1141 xC2
Call Rejected, in Released St
1161 xB0
Credit Card Not Supported
1164 x92
Outgoing call -- GES cannot provide requested voice service
1165 xC0
Invalid Bearer Capability
1165 xC1
Invalid Net Specific Facilities
1221 x20
GES Selective Release
1221 x21
No Power to Sustain Call
1221 x22
Satellite Handover
1221 x23
System Logged--Off
1221 x24
Equipment Failure (loss of min--op)
1221 x25
HGA Failed
1221 x26
HGA Deselected
1221 x27
Modem Revoked
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Table D--2.
SCLV and Detailed Code Descriptions (cont)
Code
Description
1221 x28
Transcoder Revoked
1221 x29
This SDU Disabled
1221 x2A
Cross--Talk Bus Failure
1221 x41
Analog Audio Interface revoked from call
1222 x32
Outgoing call -- Insufficient Power for Setup
1222 x33
Outgoing call -- No Modem for Setup
1222 x34
Outgoing call -- No Transcoder for Setup
1222 x35
Not Logged On
1222 x36
Outgoing call -- Cockpit Camp--On Cancel
1222 x37
Outgoing call -- Call Failed to Preempt
1222 x38
Missing Resource for Setup
1222 x39
Incoming call -- Destination I/F Not Wired
1222 x3A
Incoming call -- Internal Equipment Failure
1222 x3B
Incoming call -- External Equipment Failure
1222 x3C
Incoming call -- Invalid DDI Called Term Id
1222 x3D
Incoming call -- No Channel Available
1222 x3E
Incoming call -- Master [other_satcom] Not OK
1222 x3F
Incoming call -- Cannot Reach CTId on Other SATCOM (e.g., XTB failure)
1222 x40
Outgoing call -- No available analog interface
1242 x90
Outgoing Calls Disallowed (ORT item xxvi)
1243 x50
Incoming Public Calls Barred (ORT item xiii)
1251 x61
C’ty Fail (C--Chan not Received)
1251 x63
C’ty Fail (No C--Chan Assignmnt)
1251 x64
C’ty Fail (No Test SU Received)
1251 x65
C’ty Fail (No S4 or S7 SU Rxed)
1251 x66
C’ty Fail (No Ack to Connect)
1251 x67
C--channel Bit Error Rate Degradation (CN59)
1251 x68
C--channel Inhibited, AES ID or ARN mismatch (CN59)
1264 x91
Incoming call -- Voice Channel Type Not Supported
1265 x70
Not Logged On for Voice
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MCS--4200/7200 Multi--Channel SATCOM System
Table D--2.
SCLV and Detailed Code Descriptions (cont)
Code
Description
1271 x80
User Busy, Handset Off--Hook
1321 x00
GES, No Channel Avail
1322 x00
GES, No Channel Unit
1323 x00
GES, Analog Equip Unavail
1324 x00
GES, Digital Equip Unavail
1331 x00
GES, Credit Card Number Rejected
1332 x00
GES, Invalid Address
1341 x00
GES, Dest Out Of Service
1342 x00
GES, AES not Authorized
1351 x00
GES, Continuity Failure
1361 x00
GES, Credit Card Type not supported
1362 x00
GES, Analog Rate not Supp
1363 x00
GES, Digital Rate not Supp
1364 x00
GES, Voice Type not Supp
1365 x00
GES, Service not Supported
1374 x00
Spot Beam Handover
NOTE: indicates the Q.931 Call STATE, for example, “Active” or “Incoming”. “X” indicates any value.
C. HSD ISDN Call SLCV And Detailed Codes
(1) Table D--3 lists the SLCV and associated descriptions for HSD ISDN call
terminations. Table D--4 lists the detailed combinations.
Table D--3.
SLCV Description for HSD ISDN Call Terminations
Description
MES is clearing the call as instructed by the relevant MES terminal
equipment (that is, normal clearing due to MES terminal “on--hook,” etc.).
MES is rejecting the call because the specified MES terminal number is
currently busy, and MES has not been authorized to divert calls which are
addressed to that number.
MES is clearing the fixed--originated call because subsequent to the
acceptance of the call and the signaling of the identity of the mobile terminal
to which the call will actually be routed, that terminal has become busy and
hence cannot be rung.
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SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
MES is clearing the call because appropriate “off-hook” signaling has not
been received from the addressed MES terminal (including any authorized
diversions) within the allowed time limit.
MES is rejecting the call because the specified MES terminal number has
not been installed, and MES has not been authorized to divert calls which
are addressed to that number.
MES is rejecting the call because the specified MES terminal number is
currently out--of--service, and MES has not been authorized to divert calls
which are addressed to that number.
MES is clearing the fixed--originated call because subsequent to the
acceptance of the call and the signalling of the identity of the mobile terminal
to which the call will actually be routed, that terminal has become
out--of--service and hence cannot be rung.
MES is prematurely clearing the mobile--originated call which is in the
process of being established because the MES user has initiated a call from
a terminal which is authorized to automatically preempt an existing
mobile--originated call.
MES is prematurely clearing the mobile--originated call which is in the
process of being established because the MES user has abandoned the call
(by placing the originating terminal “on--hook”).
LES is rejecting the call because the “Service Nature” and/or “Service Type”
and/or “Channel parameter” information received from the MES is invalid
(eg, not currently defined in the SDM, mutually contradictory, or not
applicable to a MES--originated call).
LES is clearing the call because the “service address” information received
from the MES is invalid (ie, less than 2 digits).
LES is clearing the call because the “service address” information received
from the MES is a 2--digit address which is either undefined or which is
currently unavailable at this LES.
LES is clearing the call because the “service address” information received
from the MES contains a country code which is regarded (by this LES) as
invalid.
LES is clearing the call because the “PID” information received from the
MES in the “scrambling vector” message (type 8DH ) is not consistent with
the PID information in the Fixed/MES--Originated (PID) and PID/MES
Registration Tables at the LES as it relates to this call.
(Spot Beam Handover): MES is ready to make the transition from the
current beam to the next beam.
MES is rejecting the call because the MES is not equipped to provide the
specified service.
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TEMPORARY REVISION NO. 23-1
INSERT PAGE 52 OF 53 FACING PAGE D-11.
Reason:
To change the capitalization of INMARSAT to Inmarsat in the Description column of Table D-3.
The description for SLVC 1-3-6-2 is changed as follows:
Table D-3.
ORT Characteristics (cont)
Description
MES is clearing the call because a long-term interruption in reception has
occurred (the definition of a “long-term interruption” depends upon the
service type, See Inmarsat SDM).
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SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
MES is rejecting the call because although it is equipped to provide the
specified service, it is not currently able to do so.
MES is rejecting or clearing the call for a reason which is not covered by any
of the currently defined “Cause” events.
Internal HSDU Termination (pertains to HS--720 only, for packages 6.0 and
subsequent). DSLCV codes are “THA” codes that are only available from
EMS.
MES is clearing the call because a “LES Connect” message (type 8CH ) has
not been received by the MES within the allowed time limit.
MES is clearing the call because the “authentication query” ISU message
(type B4H ) and/or the “authentication query” SSU message (type B5H )
have not been received by the MES within the allowed time limit.
MES is clearing the call because an expected supplementary services SU(s)
has (have) not been received by the MES within the allowed time limit.
MES is clearing the call because the “supplementary services interrogation”
ISU (type B2H ), and/or “subscriber digits” SSU (type AD H ) messages
have not been received by the MES within the allowed time limit.
MES is clearing the call because a “SCPC channel release” SU (type 8A H )
has not been received by the MES, in response to the transmission of a
“notification acknowledge” message (type BAH) during the supplementary
services call diversion information retrieval process, within the allowed time
limit.
(Spot Beam Handover): MES is clearing the call session in the next beam
because the MES did not detect the LESH carrier on the new frequency.
LES is rejecting the call because the “spot--beam ID” information received
from the MES is invalid (ie, ID is not allocated on satellite in use).
LES is clearing the call because the “Scrambling Vector” information
received from the MES is invalid (ie, 0000 H , 6959 H or 7FFF H ).
MES is clearing the call because the Above--decks equipment is about to
“cable unwrap”.
MES is clearing the call because a long--term interruption in reception has
occurred (the definition of a “long--term interruption” depends upon the
service type, See INMARSAT SDM).
MES is clearing the call because the call has lasted more than 700 km in
linear traveled distance (used for Aero Class MES only). Not used by HSU.
MES is clearing the call because it has moved out of spot beam coverage.
Aeronautical Class MES only: MES in “cooperative mode” is clearing the call
because of a preemption request from the master entity. This code is used
by the HSU for any channel release commanded from the SDU when an
HSD call is in progress.
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SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
LES is rejecting the call because an appropriate terrestrial circuit is not
currently available at this specific LES.
LES is rejecting the call because an appropriate channel unit and associated
terrestrial circuit are not currently available at this LES. [This “cause” is only
utilized when there is a permanent “one--to--one” connection between
appropriate channel units and their terrestrial circuits].
(Spot Beam Handover): LES is ready to make the transition from the current
beam to the next beam and is clearing the call session in the current beam
(normal clear).
LES is rejecting the call because an appropriate satellite channel is not
currently available at this specific LES.
LES is rejecting the call because the requested service is not provided by
this specific LES.
LES is rejecting the call because the requested service is temporarily not
available at this specific LES.
LES is rejecting the call because the specified MES is not authorized for any
service at this specific LES.
LES is rejecting the call because the specified MES is not authorized to use
specific requested service via this specific LES.
LES is clearing the call because the data received from the MES in the
“authentication reply” message (type B6H) has been declared “invalid” by
the LES authentication process.
LES is rejecting the call because the specified PID is not authorized for any
service at this specific LES.
LES is rejecting the call because the specified PID is not authorized to use
specific requested service via this specific LES.
LES is clearing the call because the service address received from the MES
is not authorized for the requested priority.
LES is rejecting or clearing the call for a reason which is not covered by any
of the currently defined “Cause” events.
LES is rejecting the call because an appropriate “Channel Assignment”
message has not been received by the LES within the allowed time limit.
LES is clearing the call because the “service address” information has not
been received by the LES within the allowed time limit.
LES is clearing the call because a “Scrambling Vector” message (type 8DH)
has not been received by the LES within the allowed time limit.
LES is clearing the call because neither the “service address” information
nor a “Scrambling Vector” message (type 8DH ) has been received by the
LES within the allowed time limit.
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SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
LES is clearing the call because a “MES Connect” message (type 99H) has
not been received by the LES within the allowed time limit.
LES is clearing the call because a “authentication reply” message (type
B6H) has not been received by the LES within the allowed time limit.
LES is clearing the call because a “notification acknowledge” message (type
BAH ) has not been received by the LES within the allowed time limit.
LES is clearing the call because the request sequence number contained in
the received “notification acknowledge” message (type BA) is not valid (i.e.
either not ‘0’ or not the next value in the sequence).
(Spot Beam Handover): LES is terminating the procedure because it did not
receive a response to the Handover Request from the NCS.
(Spot Beam Handover): LES is clearing the call session in the next beam
because the MES did not indicate that it was ready to make the transition
(possibly because the MES did not receive the Channel Assignment).
LES is rejecting the call because the “Channel Assignment” message
received from the NCS contains inappropriate or conflicting information.
LES is clearing this MES ID and channel number in the busy lists at LES
and NCS because a new call to/from this MES is being set--up (and thus
any previous call to/from this MES must have cleared).
LES is attempting to clear an MES which has sent an SCPC channel
release message but is found still to be transmitting 5.12 seconds later.
LES is rejecting the call because an appropriate channel unit is not currently
available at this specific LES.
LES is clearing the call because of an interruption in reception of the MES
carrier exceeding the allowed time limit.
LES is clearing the call because an appropriate SCPC MES carrier has not
been received by the LES (at the commencement of the call) within the
allowed time limit.
(Spot Beam Handover): LES is clearing the call session in the next beam
because the LES did not detect the MESH carrier on the new frequency.
LES is clearing the call because of a malfunction in the authentication
checking database or in the communications links thereto.
NCS is rejecting the call because the specified MES ID is in the “MES busy”
list at the NCS.
NCS is rejecting the call because the specified MES is busy with an IPDS
call at the NCS.
NCS is rejecting the call because an appropriate SCPC channel is not
currently available.
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MCS--4200/7200 Multi--Channel SATCOM System
SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
NCS is rejecting the call because no SCPC channel exists at the NCS which
matches the contents of the Channel Parameters, Service Nature, Service
Type, MES Category, Spot Beam ID and Priority fields contained in the
Request for Channel Assignment.
NCS is rejecting the call because no SCPC channel is currently available for
the specified leasemarked MES.
NCS is rejecting the call because the MES is outside the spot beam
coverage area.
NCS is rejecting the call because an appropriate SCPC channel is not
currently available and channel pre--emption failed.
NCS is rejecting the call because the requested spot beam indicates failed
spot beam selection (“FF” ) and an appropriate global SCPC channel is not
currently available.
(Spot Beam Handover) NCS is rejecting the Handover Request because an
appropriate SCPC channel is not available in the next beam.
NCS is rejecting the call because the specified MES ID was not found in the
“Forward and Return MES ID” cross--reference table.
NCS is rejecting the call because the specified MES is not authorized for
any service (except for Distress calls) at the NCS.
NCS is rejecting the call because the specified LES is not authorized for the
requested service at the NCS.
NCS is rejecting or clearing the call for a reason which is not covered by any
of the currently defined “Cause” events.
NCS is rejecting the call because the requested service variant is invalid.
NCS is rejecting the call because no message was received from the
specified MES (in reaction to a Call Announcement message) within the
allowed time limit.
NCS is rejecting the call because the specified MES was busy and the MES
pre--emption failed (i.e. no response within the allowed time limit).
NCS is rejecting the call because the Request for Call Announcement or
Request for Channel Assignment contains invalid or inappropriate
information.
NCS is rejecting the call because the specified MES ID is in the “MES busy”
list at the NCS, and is listed as being busy with a call through the same LES
as that now requesting a “call announcement” addressed to that MES.
NCS is rejecting the call because the specified MES is busy with an IPDS
call through the same LES which is requesting the call announcement.
LES is clearing the call because of the receipt of “on--hook” signalling from
the relevant terrestrial circuit (i.e., normal clearing).
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SLCV Description for HSD ISDN Call Terminations (cont)
Table D--3.
Description
LES is clearing the call because the terrestrial called party is engaged
(busy).
LES is clearing the call because appropriate “off--hook” signalling from the
terrestrial called party has not been received by the LES within the allowed
time limit.
LES is clearing the call because of the detection of a failure in the relevant
terrestrial circuit.
The LES is clearing the call because the terrestrial calling party or the
terrestrial network has cleared the call before the “MES connect” message
has been received by the LES.
Table D--4.
Detailed Codes
Description
ID
0x00
Default value
0x01
Channel out of range
0x04
MES time--out
0x05
Incoming call in progress
0x09
Call spacing restriction not fulfilled
0x0B
Timeout on phone number dialing
0x0E
Invalid Ocean Region
0x10
Invalid Telephone Interface type
0x11
The terminal id already in use
0x22
Min--op not achieved
0x24
HSU equipment failure
0x30
Cooperative Preempt: High Priority Call
0x31
Cooperative Preempt: Ocean Region Handover
0x32
Cooperative Preempt: System Failure
0x33
Cooperative Preempt: No Power Available
0x34
Cooperative Preempt: Not Logged On
0x35
Cooperative Preempt: GNSS Frequency Check Error
0x36
Cooperative Preempt: Spare
0x37
Cooperative Preempt: Invalid Parameter
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Table D--4.
Detailed Codes (cont)
ID
Description
0x40
Ruthless Preempt: High Priority Call
0x41
Ruthless Preempt: Ocean Region Handover
0x42
Ruthless Preempt: System Failure
0x43
Ruthless Preempt: No Power Available
0x44
Ruthless Preempt: Not Logged On
0x45
Ruthless Preempt: GNSS Frequency Check Error
0x46
Ruthless Preempt: Spare
0x47
Ruthless Preempt: Invalid Parameter
0x50
EIRP Request Reject: High Priority Call
0x51
EIRP Request Reject: Ocean Region Handover
0x52
EIRP Request Reject: System Failure
0x53
EIRP Request Reject: No Power Available
0x54
EIRP Request Reject: Not Logged On
0x55
Power Not Available (prior to Package 6.0)
0x55
EIRP Request Reject: GNSS Frequency Check Error (Package 6.0 and subsequent)
0x56
EIRP Request Reject: Spare
0x57
EIRP Request Reject: Invalid Parameter
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX E
MESSAGING
1. PPPoE Messaging
A. General
(1) The following subsections define the format and services for the PPPoE discovery
packets as defined in RFC 2516.
B. PPPoE Active Discovery Offer (PADO)
(1) The HSU will respond to PPPoE Active Discovery Initiation (PADI) packets in
accordance with RFC 2516. If the requested service in not available, the HSU will not
provide a PADO response.
(2) The HSU will support service names of length less than or equal to 64 characters.
The conditions for the PADO response and the PADO content are as specified in
Table E--1.
Table E--1.
PADI Service Name
PADO Services
PADO Response
Controlling Condition
No service name tag
Null terminated, or PacketData, or
Swift64
If all services are available or if
SwiftBroadband PS services are
available or if MPDS services are
available. This PADI may be used
as a status poll from a server.
PacketData
PacketData
SwiftBroadband PS services or
MPDS services are available on at
least one channel.
BGAN
BGAN
SwiftBroadband PS services
available on at least one channel.
BGAN--1
BGAN--1
SwiftBroadband PS services
available on Channel Card 1.
BGAN--2
BGAN--2
SwiftBroadband CS and PS
services available on Channel
Card 2.
MPDS
MPDS
MPDS service available on at
least one channel.
MPDS--1
MPDS--1
MPDS service available on at
least on channel of Channel Card
1 (HSU channel 1 or 2).
MPDS--2
MPDS--2
MPDS service available on at
least on channel of Channel Card
2 (HSU channel 3 or 4).
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Table E--1.
PADI Service Name
PADO Services (cont)
PADO Response
Controlling Condition
MPDS--1A
MPDS--1A
MPDS service available on HSU
Channel 1.
MPDS--1B
MPDS--1B
MPDS service available on HSU
Channel 2.
MPDS--2A
MPDS--2A
MPDS service available on HSU
Channel 3.
MPDS--2B
MPDS--2B
MPDS service available on HSU
Channel 4.
MPDS--C1
MPDS--C1
MPDS service is available on HSU
Channel 1.
MPDS--C2
MPDS--C2
MPDS service is available on HSU
Channel 2.
MPDS--C3
MPDS--C3
MPDS service is available on HSU
Channel 3.
MPDS--C4
MPDS--C4
MPDS service is available on HSU
Channel 4.
123
123
MPDS service available on at
least one channel.
28#
28#
M--ISDN service is available on at
least one channel.
Numeric digits (See below)
Numeric digits (See below)
SwiftBroadband CS or M--ISDN
service available on at least one
channel.
(3) The PADI response to a series of numeric digits is detailed in the following:
(a) Definitions:
• “Dialed” digits are defined as the set { 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, *}
• “Dial Termination” characters are defined as the set { # (octothorp, ASCII 23x),
: (colon, ASCII 3Ax) }
• “Unrecognized” characters are defined as the rest of the ASCII character set.
• “Filtered Service Name” is the service--name with unrecognized characters
removed, stopping at (but not including) the first dial termination character, if
any.
(b) If the PADI service name contains up to the first dial termination character, no
unrecognized characters, and consists of two (2) or more dialed digits, and if
SwiftBroadband CS or Swift64 M--ISDN service is available on a channel, the
HSU will respond with a PADO echoing the service name.
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(c) If the PADI filtered service name consists of seven (7) or more dialed digits, and
if SwiftBroadband CS or Swift64 M--ISDN service is available on a channel, the
HSU will respond with a PADO echoing the service name.
(d) If the PADI service name consists of the specific string “123”, and if MPDS
service is available on any available channel, the HSU will respond with a PADO
echoing the service name.
C. PPPoE Active Discovery Request (PADR)
(1) The HSU will respond to PPPoE Active Discovery Request (PADR) packets in
accordance with RFC 2516. If the requested service in not available, the HSU will not
initiate a PPP session and will send a PPPoE active discovery session confirmation
(PADS) packet with a service--name error tag.
(2) The HSU will support service names of length less than or equal to 64 characters.
(3) The HSU response to the PADR packet is as specified in Table E--2.
Table E--2.
PADR Service
Name
PADR Services
HSU response
No service name
tag
If SwiftBroadband services are available, a PS session is initiated using the PDP
parameters provided by the SDU. If SwiftBroadband services are not available and
MPDS services are available, an MPDS session will be initiated.
PacketData
If SwiftBroadband services are available, a PS session is initiated using the PDP
parameters provided by the SDU. If SwiftBroadband services are not available and
MPDS services are available, an MPDS session will be initiated.
BGAN
A SwiftBroadband PS session is initiated on an available channel card.
BGAN--1
A SwiftBroadband PS session is initiated on Channel Card 1.
BGAN--2
A SwiftBroadband PS session is initiated on Channel Card 2.
MPDS
An MPDS session is initiated on an available channel.
MPDS --1
An MPDS session is initiated on Channel Card 1 (HSU channel 1 or 2).
MPDS --2
An MPDS session is initiated on Channel Card 2 (HSU channel 3 or 4).
MPDS--1A
MPDS session is initiated on HSU Channel 1.
MPDS--1B
MPDS session is initiated on HSU Channel 2.
MPDS--2A
MPDS session is initiated on HSU Channel 3.
MPDS--2B
MPDS session is initiated on HSU Channel 4.
MPDS--C1
MPDS session is initiated on HSU Channel 1.
MPDS--C2
MPDS session is initiated on HSU Channel 2.
MPDS--C3
MPDS session is initiated on HSU Channel 3.
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Table E--2.
PADR Service
Name
PADR Services (cont)
HSU response
MPDS--C4
MPDS session is initiated on HSU Channel 4.
123
MPDS session is initiated on any available channel.
28#
M--ISDN 64k UDI session initiated to called party number “28” on any available
channel.
Numeric digits
(See below)
If SwiftBroadband services are available, a CS session is initiated on any available
channel to the called party number defined below. If SwiftBroadband services are not
available and M--ISDN service is available, a 64k UDI session is initiated on any
available channel to the called party number defined below.
(4) The HSU will determine the called party number from the PADR service name as
detailed in the following:
(a) Definitions:
• “Dialed” digits are defined as the set { 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, *}
• “Dial Termination” characters are defined as the set { # (octothorp, ASCII 23x),
: (colon, ASCII 3Ax) }
• “Unrecognized” characters are defined as the rest of the ASCII character set.
• “Filtered Service Name” is the service--name with unrecognized characters
removed, stopping at (but not including) the first dial termination character, if
any.
(b) If the PADR service name contains up to the first dial termination character, no
unrecognized characters, and consists of two (2) or more “dialed” digits, and if
SwiftBroadband CS service is available, the HSU will initiate a SwiftBroadband
CS session on an available channel using the service name as the called party
number.
(c) If the PADR service name contains up to the first dial termination character, no
unrecognized characters, and consists of two (2) or more “dialed” digits, and
SwiftBroadband CS service is not available, and Swift64 M--ISDN is available,
the HSU will initiate a M--ISDN 64k UDI session on an available channel using
the service name as the called party number.
(d) If the PADR filtered service name contains up to seven (7) or more “dialed” digits,
and if SwiftBroadband CS service is available, the HSU will initiate a
SwiftBroadband CS session on an available channel using the filtered service
name as the called party number.
(e) If the PADR filtered service name contains up to seven (7) or more “dialed” digits,
and SwiftBroadband CS service is not available, and Swift64 M--ISDN is
available, the HSU will initiate an M--ISDN 64k UDI session on an available
channel using the filtered service name as the called party number.
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(f)
If the PADR service name consists of the specific string “123”, and if MPDS
service is available on any channel, the HSU will initiate an MPDS session on an
available channel.
D. PPPoE Active Discovery Session--Confirmation (PADS)
(1) The HSU will provide PPPoE Active Discovery Session--Confirmation (PADS) packets
in response to PADR packets in accordance with RFC 2516.
(2) If the requested service in not available, the HSU will not initiate a PPP session and
will send a PPPoE active discovery session confirmation (PADS) packet with a
service--name error tag as specified in Table E--3.
(3) The HSU may provide a PADS response prior to the establishment of the
over--the--satellite call connection.
Table E--3.
Service Name Error
PADR Service Name
Service--Name Error Tag
No Service--Name tag
Missing Service--Name
No Service--Name tag
Default service disabled
(and default service is disabled by a HSU
configuration item)
Service--Name not recognized
Unrecognized service
(not from set of Table E--2)
Requested Service--Name is disabled or not
available
Service disabled or unavailable
Requested Service--Name became unavailable after
PADR received, but before PPP session established
Unable to reserve the channel
E.
PPPoE Active Discovery Termination (PADT)
(1) The HSU will provide a PPPoE Active Discovery Termination (PADT) packet in
response to termination of the PPPoE session.
(2) The PPPoE session may be terminated by the HSU or by a PADT from the host.
(3) The HSU will send periodic Echo--Request packets to the host to assess continued
connectivity.
(4) The HSU will generate a Generic Error tag upon termination of every session,
including those that terminate normally. The Generic--Error tag is of the following
format:
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(a) SLCV – nnnn/dddd: SLCV_cause_string [detailed_cause_string] Where:
• nnnn is the Inmarsat SLCV termination code as defined in Table E--4.
• dddd is the detailed cause code defined in Table E--4.
• SLCV_cause_string is the (modified) Inmarsat standard cause code
wording defined in Table E--4.
• detailed_cause_string is extended cause description as defined in
Table E--4.
(5) The HSU will generate an AC--System--Error tag upon termination of every session,
including those that terminate normally. The AC--System--Error tag is as defined
below.
(a) If the PPPoE session was a Swift64 64k UDI session, the AC--System--Error tag
will be of the following format:
Q850 – qqq: Q.850_string Where:
• qqq is the ISDN Q.850 cause code defined in Table E--5.
• Q.850_string is the Q.850 cause string defined in Table E--5.
(b) If the PPPoE session was a Swift64 MPDS session, the AC--System--Error tag
will be of the following format:
MPDS – mmm: +WQ_cause_string defined in Table E--6. Where:
• qqq is the MPDS AT +WQ cause number defined in Table E--6.
• +WQ_cause_string is the MPDS AT +WQ cause string defined in
Table E--6.
(c) If the PPPoE session was a SwiftBroadband PS session, the AC--System--Error
tag will be of the following format:
BGAN – bbb: TBD Where:
• bbb and TBD are not specified.
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings
SLCV cause string
1001
0000
call cleared by MES terminal
1011
0000
call failed, MES terminal busy
1012
0000
call cleared, MES terminal
busy
1021
0000
call failed, MES time--out (no
answer)
1081
0000
call failed, MES terminal not
installed
Detailed cause string
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Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
1091
0000
call failed, MES terminal
out--of--service
1092
0000
call cleared, MES terminal
out--of--service
1141
0000
MES preempted clear by
higher priority call
1142
0000
MES preempted fixed call by
higher priority call
1143
0000
offered call cleared,
pre--empted at MES
1144
0000
call cleared, MES initiated
preemption
1145
0000
attempted call cleared,
pre--empted at MES
1146
0000
attempted call abandoned by
MES terminal
1191
0000
MES outside spot beam
11A0
0000
call cleared, credit card not
accepted
11D1
0000
call failed, LES service call
type Incorrect
11D2
0000
call failed, insufficient digits in
service address
11D3
0000
call failed, invalid service
address
11D4
0000
call cleared, credit card data
information invalid
11D5
0000
call cleared, invalid country
code
11D6
0000
call cleared, PID information is
not consistent
11D7
0000
call rejected, invalid service for
pri. 1 or 2 call
11D8
0000
call cleared, dialed number not
2 or 3 digits for pri. 1 or 2 call
11E0
0000
call cleared, invalid credit card
PIN at this LES
Detailed cause string
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Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
Comments
11E1
0000
call cleared, too many invalid
credit card call attempts
1202
0000
handover, MES ready
1262
0000
MES distress timeout
1281
0000
call failed, MES cannot accept
1291
0000
call failed, MES cannot accept
at present
1291
0034
call failed, MES cannot accept Call cleared, SDU not logged
at present
On
Cooperative Preempt:
Not Logged On
1291
0035
call failed, MES cannot accept Call cleared, GNSS frequency
at present
check error
Cooperative Preempt:
GNSS Frequency
Check Error
1291
0044
call failed, MES cannot accept Call cleared, SDU not logged
at present
On
Ruthless Preempt:
Not Logged On
1291
0045
call failed, MES cannot accept Ruthless Preempt: GNSS
at present
Frequency Check Error
Call cleared, GNSS
frequency check error
1291
0054
call failed, MES cannot accept EIRP Request rejected due to: Call rejected, SDU not
at present
Not Logged On
logged On
1291
0055
call failed, MES cannot accept Call rejected, GNSS
at present
frequency check error
12B1
0000
call cleared by MES for
unspecified reason
12B1
0024
call cleared by MES for
unspecified reason
HSU Equipment Failure
12B1
0032
call cleared by MES for
unspecified reason
Call cleared, SDU reporting
system failure
Cooperative Preempt:
System Failure
12B1
0036
call cleared by MES for
unspecified reason
Call cleared, pre--empted by
SDU for undeclared reason
Cooperative Preempt:
Spare
12B1
0037
call cleared by MES for
unspecified reason
Call cleared, pre--empted by
SDU for invalid parameter
Cooperative Preempt:
Invalid Parameter
12B1
0042
call cleared by MES for
unspecified reason
Call cleared, SDU reporting
system failure
Ruthless Preempt:
System Failure
12B1
0046
call cleared by MES for
unspecified reason
Call cleared, pre--empted by
SDU for undeclared reason
Ruthless Preempt:
Spare
12B1
0047
call cleared by MES for
unspecified reason
Call cleared, pre--empted by
SDU for invalid parameter
Ruthless Preempt:
Invalid Parameter
EIRP Request
rejected due to:
GNSS Frequency
Check Error
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Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
Comments
12B1
0052
call cleared by MES for
unspecified reason
Call rejected, SDU reporting
system failure
EIRP Request
rejected due to:
System Failure
12B1
0056
call cleared by MES for
unspecified reason
Call rejected, pre--empted by
SDU for undeclared reason
EIRP Request
rejected due to: Spare
12B1
0057
call cleared by MES for
unspecified reason
Call rejected, pre--empted by
SDU for invalid parameter
EIRP Request
rejected due to:
Invalid Parameter
12C2
0000
call cleared, no credit card
valid message received
12C3
0000
call failed, MES time--out (no
terrestrial answer)
12C4
0000
call cleared, authentication
query not received
12C5
0000
call cleared, MES missing sup
service SU
12C6
0000
call cleared, MES missing sup
service 2 SU
12C7
0000
call cleared, MES missing
SCPC channel release SU
sup service
12C8
0000
handover failed, LES not
detected
12D1
0000
call failed, spot beam data
invalid
12D2
0000
call failed, invalid scrambling
vector
1351
0000
call cleared, insufficient free
memory
1361
0000
call cleared by MES cable
unwrap
1362
0000
call cleared, long interruption
in reception at MES
1363
0000
MES secondary clear due to
repoint OR
1363
0031
MES secondary clear due to
repoint OR
Call cleared, SDU re--pointing
antenna to different Ocean
Region
Cooperative Preempt:
Ocean Region
Handover
23--20--35
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Page E--9
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
Comments
1363
0041
MES secondary clear due to
repoint OR
Call cleared, SDU re--pointing
antenna to different Ocean
Region
Ruthless Preempt:
Ocean Region
Handover
1363
0051
MES secondary clear due to
repoint OR
Call rejected, SDU re--pointing EIRP Request
antenna to different Ocean
rejected due to:
Region
Ocean Region
Handover
1391
0000
call cleared, traveled distance
exceeds 700km
1392
0000
call cleared, spot beam
transition
1393
0000
call cleared, cooperative mode
1393
0030
call cleared, cooperative mode Call cleared, pre--empted by
higher priority call
Cooperative Preempt:
High Priority Call
1393
0033
call cleared, cooperative mode Call cleared, no power
available from SDU
Cooperative Preempt:
No Power Available
1393
0040
call cleared, cooperative mode Call cleared, pre--empted by
higher priority call
Ruthless Preempt:
High Priority Call
1393
0043
call cleared, cooperative mode Call cleared, no power
available from SDU
Ruthless Preempt: No
Power Available
1393
0044
call cleared, cooperative mode Channel cleared, SDU not
logged on
Ruthless Preempt:
Not Logged On
1393
0050
call cleared, cooperative mode Call rejected, pre--empted by
higher priority call
EIRP Request
rejected due to: High
Priority Call
1393
0053
call cleared, cooperative mode Call rejected, no power
available from SDU
EIRP Request
rejected due to: No
Power Available
1451
0000
call failed, terrestrial circuits
congested
1452
0000
call failed, LES congested (no
channel and no circuit)
1502
0000
spotbeam handover, LES
ready, normal clear
1551
0000
call failed, LES congested (no
channel)
1581
0000
call failed, service not
provided at this LES
23--20--35
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Page E--10
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
1591
0000
call failed, service temporarily
not available at this LES
1592
0000
call cleared, credit card type
not supported
15A1
0000
call failed, MES not authorised
at this LES
15A2
0000
call failed, service not
authorised at this LES
15A3
0000
call cleared, credit card not
authorised
15A4
0000
call cleared, authentication
reply invalid
15A5
0000
call failed, PID not authorised
for any service
15A6
0000
call failed, PID not authorised
for requested service
15B1
0000
call cleared by LES for
unspecified reason
15C1
0000
call failed, no channel
assignment from LES
15C2
0000
call failed, LES time--out (no
service address)
15C3
0000
call failed, LES time--out (no
scrambling vector)
15C4
0000
call failed, no service address
and no scrambling vector
15C5
0000
call cleared, incomplete credit
card data information
15C7
0000
call failed, LES time--out (no
MES connect)
15C9
0000
call cleared, no authentication
reply
15CA
0000
call cleared, notification ack
not received
15CB
0000
call cleared, invalid sequence
number in notification ack
15CC
0000
handover failed, no response
to request
Detailed cause string
23--20--35
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Page E--11
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
15CD
0000
handover failed, MES not
ready
15D1
0000
call failed, LES time--out
(invalid assignment)
15D2
0000
LES MES already busy
15E1
0000
call cleared but MES still
transmitting (FAULT)
1651
0000
call failed, LES congested (no
channel unit)
1661
0000
call failed, long interruption in
reception at LES
1662
0000
LES long term blockage of
SCPC MES
16C2
0000
LES missing MES SCPC
16C3
0000
handover failed, MES not
detected
1790
0000
call cleared, failure credit card
validation process
1791
0000
call cleared, failure
authentication process
1811
0000
NCS MES ID busy
1812
0000
NCS MES ID busy MPDS
1813
0000
Call waiting request rejected,
MES not accepted call
1814
0000
Call waiting request rejected,
RLES shows MES busy
1841
0000
call cleared, NCS initiated
preemption for incoming pri.1
call
1842
0000
call cleared, NCS initiated
preemption for incoming pri.2
call
1843
0000
call cleared, NCS initiated
preemption for incoming pri.3
call
1844
0000
call cleared, NCS initiated
preemption
Detailed cause string
23--20--35
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Comments
Page E--12
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
1851
0000
call failed, satellite congestion
NCS reject no SCPC available
1852
0000
call failed, satellite congestion
NCS reject SCPC does not
match request
1853
0000
call failed, lease channel
congestion
1854
0000
call failed, MES outside spot
beam coverage area
1855
0000
call rejected, preemption
failed, no channel available
1856
0000
call rejected, spot beam
selection failed
1857
0000
handover failed, channel not
available
185A
0000
NCS Reject Lease--marked
MES ---- No Matching SCPC
channel
18A1
0000
NCS MES ID not found
18A2
0000
call failed, MES not authorised
18A3
0000
call failed, LES not authorised
18B1
0000
call failed by NCS for
unspecified reason
18B2
0000
call rejected, invalid service
requested
18C1
0000
NCS MES burst missing
18C3
0000
NCS MES busy preemption
failed
18D1
0000
call failed, invalid call request
18E1
0000
NCS MES busy already
18E2
0000
NCS MES busy already
MPDS
1D61
0000
Call wait failed, fixed line hung
up
1F01
0000
call cleared by terrestrial
circuit
Detailed cause string
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Page E--13
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
1F11
0000
call failed, terrestrial party
busy
1F21
0000
call failed, LES time--out (no
answer)
1F61
0000
call failed, terrestrial circuit
failure
1F62
0000
call failed, early clear by
terrestrial circuit
0000
0000
MPDS channel cleared
0000
0064
MPDS channel cleared
MPDS Port error code 100
401
0000
01F4
MPDS channel cleared
Unknown Error 500
0000
01F5
MPDS channel cleared
LES Access Code does not
support MPDS
0000
01F6
MPDS channel cleared
Network does not recognise
Mobile ID
0000
01F7
MPDS channel cleared
Network does not recognise
Sim Card
0000
01F8
MPDS channel cleared
Authentication Failed to
Complete
0000
01F9
MPDS channel cleared
Authentication Failure
0000
01FA
MPDS channel cleared
Authorisation Failure
0000
01FB
MPDS channel cleared
Authorisation Failure -- Mobile
Barred
0000
01FC
MPDS channel cleared
Authorisation Failure -- Mobile
Barred on this LES Access
Code
0000
01FD
MPDS channel cleared
Authorisation Failure -- SIM
Card Barred on this LES
Access Code
0000
01FE
MPDS channel cleared
Authorisation Failure -Temporarily Unable to Accept
Credit Cards
0000
01FF
MPDS channel cleared
Authorisation Failure -- Unable
to Accept Credit Cards
Comments
No Inmarsat SLCV for
termination of MPDS
session
23--20--35
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Page E--14
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
0000
0200
MPDS channel cleared
Authorisation Failure -- Credit
Card Refused
0000
0201
MPDS channel cleared
Authorisation Failure -- This
Service not Allowed
0000
0202
MPDS channel cleared
Authorisation Failure -- Service
Option(s) not Allowed
0000
0203
MPDS channel cleared
Authorisation Failure -- QoS
not Allowed
0000
0204
MPDS channel cleared
Authorisation Failure -Unsupported Service
Option(s)
0000
0205
MPDS channel cleared
QoS Option(s) Unsupported
By Mobile
0000
0206
MPDS channel cleared
QoS Option(s) Unsupported
By Network
0000
0207
MPDS channel cleared
Satellite Network Congestion
0000
0208
MPDS channel cleared
Satellite Network Unavailable
0000
0209
MPDS channel cleared
Service Congestion
0000
020A
MPDS channel cleared
Service Unavailable
0000
020B
MPDS channel cleared
Terrestrial Network
Congestion
0000
020C
MPDS channel cleared
Terrestrial Network
Unavailable
0000
020D
MPDS channel cleared
Terrestrial Network Destination
-- Busy
0000
020E
MPDS channel cleared
Terrestrial Network Destination
-- No Answer
0000
020F
MPDS channel cleared
Terrestrial Network Destination
-- Unavailable
0000
0210
MPDS channel cleared
Terrestrial Network Destination
-- No Carrier
0000
0211
MPDS channel cleared
Service Timed Out
0000
0212
MPDS channel cleared
Terminated by Network
Operator
0000
0213
MPDS channel cleared
Insufficient Resources at
Mobile
0000
0214
MPDS channel cleared
Mobile Failure
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Comments
Page E--15
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
0000
0215
MPDS channel cleared
Mobile -- Connection to DTE
Lost
0000
0216
MPDS channel cleared
Mobile -- Unrecoverable DTE
Protocol Error
0000
0217
MPDS channel cleared
Mobile Reset
0000
0218
MPDS channel cleared
User Cancellation of
Connection Establishment
0000
0258
MPDS channel cleared
Unable to Find Satellite
Access Node
0000
0259
MPDS channel cleared
Unable to Establish
Communication with Satellite
Access Node
0000
025A
MPDS channel cleared
Link with Satellite Access
Node Lost
0000
02BC
MPDS channel cleared
Reason Unspecified
0000
02BD
MPDS channel cleared
L3 Release
0000
02BE
MPDS channel cleared
L3 Deregister
0000
02BF
MPDS channel cleared
L3 Reject
0000
02CC
MPDS channel cleared
SAN Idle Timer Expiry
0000
02CD
MPDS channel cleared
MAN Idle Timer Expiry
0000
02CE
MPDS channel cleared
SAN Connect Timer
0000
02CF
MPDS channel cleared
SAN Modify Timer
0000
02D0
MPDS channel cleared
SAN Handover Timer
0000
02D1
MPDS channel cleared
SAN Connection Timer
0000
02D2
MPDS channel cleared
MAN Connection Timer
0000
02DC
MPDS channel cleared
Insufficient operating system
resources at MAN
0000
02DD
MPDS channel cleared
Insufficient memory at MAN
0000
02EC
MPDS channel cleared
Invalid L3 Call Ref in Establish
SDU
0000
02ED
MPDS channel cleared
Invalid L3 Call Ref in Modify
SDU
0000
02FC
MPDS channel cleared
Unsupported MPDS MAC
version
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Page E--16
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
0000
02FD
MPDS channel cleared
Invalid Bearer Connection
type in Establish SDU
0000
02FE
MPDS channel cleared
Invalid Bearer Control type in
Establish SDU
0000
02FF
MPDS channel cleared
Invalid Bearer Connection ID
in Establish SDU
0000
0300
MPDS channel cleared
Invalid Bearer Connection
type in Modify SDU
0000
0301
MPDS channel cleared
Invalid Bearer Control type in
Modify SDU
0000
0302
MPDS channel cleared
Invalid Bearer Connection ID
in Modify SDU
0000
0303
MPDS channel cleared
Invalid Handover SDU
0000
0304
MPDS channel cleared
Invalid SDU type
0000
0305
MPDS channel cleared
SDU Incorrectly Formatted
0000
030C
MPDS channel cleared
Connection sub--layer protocol
failure (MAN specific
signaling)
0000
030D
MPDS channel cleared
Connection sub--layer protocol
failure (HDLC signaling)
0000
031C
MPDS channel cleared
Control sub--layer protocol
failure
0000
032C
MPDS channel cleared
Channel Unit failure
0000
032D
MPDS channel cleared
Hardware failure
0000
032E
MPDS channel cleared
MAN not responding to
frequency corrections
0000
032F
MPDS channel cleared
MAN not responding to power
corrections
0000
0330
MPDS channel cleared
MAN not responding to timing
corrections
0000
033C
MPDS channel cleared
Internal SAN failure
0000
033D
MPDS channel cleared
SAN Shutting Down
0000
034C
MPDS channel cleared
Bearer Control -- No satellite
link
0000
034D
MPDS channel cleared
Bearer Control -- No suitable
contention slot
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Page E--17
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--4.
SLCV
dddd
SLCV Cause Codes and Strings (cont)
SLCV cause string
Detailed cause string
0000
034E
MPDS channel cleared
Bearer Control -- Status
Acknowledgement failure
0000
034F
MPDS channel cleared
Bearer Control -- Incorrect
SAN ID
0000
035C
MPDS channel cleared
No such MAN
0000
035D
MPDS channel cleared
Invalid L3 Call Reference
Table E--5.
Comments
Q.850 Cause Codes and Strings
Q.850 Value
(qqq)
Q8.50 string
Unallocated number
No route to specified transit network
No route to destination
Send special information tone
Misdialed trunk prefix
Channel unacceptable
Call awarded and being delivered in an established channel
Preemption
Preemption -- circuit reserved for reuse
10
Normal call clearing
16
Normal call clearing
17
User busy
18
No user responding
19
No answer from user
20
Subscriber absent
21
Call rejected
22
Number changed
26
Non--selected user clearing
27
Destination out of order
28
Invalid number format -- address incomplete
29
Facility rejected
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Page E--18
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--5.
Q.850 Cause Codes and Strings (cont)
Q.850 Value
(qqq)
Q8.50 string
30
Response to a status enquiry
31
Normal, unspecified
34
No circuit/channel available
38
Network out of order
39
Permanent frame mode connection out--of--service
40
Permanent frame mode connection operational
41
Temporary failure
42
Switching equipment congestion
43
Access information discarded
44
Request channel not available
46
Precedence call blocked
47
Resource not available
49
Quality of service unavailable
50
Requested facility not subscribed
52
Outgoing calls barred
53
Outgoing calls barred within CUG
54
Incoming calls barred
55
Incoming calls barred within CUG
57
Bearer capability not authorized
58
Bearer capability not presently available
62
Inconsistency in designated outgoing access information and subscriber class
63
Service or option not available
65
Bearer capability not implemented
66
Channel type not implemented
69
Request facility not implemented
70
Only restricted digital information bearer capability is available
79
Service or option not implemented, unspecified
81
Invalid call reference value
82
Identified channel does not exist
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Page E--19
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--5.
Q.850 Cause Codes and Strings (cont)
Q.850 Value
(qqq)
Q8.50 string
83
Suspended call exists, but call identity does not
84
Call identity in use
85
No call suspended
86
Call with the specified call identity is cleared
87
User not a member of CUG
88
Incompatible destination
90
Non--existent CUG
91
Invalid transit network selection
95
Invalid message, unspecified
96
Mandatory information element is missing
97
Message type non--existent or not implemented
98
Message not compatible with call state or message type non--existent
99
Information element non--existent or not implemented
100
Invalid information element contents
101
Message not compatible with call state
102
Recovery on timer expiry
103
Parameter non--existent or not implemented -- passed on
110
Message with unrecognized parameter, discarded
111
Protocol error, unspecified
127
Internetworking, unspecified
Table E--6.
MPDS +WQ Cause Codes and Strings
+WQ cause code string
mmm
100
MPDS Port error code 100 401
500
Unknown Error 500
501
LES Access Code does not support MPDS
502
Network does not recognize Mobile ID
503
Network does not recognize Sim Card
504
Authentication Failed to Complete
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Page E--20
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--6.
MPDS +WQ Cause Codes and Strings (cont)
mmm
+WQ cause code string
505
Authentication Failure
506
Authorization Failure
507
Authorization Failure -- Mobile Barred
508
Authorization Failure -- Mobile Barred on this LES Access Code
509
Authorization Failure -- SIM Card Barred on this LES Access Code
510
Authorization Failure -- Temporarily Unable to Accept Credit Cards
511
Authorization Failure -- Unable to Accept Credit Cards
512
Authorization Failure -- Credit Card Refused
513
Authorization Failure -- This Service not Allowed
514
Authorization Failure -- Service Option(s) not Allowed
515
Authorization Failure -- QoS not Allowed
516
Authorization Failure -- Unsupported Service Option(s)
517
QoS Option(s) Unsupported By Mobile
518
QoS Option(s) Unsupported By Network
519
Satellite Network Congestion
520
Satellite Network Unavailable
521
Service Congestion
522
Service Unavailable
523
Terrestrial Network Congestion
524
Terrestrial Network Unavailable
525
Terrestrial Network Destination -- Busy
526
Terrestrial Network Destination -- No Answer
527
Terrestrial Network Destination -- Unavailable
528
Terrestrial Network Destination -- No Carrier
529
Service Timed Out
530
Terminated by Network Operator
531
Insufficient Resources at Mobile
532
Mobile Failure
533
Mobile -- Connection to DTE Lost
534
Mobile -- Unrecoverable DTE Protocol Error
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Page E--21
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--6.
MPDS +WQ Cause Codes and Strings (cont)
mmm
+WQ cause code string
535
Mobile Reset
536
User Cancellation of Connection Establishment
600
Unable to Find Satellite Access Node
601
Unable to Establish Communication with Satellite Access Node
602
Link with Satellite Access Node Lost
700
Reason Unspecified
701
L3 Release
702
L3 Deregister
703
L3 Reject
716
SAN Idle Timer Expiry
717
MAN Idle Timer Expiry
718
SAN Connect Timer
719
SAN Modify Timer
720
SAN Handover Timer
721
SAN Connection Timer
722
MAN Connection Timer
732
Insufficient operating system resources at MAN
733
Insufficient memory at MAN
748
Invalid L3 Call Ref in Establish SDU
749
Invalid L3 Call Ref in Modify SDU
764
Unsupported MPDS MAC version
765
Invalid Bearer Connection type in Establish SDU
766
Invalid Bearer Control type in Establish SDU
767
Invalid Bearer Connection ID in Establish SDU
768
Invalid Bearer Connection type in Modify SDU
769
Invalid Bearer Control type in Modify SDU
770
Invalid Bearer Connection ID in Modify SDU
771
Invalid Handover SDU
772
Invalid SDU type
773
SDU Incorrectly Formatted
23--20--35
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Page E--22
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Table E--6.
MPDS +WQ Cause Codes and Strings (cont)
mmm
+WQ cause code string
780
Connection sub--layer protocol failure (MAN specific signaling)
781
Connection sub--layer protocol failure (HDLC signaling)
796
Control sub--layer protocol failure
812
Channel Unit failure
813
Hardware failure
814
MAN not responding to frequency corrections
815
MAN not responding to power corrections
816
MAN not responding to timing corrections
828
Internal SAN failure
829
SAN Shutting Down
844
Bearer Control -- No satellite link
845
Bearer Control -- No suitable contention slot
846
Bearer Control -- Status Acknowledgement failure
847
Bearer Control -- Incorrect SAN ID
860
No such MAN
861
Invalid L3 Call Reference
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Page E--23
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
Blank Page
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Page E--24
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
APPENDIX F
FAILURE OVERVIEW
1. Fault Codes
CODE
FAILURE DESCRIPTION
UNKNOWN LEVEL 1 UNKNOWN SRU
00 0 01
RESERVED
00 0 02
SPARE
00 0 03
RESERVED
00 0 04
RESERVED
00 0 05
RESERVED
00 0 06
RESERVED
00 0 07
RESERVED
00 0 08
RESERVED
SDU
UNKNOWN SDU SRU
01 0 01
01 0 02
01 0 03
01 0 04
01 0 05
01 0 06
01 0 07
01 0 08
01 0 09
01 0 0A
01 0 0B
01 0 0C
01 0 0D
01 0 0E
01 0 0F
01 0 10
01 0 11
01 0 12
01 0 13
01 0 14
01 0 15
01 0 96
SPARE
HMPM HPA CMD WORD (143) UPDATE RATE FAIL
HMPM HPA CMD WORD (143) DATA FAIL
RESERVED
RESERVED
RESERVED
HSU1--SDU W’BURG DATA TX FAIL
HSU1--SDU W’BURG SOLO WORD ACK FAIL
SPARE
SPARE
HSU2--SDU W’BURG DATA TX FAIL
HSU2--SDU W’BURG SOLO WORD ACK FAIL
SPARE
SPARE
SPARE
HGA HPA COMMAND WORD (NCD)
SPARE
LGA HPA COMMAND WORD (NCD)
RESERVED
RESERVED
RESERVED
INCOMPLETE ID PROM RESPONSES
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Page F--1
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
FAILURE DESCRIPTION
SMPM: SDU MAIN PROCESSOR MODULE
01 1 81
SDU H/W--S/W COMPATIBILITY FAIL
01 1 82
BATTERY VOLTAGE LOW
01 1 83
WATCHDOG TIMEOUT FAIL
01 1 84
MICRO BOOT ROM FAIL
01 1 85/05
EEPROM FAIL
01 1 86/06
FLASH FAIL
01 1 87/07
SRAM FAIL
01 1 88/08
REAL TIME CLOCK FAIL
01 1 89
QUART FAIL
01 1 0A
SOFTWARE ERROR (SYSFAIL)
01 1 0B
FLASH--PSRAM MISCOMPARE
01 1 0C
FLASH--PSRAM MISCOMPARE EXTENSION
01 1 0D
FLASH--PSRAM MISCOMPARE EXTENSION
CODA: SDU VOICE CODEC MODULE A
01 2 81/01
PROGRAM MEMORY CRC FAIL
01 2 82
RESERVED
01 2 83
RESERVED
01 2 84
RESERVED
01 2 05
RESERVED
01 2 86
RESERVED
01 2 87/07
TIMING GENERATOR FAIL
01 2 88
DUAL PORT RAM FAIL CODEC SIDE
01 2 89
RESERVED
01 2 8A/0A
PROGRAM MEMORY W/R FAIL
01 2 8B PP
DSP INTERNAL MEMORY W/R FAIL
01 2 8C/0C
DSP COMPREHENSIVE FAIL
01 2 0D
HEALTH COUNT UPDATE
01 2 8E
DUAL PORT RAM FAIL SMPM SIDE
01 2 0F
SPARE
01 2 90
BUS ERROR
01 2 91
SELF TEST MISOPERATION
01 2 12
COMMUNICATION PROBLEM
01 2 93/13
RESERVED
01 2 94
ST BUS AUDIO LOOPBACK FAIL
01 2 95
SW DOWNLOAD FAIL
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
FAILURE DESCRIPTION
CODE
CODB: SDU VOICE CODEC MODULE B
01 3 Same entries as for CODA above except substitute CODB for CODA, SRU code 3 for
code 2, [CODEC_B] for [CODEC_A] and for .
Fault codes for codecs C--F have Level 2 (SRU) codes E--H. They are listed in the appropriate
section of this table for those SRU codes.
SIOM: SDU INPUT/OUTPUT MODULE (EXCLUSIVE TO SIOM)
01 4 81
A429 XMTR LOOP--BACK TO OTHER SDU FAIL
01 4 82
A429 XMTR LOOP--BACK TO CFDS FAIL
01 4 83
A429 XMTR LOOP--BACK TO ADL FAIL
01 4 84
A429 XMTR LOOP--BACK TO PDL FAIL
01 4 85
A429 XMTR LOOP--BACK TO (C)MUs FAIL
01 4 86
A429 XMTR LOOP--BACK TO SCDUs FAIL
01 4 87
A429 XMTR LOOP--BACK TO MULTI--CNTRL FAIL
01 4 88
RESERVED
01 4 89
A429 XMTR LOOP--BACK TO RMP/CAP FAIL
01 4 8A
A429 XMTR LOOP--BACK TO SNU/CPDF FAIL
01 4 8B
A429 XMTR LOOP--BACK TO HSU1 FAIL
01 4 8C
A429 XMTR LOOP--BACK TO HSU2 FAIL
01 4 8D
A429 XMTR LOOP--BACK SPARE
01 4 8E
A429 XMTR LOOP--BACK SPARE
01 4 8F
A429 XMTR LOOP--BACK SPARE
01 4 90
A429 XMTR LOOP--BACK SPARE
01 4 91
RESERVED
01 4 AB
SIOM BUS ERROR
01 4 2C
A429 TX TO OTHER SDU BUFFER FULL
01 4 2D
A429 TX TO CFDS BUFFER FULL
01 4 2E
A429 TX TO ADL BUFFER FULL
01 4 2F
A429 TX TO PDL BUFFER FULL
01 4 30
A429 TX TO (C)MUs BUFFER FULL
01 4 31
A429 TX TO SCDUs BUFFER FULL
01 4 32
A429 TX TO MULTI--CTRL BUFFER FULL
01 4 33
RESERVED
01 4 34
A429 TX TO RMP/CAP BUFFER FULL
01 4 35
A429 TX TO SNU/CPDF BUFFER FULL
01 4 36
A429 TX TO HSU1 BUFFER FULL
01 4 37
A429 TX TO HSU2 BUFFER FULL
01 4 38
A429 TX BUFFER FULL SPARE
01 4 39
A429 TX BUFFER FULL SPARE
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
01 4 3A
01 4 3B
01 4 BC
01 4 3D
FAILURE DESCRIPTION
A429 TX BUFFER FULL SPARE
A429 TX BUFFER FULL SPARE
SIOM INTERRUPT FAIL
IRS ASIC MATCHING PROBLEM
SMDM1: SDU MODEM MODULE #1
01 5 81
PROCESSOR FAIL
01 5 82/02
RESERVED
01 5 83/03
RESERVED
01 5 84/04
PROGRAM CRC FAIL
01 5 85/05
RESERVED
01 5 86/06
RESERVED
01 5 87
RESERVED
01 5 88/08
RESERVED
01 5 89/09
RESERVED
01 5 0A
MODEM TO RFM INTERFACE FAIL
01 5 8B
TIMER/INTERRUPT FAIL
01 5 8C
RESERVED
01 5 8D
RESERVED
01 5 8E
EXTERNAL MEMORY FAIL
01 5 8F/0F
RESERVED
01 5 90/10
RESERVED
01 5 91
MODEM DPR FAIL
01 5 92
RESERVED
01 5 93/13
RESERVED
01 5 94/14
RESERVED
01 5 95
SMPM SIDE DPR FAIL
01 5 16
SW DOWNLOAD FAIL
01 5 17
HEALTH COUNT UPDATE FAIL
01 5 18
RESERVED
01 5 99
BUS ERROR
01 5 9A
SELF TEST MISOPERATION
01 5 1B
SOFTWARE FAIL
01 5 1C
COMMUNICATIONS PROBLEM
01 5 1D
RESERVED
01 5 9E
RFM SSI LOOPBACK FAIL
01 5 9F
RESERVED
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
FAILURE DESCRIPTION
CODE
SMDM2: SDU MODEM MODULE #2
01 6 Same entries as for SMDM1 above except substitute SMDM2 for SMDM1, SRU code 6
for code 5, [MODEM_2] for [MODEM_1] and for .
SMDM3: SDU MODEM MODULE #3
01 7 Same entries as for SMDM1 above except substitute SMDM3 for SMDM1, SRU code 7
for code 5, [MODEM_3] for [MODEM_1] and for .
Fault codes for modems 4--7 have Level 2 (SRU) codes J, L, M and N. They are listed in this
table in the appropriate section for those SRU codes.
SRFM: SDU RADIO FREQUENCY MODULE
01 8 81
RESERVED
01 8 82
RESERVED
01 8 83
RESERVED
01 8 84
RESERVED
01 8 85
RESERVED
01 8 86
RESERVED
01 8 87
RESERVED
01 8 88
RESERVED
01 8 89
RESERVED
01 8 0A
SPARE
01 8 0B
SPARE
01 8 0C
SPARE
01 8 0D
SPARE
01 8 8E/0E
RF SYNTH CHAN1 LOCK DETECT FAIL
01 8 8F/0F
RESERVED
01 8 90/10
RF SYNTH CHAN2 LOCK DETECT FAIL
01 8 91/11
RESERVED
01 8 92/12
RF SYNTH CHAN3 LOCK DETECT FAIL
01 8 93/13
RESERVED
01 8 94/14
RESERVED
01 8 95/15
RESERVED
01 8 96/16
RF SYNTH CHAN4 LOCK DETECT FAIL
01 8 97/17
RF SYNTH CHAN5 LOCK DETECT FAIL
01 8 98/18
RF SYNTH CHAN6 LOCK DETECT FAIL
01 8 99/19
RF SYNTH CHAN7 LOCK DETECT FAIL
01 8 9A/1A
RF SYNTH CHAN8 LOCK DETECT FAIL
01 8 9B/1B
RF SYNTH TX BLOCK PLO LOCK DETECT FAIL
01 8 9C/1C
RF SYNTH RX BLOCK PLO LOCK DETECT FAIL
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
01 8 9D/1D
01 8 9E/1E
01 8 A0
01 8 A1
01 8 A2
01 8 A3
01 8 A4
01 8 A5
01 8 A6
01 8 A7
01 8 A8
01 8 A9
01 8 AA
01 8 AB
01 8 AC
01 8 AD
01 8 AE
01 8 AF
01 8 30
01 8 31
01 8 32
01 8 33
01 8 34
01 8 35
01 8 36
01 8 37
01 8 38
01 8 39
01 8 3A
01 8 3B
01 8 3C
01 8 3D
01 8 3E
01 8 3F
01 8 C0/40
01 8 C1/41
01 8 C2/42
01 8 C3/43
01 8 C4/44
FAILURE DESCRIPTION
RF SYNTH RX CHAN PLO LOCK DETECT FAIL
RF SYNTH TX DOPPLER PLO LOCK DETECT FAIL
RFM CHAN 1 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 1 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 2 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 2 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 3 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 3 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 4 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 4 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 5 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 5 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 6 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 6 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 7 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 7 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 8 L--BAND LOOP--BACK (TX) FAIL
RFM CHAN 8 L--BAND LOOP--BACK (RX) FAIL
RFM CHAN 1 TX CALIBRATION ERROR
RFM CHAN 2 TX CALIBRATION ERROR
RFM CHAN 3 TX CALIBRATION ERROR
RFM CHAN 4 TX CALIBRATION ERROR
RFM CHAN 5 TX CALIBRATION ERROR
RFM CHAN 6 TX CALIBRATION ERROR
RFM CHAN 7 TX CALIBRATION ERROR
RFM CHAN 8 TX CALIBRATION ERROR
RFM CHAN 1 RX CALIBRATION ERROR
RFM CHAN 2 RX CALIBRATION ERROR
RFM CHAN 3 RX CALIBRATION ERROR
RFM CHAN 4 RX CALIBRATION ERROR
RFM CHAN 5 RX CALIBRATION ERROR
RFM CHAN 6 RX CALIBRATION ERROR
RFM CHAN 7 RX CALIBRATION ERROR
RFM CHAN 8 RX CALIBRATION ERROR
RFM CHAN 1 AGC TELLBACK FAIL
RFM CHAN 2 AGC TELLBACK FAIL
RFM CHAN 3 AGC TELLBACK FAIL
RFM CHAN 4 AGC TELLBACK FAIL
RFM CHAN 5 AGC TELLBACK FAIL
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
01 8 C5/45
01 8 C6/46
FAILURE DESCRIPTION
RFM CHAN 6 AGC TELLBACK FAIL
RFM CHAN 7 AGC TELLBACK FAIL
01 8 C7/47
RFM CHAN 8 AGC TELLBACK FAIL
01 8 C8/48
RFM BLOCK AGC TELLBACK FAIL
01 8 C9
I/Q CALIBRATION FAIL
01 8 D0
01 8 D1
RFM CHAN 1 AGC CALIBRATION ERROR
RFM CHAN 2 AGC CALIBRATION ERROR
01 8 D2
RFM CHAN 3 AGC CALIBRATION ERROR
01 8 D3
RFM CHAN 4 AGC CALIBRATION ERROR
01 8 D4
RFM CHAN 5 AGC CALIBRATION ERROR
01 8 D5
RFM CHAN 6 AGC CALIBRATION ERROR
01 8 D6
01 8 D7
RFM CHAN 7 AGC CALIBRATION ERROR
RFM CHAN 8 AGC CALIBRATION ERROR
01 8 D8
RFM BLOCK AGC CALIBRATION ERROR
SCFM: SDU CHANNEL FILTER MODULE
01 9 81/01
01 9 82/02
01 9 83/03
01 9 04
01 9 05
01 9 06
01 9 07
01 9 08
RESERVED
RESERVED
RESERVED
RESERVED
RESERVED
RESERVED
RESERVED
RESERVED
01 9 09
RESERVED
01 9 0A
RESERVED
OCXO: SDU OVEN CONTROLLED CRYSTAL OSCILLATOR
01 A 01
OVEN READY FAIL
SMB: SDU MOTHER BOARD
01 B NONE
SPSU: SDU AC OR DC POWER SUPPLY UNIT
01 C 01
01 C 02
01 C 03
PSU TEMP LIMITS FAIL
SPARE
PSU SECONDARY VOLTAGE FAIL
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
FAILURE DESCRIPTION
SFPDM: SDU FRONT PANEL DISPLAY MODULE
01 D 01
TEST (PAST) SWITCH STUCK
01 D 02
MANUAL SCROLL SWITCH STUCK
CODC: SDU VOICE CODEC MODULE C
01 E Same entries as for CODA (01 2 xx) above except substitute CODC for CODA, SRU
code E for code 2, [CODEC_C] for [CODEC_A] and for .
CODD: SDU VOICE CODEC MODULE D
01 F Same entries as for CODA (01 2 xx) above except substitute CODD for CODA, SRU
code F for code 2, [CODEC_D] for [CODEC_A] and for .
CODE: SDU VOICE CODEC MODULE E
01 G Same entries as for CODA (01 2 xx) above except substitute CODE for CODA, SRU
code G for code 2, [CODEC_E] for [CODEC_A] and for .
CODF: SDU VOICE CODEC MODULE F
01 H Same entries as for CODA (01 2 xx) above except substitute CODF for CODA, SRU
code H for code 2, [CODEC_F] for [CODEC_A] and for .
01 I
Not used.
SMDM4: SDU MODEM MODULE #4
01 J Same entries as for SMDM1 (01 5 xx) above except substitute SMDM4 for SMDM1,
SRU code J for code 5, [MODEM_4] for [MODEM_1] and for
.
01 K Not used.
SMDM5: SDU MODEM MODULE #5
01 L Same entries as for SMDM1 (01 5 xx) above except substitute SMDM5 for SMDM1,
SRU code L for code 5, [MODEM_5] for [MODEM_1] and for
.
SMDM6: SDU MODEM MODULE #6
01 M Same entries as for SMDM1 (01 5 xx) above except substitute SMDM6 for SMDM1,
SRU code M for code 5, [MODEM_6] for [MODEM_1] and for
.
SMDM7: SDU MODEM MODULE #7
01 N Same entries as for SMDM1 (01 5 xx) above except substitute SMDM7 for SMDM1,
SRU code N for code 5, [MODEM_7] for [MODEM_1] and for
.
23--20--35
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
FAILURE DESCRIPTION
CODE
VIM: VOICE INTERFACE MODULE
01 P 81
CABIN INTERFACE 1 AUDIO LOOPBACK FAIL
01 P 82
CABIN INTERFACE 2 AUDIO LOOPBACK FAIL
01 P 83
COCKPIT INTERFACE 1 AUDIO LOOPBACK FAIL
01 P 84
COCKPIT INTERFACE 2 AUDIO LOOPBACK FAIL
01 P 85
CTU CEPT--E1 AUDIO LOOPBACK FAIL
01 P 06
SPARE
01 P 07
CABIN AUDIO DISCRETE OUTPUTS LOOPBACK FAIL
01 P 08
COCKPIT AUDIO DISCRETE OUTPUTS LOOPBACK FAIL
01 P 89
CTU CEPT--E1 HDLC LOOPBACK FAIL
01 P 8A
CABIN INTERFACE 1 BUS ERROR
01 P 8B
CABIN INTERFACE 2 BUS ERROR
01 P 8C
COCKPIT INTERFACE 1 BUS ERROR
01 P 8D
COCKPIT INTERFACE 2 BUS ERROR
01 P 8E
CTU CEPT--E1 BUS ERROR
“OTHER” SATCOM SYSTEM
02 0 01
PROTOCOL VERSION NUMBER INCOMPATIBLE
02 0 02
SDU/SDU MESSAGE PROTOCOL ERROR
HSU
Only applicable to Package 6.0 and subsequent.
UNKNOWN HSU SRU
03 0 01
03 0 02
03 0 03
03 0 84
03 0 05
03 0 86/06
03 0 87/07
03 0 08
03 0 09--0B
03 0 0C
03 0 0D
03 0 8E/0E
03 0 0F
03 0 10
03 0 11
HSU SELF--DECLARED FAILURE
HSU WILLIAMSBURG PROTOCOL ALO/ALR FAIL
HSU WILLIAMSBURG PROTOCOL DATA XFER FAIL
HSU SELF--TEST MISOPERATION
HSU SERIAL PORT MIS--WIRING
HSU TOTC RESET
HSU POC RESET
SPARE
RESERVED
HSU CHANNEL 1 FAILURE
HSU CHANNEL RELEASE ACKNOWLEDGE FAILURE
HSU RF LOOPBACK INHIBIT FAILURE
HSU CHANNEL 2 FAILURE
HSU CHANNEL 3 FAILURE
HSU CHANNEL 4 FAILURE
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
FAILURE DESCRIPTION
HSCC1: HSU CHANNEL CARD 1
03 1 01
HSU CC1 MODEM FAULT
03 1 02
HSU CC1 MODEM FAILURE
03 1 03
HSU CC1 PERIPHERAL ERROR
03 1 04
HSU CC1 PERIPHERAL FAILURE
03 1 05
HSU CC1 CP SW INCOMPATIBILITY
03 1 06
RESERVED
03 1 07
HSU CC1 RF FAULT
03 1 08
HSU CC1 RF FAILURE
03 1 09
HSU CC1 TAL ERROR
03 1 0A
HSU CC1 MODEM CALIBRATION MISSING
03 1 0B
HSU CC1 TEMPERATURE UNREADABLE
03 1 0C
HSU CC1 OVER TEMPERATURE
03 1 0D
RESERVED
03 1 0E
HSU CC1 TURBO FAULT
03 1 0F
HSU CC1 TURBO FAILURE
03 1 10
RESERVED
03 1 11
HSU CC1 VCODEC FAULT|
03 1 12
HSU CC1 VCODEC FAILURE
03 1 93
HSU CC1 APPLICATION CODE ERROR
HSCC2: HSU CHANNEL CARD 2
03 2 01
HSU CC2 MODEM FAULT
03 2 02
HSU CC2 MODEM FAILURE
03 2 03
HSU CC2 PERIPHERAL ERROR
03 2 04
HSU CC2 PERIPHERAL FAILURE
03 2 05
HSU CC2 CP SW INCOMPATIBILITY
03 2 06
RESERVED
03 2 07
HSU CC2 RF FAULT
03 2 08
HSU CC2 RF FAILURE
03 2 09
HSU CC2 TAL ERROR
03 2 0A
HSU CC2 MODEM CALIBRATION MISSING
03 2 0B
HSU CC2 TEMPERATURE UNREADABLE
03 2 0C
HSU CC2 OVER TEMPERATURE
03 2 0D
RESERVED
03 2 0E
HSU CC2 TURBO FAULT
03 2 0F
HSU CC2 TURBO FAILURE
03 2 10
RESERVED
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
03 2 11
03 2 12
03 2 93
FAILURE DESCRIPTION
HSU CC2 VCODEC FAULT
HSU CC2 VCODEC FAILURE
HSU CC2 APPLICATION CODE ERROR
HSDIO: HSU DATA I/O CARD
03 3 01
RESERVED
03 3 02
HSU UNRECOVERABLE SW / PROTOCOL ERROR
03 3 03
HSU I/O CHANNEL CARD 1 UNSERVICEABLE
03 3 04
HSU I/O CHANNEL CARD 2 UNSERVICEABLE
03 3 85
HSU CONFIGURATION ERROR
03 3 86
HSU I/O PERIPHERAL FAILURE
03 3 07
HSU I/O BOTH CHANNEL CARDS UNSERVICEABLE
03 3 08
HSU I/O RAM FAULT
03 3 09
HSU I/O ROM FAULT
03 3 0A
HSU SW CONFIGURATION ERROR
03 3 0B
HSU PPPoE SESSION FAILURE
HSCP: HSU CONTROL PROCESSOR
03 4 01
RESERVED
03 4 02
RESERVED
03 4 03
RESERVED
03 4 04
RESERVED
03 4 05
RESERVED
03 4 06
RESERVED
03 4 87/07
HSU CP CHANNEL CARD 1 UNRESPONSIVE
03 4 88/08
HSU CP CHANNEL CARD 2 UNRESPONSIVE
03 4 89/09
HSU CP BOTH CHANNEL CARDS UNRESPONSIVE
03 4 8A/0A
HSU DATA I/O CARD UNRESPONSIVE
03 4 0B CM
HSU CP RAM FAULT
03 4 0C CM
HSU CP ROM FAULT
03 4 0D CM
HSU OVER TEMPERATURE
03 4 0E CM
HSU CHANNEL CARD 1 OVER TEMPERATURE
03 4 0F CM
HSU CHANNEL CARD 2 OVER TEMPERATURE
03 4 10 CM
HSU BOTH CHANNEL CARDS OVER TEMPERATURE
03 4 91 PP
HSU ADL BUS INTERFACE FAILURE
03 4 92 PP
HSU PDL BUS INTERFACE FAILURE
03 4 93 PP
HSU DATA I/O DUART FAILURE
03 4 94 PP
HSU CHANNEL CARD 1 DUART FAILURE
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
03 4 95 PP
03 4 96 PP
03 4 97 PP
03 4 98 PP
03 4 99 PP
FAILURE DESCRIPTION
HSU CHANNEL CARD 2 DUART FAILURE
HSU BOTH CHANNEL CARDS DUART FAILURE
HSU MAINTENANCE INTERFACE DUART FAILURE
HSU DISCRETE OUTPUT FAILURE
HSU BOARD CONFIGURATION/REVISION FAILURE
HOCXO: HSU OVEN--CONTROLLED 10 MHZ OSCILLATOR
03 5 01
HSU OCXO TIMEOUT
03 5 02
HSU OCXO TEMPERATURE UNSTABLE
HSPSU: HSU POWER SUPPLY UNIT 1
03 6 01
HSU POWER SUPPLY FAIL
03 6 02
HSU PSU OVER TEMPERATURE
HSCDM: HSU CONFIGURATION DATA MODULE
03 7 NONE
HSFP: HSU FRONT PANEL
03 8 81
HSU SELF--TEST BUTTON STUCK
HSBP: HSU BACKPLANE
03 9 NONE
HGA/IGA HPA
This section lists failure codes inclusive of all HPA designs. Each HPA uses the SRU codes
appropriate to its design.
UNKNOWN HGA/IGA HPA SRU
04 0 01
STATUS WORD (143) UPDATE RATE FAIL
04 0 02
STATUS WORD (143) DATA FAIL
04 0 03
MNTNC WORD (350) UPDATE RATE FAIL
04 0 04
MNTNC WORD (350) DATA FAIL
04 0 05
SPARE
04 0 06
SPARE
04 0 87
SELF--TEST MISOPERATION
04 0 08
RF OVERDRIVE ERROR
04 0 09
RF SUPPLY CURRENT FAIL
04 0 0A
OVER TEMP (COMB/DET) SHUTDOWN
04 0 0B
NO RESPONSE TO CARRIER COMMAND
04 0 0C
FAILURE WARNING W/NO DISC’S SET
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
04 0 0D
04 0 0E
04 0 0F
04 0 10
04 0 40
04 0 41
FAILURE DESCRIPTION
429 MNTNC WORD PSU FAIL (350)
429 MNTNC WORD INTERNAL RAM FAIL
429 MNTNC WORD INTERNAL ROM FAIL
CLASS C HPA MAX AVAIL PWR FAIL
SELF--TEST BUTTON STUCK
RESERVED (HP--720 “RF Power Input Low”)
HPSU: HPA AC OR DC POWER SUPPLY UNIT
04 1 01
PSU OVER TEMP SHUTDOWN
04 1 02
PSU TEMP SENSOR FAIL
04 1 03
PSU BIAS +5VDC FAIL
04 1 04
PSU +28/+25.5 VDC FAIL
04 1 05
PSU +5 VDC FAIL
04 1 06
PSU +15 VDC FAIL
04 1 07
PSU --15 VDC FAIL
04 1 08
PSU --85 VDC FAIL
04 1 09
PSU +8 VDC FAIL
04 1 0A
PSU +16 VDC FAIL
04 1 40
INTERNAL POWER SUPPLY FAIL
04 1 41
PSU OVER TEMP
HMPM: HPA MAIN PROCESSOR MODULE
04 2 81
H/W--S/W COMPATIBILITY FAIL
04 2 02
SPARE
04 2 83/03
BOOT FLASH MEMORY FAIL
04 2 04
A429 SDU XMTR LOOP--BACK FAIL
04 2 05
SPARE
04 2 06
SPARE
04 2 87
A429 MULTICNT RCVR FAIL
04 2 88
A429 ADL RCVR FAIL
04 2 89
A429 PDL--TO--HPA RCVR FAIL
04 2 0A
MAINTENANCE MEMORY CRC FAIL
04 2 0B
MAINTENANCE MEMORY WRITE FAIL
04 2 8C/0C
CALIBRATION MEMORY CRC FAIL
04 2 0D
CALIBRATION MEMORY WRITE FAIL
04 2 8E/0E
PROGRAM FLASH MEMORY FAIL
04 2 0F
SPARE
04 2 90
RAM FAIL
04 2 11
CPU OVER TEMP SHUTDOWN
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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
04 2 12
04 2 93/13
04 2 94/14
04 2 95/15
04 2 96/16
04 2 17
04 2 98
04 2 19
04 2 1A
04 2 1B
04 2 9C/1C
04 2 9D
04 2 9E
04 2 1F
04 2 A0
04 2 21
04 2 A2
04 2 23
04 2 24
04 2 A5
04 2 A6
04 2 A7
04 2 A8
04 2 29
04 2 2A
04 2 2B
04 2 2C
04 2 AD/2D
04 2 2E
04 2 2F
04 2 30
04 2 31
04 2 32
04 2 B3/33
04 2 B4
04 2 35
04 2 C0
04 2 C1/41
04 2 C2
FAILURE DESCRIPTION
CPU TEMP SENSOR FAIL
CPU GND REF FAIL
FAN RELAY DRIVER FAIL
BIAS ENABLE LOOPBACK FAIL
VAR ATTN DRIVER FAIL
FRONT PANEL TEST SWITCH STUCK
WATCHDOG TIMEOUT FAIL
DRIVER GND FAIL
SPARE
SPARE
DRIVER TEST -- MUX
DRIVER TEST -- GREEN LED
DRIVER TEST -- RED LED
SPARE
DRIVER TEST--MUTE ATTENUATOR
SPARE -- -- -- -- - DRIVER TEST -- SER DATA CONCATENATE
SPARE
SPARE
MUTE INPUT TEST
CPU DEVICE TEST
ACTUAL POWER CALIBRATION
VALIDATION OF UPLOAD
MUTE ATTEN P OUT OF LIMITS
CODE VPP OUT OF LIMITS
MAINT LOG VPP OUT OF LIMITS
CAL MEM VPP OUT OF LIMITS
ADC REF OUT OF LIMITS
PWR LO OUT OF LIMITS
PSU TEMP LO OUT OF LIMITS
AMPS LO OUT OF LIMITS
SOFTWARE FAULT
SPARE
DISC OUTPUT TEST -- FAN
RS--422 INTERNAL LOOPBACK FAIL
IGA LNA/DIP ON/OFF DISC LOOP FAIL
I2C INTERFACE FAILURE
RAM FAILURE
KERNAL CODE ERROR
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page F--14
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
04 2 C3
04 2 C4
04 2 C5
04 2 C6
04 2 C7
04 2 C8
04 2 C9/49
04 2 CA/4A
04 2 CB
04 2 4C
04 2 4D
FAILURE DESCRIPTION
APPLICATION CODE ERROR
CONFIGURATION ERROR
SDU BUS I/F FAILURE
ADL BUS I/F FAILURE
PDL BUS I/F FAILURE
MAINTENANCE DUART FAILURE
DISCRETE OUTPUTS FAILURE
CP TEMP SENSOR FAILURE
BOARD CONFIG/REV FAILURE
I2C INTERFACE FAILURE
ROM FAILURE
DRIV: HPA RF DRIVER
04 3 01
04 3 02
04 3 03
04 3 04
04 3 05
DRIVER RF OUTPUT FAIL
DRIVER TEMP SENSOR FAIL
DRIVER OVER TEMP SHUTDOWN
DRIVER VCC FAIL
SPARE
SPLT: HPA RF SPLITTER
04 4 01
SPARE
PWR1: HPA RF POWER AMPLIFIER (1)
04 5 01
RF BALANCE FAIL
04 5 02
VCC FAIL
04 5 03
SPARE
PWR2: HPA RF POWER AMPLIFIER (2)
04 6 Same as for PWR1 except sub. SRU code 6 for 5 and for .
PWR3: HPA RF POWER AMPLIFIER (3)
04 7 Same as for PWR1 except sub. SRU code 7 for 5 and for .
C/DET: HPA RF POWER COMBINER/DETECTOR
04 8 01
FORWARD OUTPUT POWER DET 1 FAIL
04 8 02
FORWARD OUTPUT POWER DET 2 FAIL
04 8 03
FORWARD OUTPUT PWR COMPARE FAIL
04 8 04
REFLECTED OUTPUT PWR DET FAIL
04 8 05
COMBINER TEMP SENSOR FAIL
04 8 06
SPARE
23--20--35
Honeywell International Inc. Do not copy without express permission of Honeywell.
Page F--15
15 Jul 2006
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
MCS--4200/7200 Multi--Channel SATCOM System
CODE
FAILURE DESCRIPTION
FPAMP: HPA RF FINAL POWER AMPLIFIER
04 9 01
FINAL AMP 1 RF BALANCE FAIL
04 9 02
FINAL AMP 1 VCC FAIL
04 9 03
SPARE
04 9 04
FINAL AMP 2 RF BALANCE FAIL
04 9 05
FINAL AMP 2 VCC FAIL
04 9 06
SPARE
04 9 C0/40
PA UNRESPONSIVE
04 9 41
SPARE
04 9 42
OVER CURRENT FAILURE
04 9 43
DRIVER AMPLIFIER DC VOLTAGE FAILURE
04 9 44
DRIVER AMPLIFIER CURRENT FAILURE
04 9 45
12 VDC FAILURE
04 9 46
PA MUTE FAILURE
04 9 47
PA OVER TEMP
04 9 48
PA STATUS FAILURE
04 9 49
PA TEMP SENSOR FAILURE
HMB: HPA MOTHER BOARD
04 A 40
BP TEMP SENSOR FAILURE
RFAM: 20W HPA RF AMPLIFIER MODULE
04 B 01
OVER TEMP SHUTDOWN
04 B 02
RFAM VCC FAIL
04 B 03
AMP 1 VCC FAIL
04 B 04
FORWARD OUTPUT POWER DET 1 FAIL
04 B 05
FORWARD OUTPUT POWER DET 2 FAIL
04 B 06