Leidos NORMARC7033 7033 Dual Frequency Glide Path User Manual General Description 7011

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Document ID	91082
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Document Description	Normarc 7033 ILS General Description
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Date Submitted	2000-03-14 00:00:00
Date Available	2000-05-03 00:00:00
Creation Date	1999-12-21 13:18:21
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Document Lastmod	1999-12-21 13:19:36
Document Title	General Description 7011.book
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NORMARC 7033
INSTRUMENT LANDING SYSTEM
GENERAL DESCRIPTION
©1999 Navia Aviation AS
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
TABLE OF CONTENTS
DESCRIPTION OF NORMARC 7033 2-FREQUENCY SYSTEM .....................1
1 GENERAL DESCRIPTION ..............................................................................1
1.1 Technical Specifications..................................................................................... 1
1.1.1 Signal Minimum Performance GP ............................................................... 1
1.1.2 Environmental Characteristics ..................................................................... 2
1.1.3 EMC Characteristics .................................................................................... 2
1.1.4 Mechanical Characteristics .......................................................................... 3
1.1.5 Power Supply............................................................................................... 3
1.2 General Information............................................................................................ 3
1.2.1 Introduction ................................................................................................. 3
1.2.2 Product Type Numbers................................................................................ 7
1.2.3 Abbreviations ............................................................................................... 7
2 PHYSICAL ORGANIZATION...........................................................................8
2.1 Module and Assembly Location ......................................................................... 8
2.2 Power Supply ..................................................................................................... 9
3 SYSTEM DESCRIPTION.................................................................................12
3.1 Overview ............................................................................................................ 12
3.2 Physical Description ........................................................................................... 12
3.3 Monitors.............................................................................................................. 13
3.4 Transmitters / Modulators................................................................................... 13
3.5 TX Control .......................................................................................................... 13
3.6 Remote Monitoring (RMS) Unit .......................................................................... 14
3.7 Remote Control Unit........................................................................................... 14
3.8 Remote Slave Panel........................................................................................... 14
3.9 Remote Maintenance Monitoring (RMM) ........................................................... 14
3.9.1 RMM Access................................................................................................ 16
3.9.2 Local Keyboard/Display Functions .............................................................. 16
3.9.3 Diagnostic functions..................................................................................... 17
4 ELECTRICAL INSTALLATION ........................................................................18
4.1
4.2
4.3
4.4
4.5
4.6
4.7
4.8
4.9
4.10
4.11
4.12
4.13
4.14
Connection Overview ......................................................................................... 18
Power and Battery.............................................................................................. 18
RF Inputs............................................................................................................ 20
RF Outputs ......................................................................................................... 20
DC Loop ............................................................................................................. 21
Remote Control .................................................................................................. 22
PC and Modem .................................................................................................. 23
DME ................................................................................................................... 24
Analog Inputs ..................................................................................................... 25
Digital Inputs and Outputs .................................................................................. 26
Battery Warning.................................................................................................. 27
Remote control connections............................................................................... 28
Remote slave connection ................................................................................... 30
Interlock switch connection ................................................................................ 31
©1999 Navia Aviation AS
Table of contents
iii
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
Table of contents
iv
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
LIST OF FIGURES
Figure1-1
Figure1-2
Figure1-3
Figure1-4
Figure2-1
Figure2-2
Figure2-3
Figure3-1
Figure3-2
Figure3-3
Figure4-1
Figure4-2
Figure4-3
Figure4-4
Figure4-5
Figure4-6
Figure4-7
Figure4-8
Figure4-9
Figure4-10
Figure4-11
Figure4-12
Figure4-13
Figure4-14
Figure4-15
Typical ILS installation .......................................................................... 4
Glidepath block diagram ....................................................................... 4
Glidepath Antenna ................................................................................ 5
Glidepath Cabinet Installation .............................................................. 6
NM 7033 Module Location - Front view. ............................................... 9
NM 7033 Module Location - Rear view of main section. ...................... 10
NM 7033 Module Location - Front view of wall-mounted section ......... 11
ILS block diagram. ................................................................................ 12
The NM 7000 series RMM/RMS systems. ........................................... 15
Local Control Panel .............................................................................. 17
ILS main cabinet connection overview. ................................................ 18
Power and backup battery connections. .............................................. 19
RF input connections. ........................................................................... 20
RF output connections. ........................................................................ 20
DC loop connections. ........................................................................... 21
Remote control connection. .................................................................. 22
PC and modem connections. ............................................................... 23
DME connections. ................................................................................ 24
Analog input connections. .................................................................... 25
Digital input/output connections. .......................................................... 26
Battery warning connections. ............................................................... 27
Remote control to ILS connection ........................................................ 28
Remote control power supply connections ........................................... 29
Remote slave connection ..................................................................... 30
Interlock switch connection .................................................................. 31
©1999 Navia Aviation AS
List of Figures
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
List of Figures
vi
©1999 Navia Aviation AS
NORMARC 7033
OPERATING MANUAL
INSTRUMENT LANDING SYSTEM
LIST OF TABLES
©1999 Navia Aviation AS
21446-3.4
List of tables
vii
OPERATING MANUAL
NORMARC 7033
INSTRUMENT LANDING SYSTEM
List of tables
viii
21446-3.4
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
DESCRIPTION OF NORMARC 7033 2-FREQUENCY SYSTEM
General Description
1.1
Technical Specifications
NM 7033 Dual-Frequency Glidepath Cabinet.
1.1.1
Signal Minimum Performance GP
Transmitter
Frequency range
Frequency tolerance
Output power (CSB + SBO) Course
Output power (CSB) Clearance
Harmonic radiation
RF difference frequency (2-freq. only)
Spurious
Output power stability
CSB/SBO stability
Modulator - Course line
Modulation depth 90/150 Hz
adjustable range
SDM stability
DDM stability
Frequency tolerance
Total harmonic dist. (90/150 Hz)
Phase locking (90 Hz to 150 Hz)
SBO phaser adjustment range
40%
10-44%
+ 0.8% SDM
+ 0.2% DDM
+ 0.05 Hz
1% maximum
5° maximum ref 150 Hz
+ 30°
Modulator - Clearance
Modulation depth
90 Hz component
150 Hz component
Adjustable range DDM
Adjustable range SDM
Stability
Frequency tolerance
Total harmonic dist. (90/150 Hz)
Phase locking (90 Hz to 150 Hz)
80%
20%
60%
20-100% 150 Hz dominance
20-90%
+ 0.2 dB
+ 0.05 Hz
1% maximum
5° maximum ref 150 Hz
Monitoring
Alarm Functions
RF power reduction
Change of nominal CL
Range (*)
1-5 dB
+ 10-60 uA
©1999 Navia Aviation AS
328.6-335.4 MHz
+ 0.002%
3-7 W adjustable
0.3-1 W adjustable
2.5 uW maximum
15 kHz + 5 kHz
25 uW maximum
+ 0.2 dB
+ 0.3 dB
GENERAL DESCRIPTION
1-1
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
Change of nominal DS from nominal
value
Change of nominal CLR (2-freq only)
Change of nominal NF
Change of nominal SDM
Difference frequency (2-freq. only)
Total period of radiation out of tolerance
Additional NF time delay
Line break, ILS - Remote Control (disable optional)
Monitor input levels:
Adjustment range, nominal level
AGC range for less than 1%
change in SDM
Monitor stability at nominal levels:
RF power values
DDM values
SDM values
Warning Functions:
RF power reduction
Change of nominal CL
Change of nominal DS
Change of nominal CLR
Change of nominal NF
Change of SDM
Difference frequency
Mains failure
Remote Control
Data Transmission Medium
Data modulation
Transmitter level
Receiver dynamic range
+ 10-60 uA
+ 10-60 uA
+ 10-60 uA
+ 2-8% SDM
+ 2-5 kHz
1-6 sec.
0-20 sec.
-5 to –34 dBm
5 dB
+ 0,3 dB
+ 1 uA
+ 1% SDM
40-75% of Alarm limit
40-75% of Alarm limit
40-75% of Alarm limit
40-75% of Alarm limit
40-75% of Alarm limit
40-75% of Alarm limit
40-75% of Alarm limit
2-wire line, 600 ohm
serial, FSK
-10dBm + 2 dB
-10dBm to -34dBm
* asymmetrical limits are possible.
1.1.2
Environmental Characteristics
Operating temperature
Storage temperature
1.1.3
EMC Characteristics
EMR:
Spurious and harmonics:
GENERAL DESCRIPTION
1-2
-10 to +55 °C
-30 to +60 °C
EN 55022 class B
CISPR 22
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
1.1.4
Mechanical Characteristics
Dimensions: (H x W x D)
ILS Rack:
Remote control:
Slave panels:
1020x600x500 mm
129x71x170 mm
129x41x170 mm
Weight:
85 kg – 95 kg depending on model
The ILS rack is wall mounted. The remote control and slave panels fit a standard 3U (132mm)
high 19" subrack.
1.1.5
Power Supply
External supply:
Input voltage:
Output voltage:
Output current:
ILS cabinet
Input voltage
Current consumption:
Stand-by Battery
1.2
230V +15%/-20%,45-65 Hz or120V +15%/-20%,
45-65 Hz
27,6V
20A max
22-28V DC
8A – 14A depending on configuration
24V DC nominal, 85 Ah-110Ah valve regulated
lead-acid battery recommended
General Information
This paragraph gives a description of a typical ILS installation and the Normarc Glidepath system. Conventions and abbreviations used in this manual are also given.
1.2.1
Introduction
This is an overview of Normarc's NM703X ILS glidepath systems.
1.2.1.1 ILS Overview
A complete Instrument Landing System comprises:
• A LOCALIZER SYSTEM, producing a radio course to furnish lateral guidance to the airport
runway.
• A GLIDE PATH SYSTEM, producing a radio course to furnish vertical guidance down the
correct descent angle to the runway.
• MARKER BEACONS, to provide accurate radio fixes along the approach course.
©1999 Navia Aviation AS
GENERAL DESCRIPTION
1-3
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
The layout of a typical ILS airport installation is shown below.
Localizer
110 MHz
Glide Path
330 MHz
Marker Beacon
75MHz
3°
HBK547-1
Figure1-1 Typical ILS installation
1.2.1.2 Glidepath Overview
The complete ILS Glidepath system comprises:
• A GP transmitter/monitor cabinet
• An antenna distribution network
• A monitor network
• A GP antenna array
• Near-field monitor antenna
A block diagram is shown below:
GP
TRANSMITTER
ILS Localizer
TRANSMITTER
AND
MODULATOR
I and II
CSB CL
SBO CL
CSB CLR*
and Glide Path
REMOTE
CONTROL
UNIT
ANTENNA
DISTRIBUTION NETW.
**
CL
MONITOR
I and II
CLR*
MONITOR
DS
NETWORK
NF
***
SLAVE
PANEL
24V
BATTERY
POWER
SUPPLY
MAINS INPUT
220V/110V AC
HBK205-1
* CLR signals only used for 2-frequency systems.
** Antenna distribution network not used for Null Reference.
*** Middle antenna used for M-Array and Modified M-Array.
GP-BLOCK DIAGRAM
Figure1-2 Glidepath block diagram
GENERAL DESCRIPTION
1-4
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
Figure1-3 Glidepath Antenna
©1999 Navia Aviation AS
GENERAL DESCRIPTION
1-5
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
Figure1-4 Glidepath Cabinet Installation
1.2.1.3 Glidepath Description
To shape the glide path signal, ground plane reflection from an area in front of the antenna
array is necessary. The specific requirements to the area are given in the antenna handbook.
The glide path site may be located on either side of the runway, but the most reliable operation
will be obtained if the site is selected on terrain least obstructed by taxiways, aircraft holding
aprons, parking ramps, buildings, power lines etc. The site should offer the widest area of
smooth ground with possibilities of levelling without excessive physical or economical effort, if
indeed levelling is deemed necessary.
The glide path antenna system should be located at a distance of 75-200 m from the runway
center line. The distance from the runway threshold is a function of several factors upon which
establishment of the optimum operational conditions depend. These factors are:
GENERAL DESCRIPTION
1-6
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
1. The glide path angle.
2 Threshold crossing height requirements.
3. Obstruction clearance requirements
4 The slope of the terrain in front of the antenna system.
5. The extent of smooth terrain in the site area and beyond the threshold.
1.2.2
Product Type Numbers
The Normarc product numbering system is based on the following three levels:
• System
• Assembly
• Module
Systems have type numbers starting with NM, for example NM 7033. Systems consist of
assemblies, modules and parts.
Assemblies have type numbers consisting of three letters, a three- or four- digit number and a
letter, for example LPA 1230A. LPA is an abbreviation of Localizer Power amplifier Assembly,
1230 is a running number, and the last letter is the variant designator. Assemblies can consist
of assemblies, modules and parts.
Modules have type numbers consisting of two letters, a three- or four- digit number and a letter, for example FD 1235A. FD is an abbreviation of Feedback Detector, 1235 is a running
number, and the last letter is the variant designator. Modules consist of parts.
Glidepath Cabinet External Label
1.2.3
AC
ADC
AGC
CL
CLR
COU
CPU
CS
Abbreviations
Alternating Current
Analog to Digital Converter
Automatic Gain Control
Course Line
Clearance
Course
Central Processing Unit
Course Sector
©1999 Navia Aviation AS
GENERAL DESCRIPTION
1-7
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
DAC
DC
DDM
DF
DL
DS
DSP
EEPROM
EMC
EMI
EPROM
FFT
FIFO
FPGA
GPA
I/F
I²C
IIC
ILS
LED
LF
LLZ
LPA
LRU
MCU
NAV
NF
PC
RAM
RF
RMM
RMS
ROM
RTC
SC
SDM
SPA
SRAM
STB
SW
TRM
TX
Digital to Analog Converter
Direct Current
Difference in Depth of Modulation
Difference Frequency
Dc Loop
Displacement Sensitivity
Digital Signal Processor
Electrically Erasable Progammable Read Only Memory
ElectroMagnetic Compatibility
ElectroMagnetic Interference
Erasable Programmable Read Only Memory
Fast Fourier Transform
First-In-First-Out
Field Programmable Gate Array
Glidepath Power amplifier Assembly
InterFace
Inter Integrated Circuit
Same as I²C
Instrument Landing System
Light Emitting Diode
Low Frequency
Localizer
Localizer Power amplifier Assembly
Line Replacable Unit
Monitor Combiner Unit
NAVigation signals
Near Field
Personal Computer
Random Access Memory
Radio Frequency
Remote Maintenance Monitor
Remote Monitoring System
Read Only Memory
Real Time Clock
Station Control
Sum in Depth of Modulation
Same Parameter Alarm
Static Random Access Memory
Standby
SoftWare
TeRMinator
Transmitter
Physical Organization
2.1
Module and Assembly Location
The figures on the following pages show the locations of the modules in the main cabinet.
Figure 2-1 shows the main section of the GP cabinet from a front view, with indications of the
plug-in board locations.
PHYSICAL ORGANIZATION
2-8
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
Figure 2-2 shows the same section from a rear view, while Figure 2-3 shows the top half of the
wall-mounted section.
In addition, the Remote Control Assembly RCA1240C/D and Remote Slave SF 1344A are
installed in the technical control room and the control tower, respectively.
2.2
Power Supply
PS 1227A
1 1
An External Power Supply, operating at 230V/120V mains input and providing 27V at 20A, is
normally supplied with the equipment. In special cases, a second external power supply is
supplied.
OS1221B
MF 1219A
LF1223A
TCA 1218A
MO1212A
RMA1215A
COA1207C
GPA1231A
GPA1232A
HBK 536-1
Figure2-1 NM 7033 Module Location - Front view.
©1999 Navia Aviation AS
PHYSICAL ORGANIZATION
2-9
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
MB 1203
TX2
CLR
TX1
CLR
TX2
CL
TX1
CL
COA 1207C
SBO 1
SBO 2
SBO
SBO
CSB
CSB
SBO 1
SBO 2
IN
IN
OUT
DUMMY
OUT
DUMMY
IN
IN
SBO
OUT
SBO
CSB
CSB
DUMMY
OUT
DUMMY
VIEW A-A
HBK 593-1
Figure2-2 NM 7033 Module Location - Rear view of main section.
PHYSICAL ORGANIZATION
2-10
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
Terminal block for
power and battery connection
and decoupling capacitor
CI 1210A
HBK541-1
Figure2-3 NM 7033 Module Location - Front view of wall-mounted section
©1999 Navia Aviation AS
PHYSICAL ORGANIZATION
2-11
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
System description
This chapter gives a functional overview of the NM70xx ILS systems.
3.1
Overview
The complete ILS electronic system is housed in a compact, wall mounted cabinet. The cabinet and the electronics, except for RF units, are common to the LLZ and GP systems
Monitor
input
signals
Monitor
Transmitter
Remote
Control
NAV
signals
out
External
sensors
RMS
TX control
Comm.
ports
Changeover
Section
Data and
diagnostics
Monitor
input
signals
Transmitter
Monitor
HBK573-1
Figure3-1 ILS block diagram.
The ILS cabinets can be configured for Cat I, Cat II, or Cat III requirements with no basic
changes.
Eight models are available:
NM 7011
Single frequency LLZ
NM 7012
Single frequency LLZ with hot standby monitoring (Cat III)
NM 7013
Two frequency LLZ
NM 7014
Two frequency LLZ with hot standby monitoring (Cat III)
NM 7031
Single frequency GP
NM 7032
Single frequency GP with hot standby monitoring (Cat III)
NM 7033
Two frequency GP
NM 7034
Two frequency GP with hot standby monitoring (Cat III)
The system is based on modern technology with extensive Remote Monitoring and Maintenance capabilities, and very high reliability and integrity. To meet this objective, the monitor
comparator and station control are based on digital hardware, while the RMS interface is
microprocessor based.
3.2
Physical Description
The cabinet contains three sections:
• The electronics card cage
• The change-over section
• The transmitter / PA section
The electronics card cage contains the RF oscillators, the LF signal generators, the monitors,
SYSTEM DESCRIPTION
3-12
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
the station control, the RMS processor, and the voltage regulators.
The change-over section contains coaxial relays, attenuators and phasers for the RF outputs.
The transmitter / PA section contains the PA blocks including couplers etc. for each output.
The cabinet is divided in two parts, with the rear part fixed to a wall, and the front part hinged
to give access to interior of the cabinet.
All external connections are made to the rear part of the cabinet.
3.3
Monitors
The ILS has duplicated monitors with inputs for Course Line (CL), Displacement Sensitivity
(DS), Near Field (NF), and Clearance (CLR) (Dual Freq. only). The signals are detected by
the input stage, and then digitized. In the next block they are filtered by a Fast Fourier Transform performed by a signal processor. The results for each parameter is then compared with
stored limits in a digital hardware comparator.
Each of the two monitors consists of two modules. For Cat III use, Hot Standby monitoring can
be added by using one additional monitor and associated RF couplers and combiners.
The design of the monitors ensures a very high integrity due to the use of digital hardware for
the alarm comparators and a very simple Fast Fourier filtering with a signal processor. In addition, the monitor is checked by automatic self-tests.
The alarm limits are stored locally in EEPROM, and can be updated from the RMS processor,
with a separate hardware write protection to ensure that the integrity is not affected by the
RMS system.
3.4
Transmitters / Modulators
The transmitters are duplicated, either single frequency or dual frequency. Each transmitter
consists of a RF oscillator, a LF generator, and one or two PA blocks (single or dual frequency).
The RF oscillator uses a synthesizer for easy frequency changes and simple logistics. The
oscillator has two outputs for use in dual frequency systems.
The LF generator contains the generators for 90Hz, 150Hz and 1020Hz signals, the ident
keyer / sequencer and interface for DME master or slave keying. All signals are generated by
division from a common clock oscillator, ensuring very stable phase relations between the
modulation signals.
The modulation balance, modulation sum, RF level and Ident morse code are set in this module by means of multiplying digital to analog converters. The values are stored locally in
EPROM and can be updated from the RMS processor with hardware write protection.
The same LF generator is used for single and dual frequency systems.
3.5
TX Control
The TX control unit controls the system dependent on alarms from the monitors and inputs
©1999 Navia Aviation AS
SYSTEM DESCRIPTION
3-13
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
from the local control, the remote control and, optionally, the RMS system. It also generate
status information to the same units. The local control and status indicators are a part of the
TX Control unit.
All functions in the TX Control are based on digital hardware to ensure the highest integrity.
3.6
Remote Monitoring (RMS) Unit
The RMS unit contains the system microprocessor. It handles storage and read-out of monitor
parameters, measurements for maintenance and fault finding, and performs fault analysis to
isolate faults to line replaceable modules. It is also used to set monitor limits and transmitter
adjustments.
The RMM handles communication to local and remote RMS computers, and in addition it handles a small display and keyboard for parameter setting and readout.
3.7
Remote Control Unit
The remote control unit is used in the tower or in the technical control room. It has indicators
for operating status as well as detailed warnings and an aural alarm device with reset. It can
control equipment on/off and change-over, and has an Access Grant-switch to allow remote
control from the RMS system.
The Remote Control Unit is connected to the ILS by one telephone pair cable.
3.8
Remote Slave Panel
The slave panel is connected to the remote control by a multipair wire. It is intended for use in
the control tower. It has indicators for normal / warning / alarm and has an aural alarm device.
in addition it can turn the equipment on and off, and has an aural alarm reset.
Optionally a slave panel with remote control functionality can be delivered.
3.9
Remote Maintenance Monitoring (RMM)
The NM7000 series has a built-in Remote Maintenance Monitoring system. This system consists of the RMS system, remote PC terminals with the RMM program installed, and the local
keyboard/display. Figure 3-2 illustrates the RMM/RMS systems
SYSTEM DESCRIPTION
3-14
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
RMM
program
RMM
program
RMM
program
Modem
Modem
Modem
Modem
Local
Remote 1
Remote 2
RMS
data bus
Local
parameter
storages
Maintenance
data bus
Local
measuring
points
RMS
hardware
RMS system
RMS
core
program
Local
Keyboard/
Display
NM70xx
HBK 598-1
RMM system
Figure3-2 The NM 7000 series RMM/RMS systems.
The centre of the RMS system is a CPU with the RMS core program. The RMS collects measurements and diagnostic data, and makes them available to the user. The collected information allows easy and cost effective maintenance, fault finding and routine reporting. In
addition, system settings are distributed and parameter readings are collected via the RMS/
CPU.
External personal computers are used for a user-friendly interface to the RMM system. The
equipment has three serial output ports, typically used to connect a local PC, a PC in the airport technical equipment room, and a modem for connection to a central maintenance facility.
©1999 Navia Aviation AS
SYSTEM DESCRIPTION
3-15
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
The local keyboard/display allow readings and control through an LCD display and a sevenbutton keypad. This gives access to the RMM functionality without the need for a PC.
3.9.1
RMM Access
Access to the RMM system is controlled by multiple hardware and software access controls.
One password is required for each access level, i.e. one password for level 1, two for level 2
and three for level 3. Optional hardware controls may inhibit writing in the upper access levels.
Access level 1
• Readout of all the monitor values, warning and alarm limits.
• Readout of all the maintenance values and warning limits.
• Readout of all the delays.
• Readout of all the monitor DDM offsets.
Access level 2
• TX1 and TX2: 90/150 Hz on/off.
• TX1 and TX2: morse normal, continuous, TST or off.
• TX1 and TX2: test-signal 90 Hz or 150 Hz dominance on/off.
• Diagnostics.
Access level 3
• Settings of all the monitor warning and alarm limits.
• Settings of all the maintenance warning limits.
• Settings of all the delays.
• Settings of all the monitor DDM offsets.
3.9.2
Local Keyboard/Display Functions
Through a menu-based interface all main commands, adjustments and monitor limits are
accessible from the front panel keypad and LCD display. In addition a quick-read function
gives read-out of all main monitor parameters in a glance.
SYSTEM DESCRIPTION
3-16
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
Figure3-3 Local Control Panel
3.9.3
Diagnostic functions
The system contains internal measuring points and diagnostic functions to isolate faults to
failed modules. The values measured are referred to as maintenance parameters. Please
refer to the NM70xx Operating Manual.
©1999 Navia Aviation AS
SYSTEM DESCRIPTION
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GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
Electrical Installation
This paragraph describes the external electrical connections of the NM 7033 main cabinet.
4.1
Connection Overview
The ILS main cabinet consists of three connector sites, illustrated in Figure 4-1
• The ILS RF signals to and from the antenna system are connected at the top of the main
cabinet. These connectors may be moved to the bottom, see Mechanical Installation.
• The power supply (supplies) and the backup battery are connected to the power connector
rail inside the cabinet back section.
• All other external connections are sited on the Connection Interface board CI1210A inside
the cabinet back section.
POWER RAIL CONNECTIONS
POWER
+27V
SUPPLY
0V
+27V
BATTERY
0V
CI 1210A CONNECTIONS
4 DC LOOPS
3 RS 232
1 REMOTE CONTROL
1 DME
2 TEMP SENSORS
1 AC LEVEL MEASUREMENT
3 DIFFERENTIAL ANALOG
CABLE FEEDTHROUGH
8 DIGITAL INPUT/OUTPUT
RF CONNECTIONS
NF
IN
DS
CL
CLR
COU/CSB
COU/SBO
OUT
HBK574-2
CLR/CSB
CLR/SBO
Figure4-1 ILS main cabinet connection overview.
4.2
Power and Battery
The power supply and the backup battery are connected to the power connector rail inside the
cabinet back section as shown in Figure 4-2. If two power supplies are used, these are parallel
ELECTRICAL INSTALLATION
4-18
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
coupled outside the cabinet. The cables used should have 4mm2 intersection.
Fuse 27AT
0V
+27V
0V
+27V
+27V
Modem
Power Supply
Battery
HBK576-3
Figure4-2 Power and backup battery connections.
A DC powered modem or other external equipment designed for 22V - 27V DC can be connected to the fused terminal block marked Modem. Maximum current consumption should be
1 A.
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-19
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.3
RF Inputs
The RF inputs are:
• Course Line - CL.
• Near Field Antenna - NF.
• Displacement Sensitivity - DS.
• Clearance - CLR (two frequency applications only).
These are connected as shown in Figure 4-3 (front view).
HBK577-2
NF
CL
CLR
DS
Figure4-3 RF input connections.
4.4
RF Outputs
The RF outputs are sited at the cabinet top as illustrated in Figure 4-4. The connections are:
All applications:
• COU SBO - COUrse Tx SideBand Only.
• COU CSB - COUrse Tx Carrier and SideBand.
Two frequency applications:
• CLR SBO - CLeaRance Tx SideBand Only.
• CLR CSB - CLeaRance Tx Carrier and SideBand
HBK578-3
CLR
SBO
CLR
CSB
SBO
CSB
Figure4-4 RF output connections.
ELECTRICAL INSTALLATION
4-20
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
4.5
DC Loop
The DC loops are connected to the Connection Interface board CI1210A in the cabinet back
section. Location and pin out are illustrated in Figure 4-5
• DL_REF* are the reference voltages from the main cabinet.
• DL_DETECT* are the return voltages from the antennas.
• GND is main cabinet ground.
Suitable female connectors are Weidemüller BLZ-5.08/6 or equivalent.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
TEMP
INDOOR
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI 1210A
LOCAL
REMOTE 2
CH.1&2
REMOTE 1
CH.3&4
HBK579-2
DC-LOOP
1 - Ch 1 In
RADIO LINK
DC-LOOP
1 - Ch 3 In
2 - Ch 1 Out
2 - Ch 3 Out
3 - GND
3 - GND
4 - Ch 2 In
4 - Ch 4 In
5 - Ch 2 Out
5 - Ch 4 Out
6 - GND
CH.1&2
6 - GND
CH.3&4
Figure4-5 DC loop connections.
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-21
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.6
Remote Control
The remote control is connected to the Connection Interface board CI1210A as illustrated in
Figure 4-6. The connection of the remote control, remote slave panel and interlock switch is
done at the remote control site and covered in chapter 4.12 - 4.14
• FSK_[P,N] is the modem line pair.
• GND is main cabinet ground.
For normal FSK modem operation the straps S9-11 on CI1210A should be mounted.
A suitable female connector is Weidemüller BLZ-5.08/4 or equivalent.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
TO MB1203
TEMP
INDOOR
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
S9-14
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI1210A
LOCAL
REMOTE 2
REMOTE 1
CH.1&2
CH.3&4
REMOTE
CONTROL
HBK580-1
RADIO LINK
1 - GND
2 - FSK_P
3 - FSK_N
4 - GND
Figure4-6 Remote control connection.
ELECTRICAL INSTALLATION
4-22
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
4.7
PC and Modem
PC terminals and modems are connected to the standard pin out RS232, 9 pins DSUB connectors on the Connection Interface board CI1210A as illustrated in Figure 4-7
Recommended connections are:
• LOCAL - the PC located at the ILS main cabinet site.
• REMOTE 1 - the PC located at the airport technical maintenance site.
• REMOTE 2 - distant PC terminals connected through a modem.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
TEMP
INDOOR
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI1210A
LOCAL
REMOTE 2
REMOTE 1
CH.1&2
RADIO LINK
CH.3&4
1 - CD (REMOTE 2 only)
2 - RXD
3 - TXD
4 - DTR (REMOTE 2 only)
5 - GND
6 - DSR (REMOTE 2 only)
7 - RTS
8 - CTS
9 - Not connected
HBK581-1
Figure4-7 PC and modem connections.
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-23
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.8
DME
Distance Measurement Equipment DME is connected to the Connection Interface board
CI1210A as illustrated in Figure 4-8
• ACT_DME[P,N] is the positive and negative terminal of the DME active signal from the
DME, respectively.
• IN_DME[P,N] is the positive and negative terminal of the morse code envelope signal from
the DME, respectively.
• OUT_DME[P,N] is the positive and negative terminal of the morse code envelope signal to
the DME, respectively.
A suitable female connector is Weidemüller BLZ-5.08/6 or equivalent.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
TEMP
INDOOR
S1-8
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI1210A
LOCAL
REMOTE 2
REMOTE 1
CH.1&2
CH.3&4
DME
1 - ACT_DMEP
RADIO LINK
2 - ACT_DMEN
3 - IN_DMEP
4 - IN_DMEN
5 - OUT_DMEP
6 - OUT_DMEN
HBK582-1
Figure4-8 DME connections.
ELECTRICAL INSTALLATION
4-24
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
4.9
Analog Inputs
The analog inputs are connected to the Connection Interface board CI1210A as illustrated in
Figure 4-9
The inputs are:
• ANALOG CH.1-3 - three differential DC analog inputs, P is the positive and N is the negative terminal.
Maximum voltage: ±15V
Input impedance: 10kohms.
• TINDOOR, TOUTDOOR - temperature measurement inputs with interface to an LM35 temperature sensor.
Maximum voltage: ±15V.
Input impedance: 10kohms.
• AC LEVEL - AC level measurement input. Intended for use with a battery eliminator (i.e.
220/9VAC) to monitor the mains voltage.
Maximum voltage: 24Vpp.
Input impedance: 10kohms.
Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.
TEMP
INDOOR
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
DIGITAL
PORT A
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI1210A
LOCAL
REMOTE 2
REMOTE 1
AC
LEVEL
TEMP
RADIO LINK
1 - VDD
V+
Vtemp
GND
2 - T*DOOR
LM35
Bottom
view
CH.1&2
3 - GND
4 - Not connected
CH.3&4
ANALOG
CH.*
1 - VACP
1 - ANLG*P
2 - GND
2 - GND
3 - VACN
3 - ANLG*N
4 - Not connected
4 - Not connected
HBK583-1
Figure4-9 Analog input connections.
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-25
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.10
Digital Inputs and Outputs
Eight bidirectional digital channels (numbered 0-7) are located on the Connection Interface
board CI1210A as illustrated in Figure 4-10
Logic levels: TTL.
Input impedance: 560ohms.
Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
TEMP
INDOOR
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI1210A
LOCAL
REMOTE 2
RADIO LINK
REMOTE 1
CH.1&2
DIGITAL
PORT A
DIGITAL
PORT B
CH.3&4
DIGITAL
PORT C
DIGITAL
PORT D
1 - USER_DIG1
1 - USER_DIG3
1 - USER_DIG5
1 - USER_DIG7
2 - GND
2 - GND
2 - GND
2 - GND
3 - USER_DIG0
3 - USER_DIG2
3 - USER_DIG4
3 - USER_DIG6
4 - GND
4 - GND
4 - GND
4 - GND
HBK575-1
Figure4-10 Digital input/output connections.
ELECTRICAL INSTALLATION
4-26
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
4.11
Battery Warning
Two inputs for main power supply failure (backup battery active) are sited on the CI1210A
connection interface board as illustrated in Figure 4-11
Logic levels: Normally high 5V or 0V =battery warning.
Input impedance: 10kohms.
Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.
TEMP
OUTDOOR
AC
LEVEL
ANALOG
CH.1
ANALOG
CH.2
ANALOG
CH.3
DIGITAL
PORT A
DIGITAL
PORT B
DIGITAL
PORT C
DIGITAL
PORT D
TO MB1203
TEMP
INDOOR
RS232
RS232
RS232
BATTERY
WARNING
REMOTE
CONTROL
DC-LOOP
DC-LOOP
DME
CI 1210A
LOCAL
REMOTE 2
CH.1&2
REMOTE 1
CH.3&4
BATTERY
WARNING
RADIO LINK
1 - BATT.WARN. CHARGER 1
2 - GND
3 - BATT.WARN. CHARGER 2
HBK602-2
4 - GND
Figure4-11 Battery warning connections.
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-27
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.12
Remote control connections
The remote control is connected to the corresponding ILS by connecting the REMOTE CONTROL connector on Connection Interface CI1210 to P9 on Motherboard MB1346, as shown in
Figure 4-12.
Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent. 600 ohms cable
should be used.
REMOTE
CONTROL
NORMARC
P9
MB1346
1 - GND
1 - TXOFF
2 - FSK_P
2 - ALARM
TXOFF
3 - FSK_N
3 - LINE_A
ALARM
4 - GND
4 - LINE_B
J2
P3
P9
J1
LINE A
LINE B
P10
RX A
CI1210
on
corresponding
ILS
or
CI 1376
on
corresponding
Marker Beacon
RX B
10
TX A
TX B
SLAVE RS485
15
P8
INTERLOCK
ALT.LINK
SLAVE
DIRECT
AUX IN/OUT
20
P6
P7
25
P5
GND
OPTO OUT
P4
GND
1-ALARM (C)
30
2-ALARM (E)
5V
3-NORM (C)
5V
4-NORM (E)
5-WARN (C)
24V
24V
6-WARN (E)
7-STBAL (C)
V_DIM
V_DIM
8-STBAL (E)
POWER OUT
POWER IN
HBK772-2
Figure4-12 Remote control to ILS connection
The power supply to the remote control is connected according to Figure 4-13. The battery
charger is connected to P2 on the MB1347 - power supply motherboard. Output connector P3
on MB1347 is connected to input connector P4 on MB1346 - remote control motherboard.
Several MB1346's are serial linked by connecting P5 on one board to P4 on the next.
Suitable female connectors are Weidemüller BLZ-5.08/4 or equivalent.
ELECTRICAL INSTALLATION
4-28
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
NORMARC
NORMARC
MB1346
MB1346
J2
P3
P9
J2
P3
P9
J1
TXOFF
ALARM
ALARM
LINE B
LINE B
P10
LINE A
P10
RX A
NORMARC
LINE A
MB1347
RX A
RX B
RX B
10
10
10
TX A
TX A
TX B
GND
SLAVE RS485
15
INTERLOCK
15
15
P8
From
P2
TX B
SLAVE RS485
ALT.LINK
J1
J1
TXOFF
P8
SLAVE
INTERLOCK
ALT.LINK
DIRECT
24V
SLAVE
24VDC
power
supply
DIRECT
20
AUX IN/OUT
AUX IN/OUT
P6
20
20
P6
POWER IN
S1
25
P7
P7
25
25
V_DIM=24V
P5
GND
OPTO OUT
P5
P4
GND
1-ALARM (C)
30
GND
2-ALARM (E)
5V
V_DIM
POWER OUT
P3
P4
GND
30
GND
30
2-ALARM (E)
5V
3-NORM (C)
5V
4-NORM (E)
24V
OPTO OUT
1-ALARM (C)
5V
3-NORM (C)
5V
4-NORM (E)
5-WARN (C)
24V
6-WARN (E)
24V
24V
5-WARN (C)
24V
6-WARN (E)
7-STBAL (C)
V_DIM
8-STBAL (E)
POWER IN
V_DIM
POWER OUT
7-STBAL (C)
V_DIM
8-STBAL (E)
POWER IN
V_DIM
POWER OUT
HBK773-1
Figure4-13 Remote control power supply connections
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-29
GENERAL DESCRIPTION
NORMARC 7033
INSTRUMENT LANDING SYSTEM
4.13
Remote slave connection
The remote slave panel SF1344 is connected to the corresponding remote control's motherboard by connecting P3 on MB1346 to P1 on SF1344. P10 on MB1346 is not used. See Figure 4-14.
Suitable connectors are standard 25 pins female DSUB (Harting 0967 025 0442 and 0967 225
4704 or equivalent), connected by a 10 wire 1:1 cable.
NORMARC
MB1346
J2
P3
P9
J1
TXOFF
ALARM
LINE A
To P1
on
SF1344
LINE B
P10
1:1
RX A
RX B
10
TX A
TX B
SLAVE RS485
15
P8
INTERLOCK
ALT.LINK
SLAVE
DIRECT
AUX IN/OUT
20
P6
25
P7
P5
GND
OPTO OUT
13 25
P4
GND
1-ALARM (C)
30
2-ALARM (E)
5V
5V
3-NORM (C)
4-NORM (E)
5-WARN (C)
24V
24V
1 - GND
2 - ALARM
3 - WARNING
4 - NORMAL
7 - GND
15 - V24P
19 - ON_OFF
21 - SILENCE
23 - INTERLOCK (if used)
25 - BUZZER
6-WARN (E)
7-STBAL (C)
V_DIM
V_DIM
8-STBAL (E)
POWER OUT
POWER IN
14
HBK 774-1
Figure4-14 Remote slave connection
ELECTRICAL INSTALLATION
4-30
©1999 Navia Aviation AS
NORMARC 7033
GENERAL DESCRIPTION
INSTRUMENT LANDING SYSTEM
4.14
Interlock switch connection
The interlock switch is either connected to P8 on MB1346 (remote control motherboard) or to
P2 on SF1344 (remote slave panel), see Figure 4-15.
MB1346 / P8
OR
SF1344 / P2
INTERLOCK
SWITCH
RWYA
RWYB
1 INTERLOCK
2 GND
LLZ runway A
LLZ runway B
GP runway A
GP runway B
HBK775-2
Figure4-15 Interlock switch connection
Note:
When MB1346A is used with Remote Control Assembly RCA1240C or D and Interlock function is not used (connected), a jumper plug must be installed in P8 (or P2).
©1999 Navia Aviation AS
ELECTRICAL INSTALLATION
4-31

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