Garmin AT SL-70 Mode C Transponder User Manual Install manual
Garmin AT, Inc. Mode C Transponder Install manual
Contents
- 1. Operation manual
- 2. Install manual
Install manual
Apollo
Mode A/C Transponder
Model SL70
Installation Manual
Final Draft
August 11, 1999
August 1999 560-0402-00
1999 by UPS Aviation Technologies. All rights reserved.
Printed in the U.S.A.
No part of this document may be transmitted, reproduced, or copied in any form or by any means
without the prior written consent of UPS Aviation Technologies. Due to our commitment to
constantly improve the quality and performance of our products, information contained in this
document is subject to change without notice.
UPS Aviation Technologies and Apollo are registered trademarks of UPS Aviation
Technologies.
UPS Aviation Technologies 2345 Turner Rd. S.E.
P.O. Box 13549 Salem, OR 97302
Salem, OR 97309 U.S.A.
Phone (503)581-8101
1-800-525-6726
In Canada 1-800-654-3415
FAX (503)364-2138
HISTORY OF REVISIONS
Revision Date Description
Draft 8/11/99 Final draft.
IMPORTANT NOTE
The conditions and tests required for TSO approval of this article are minimum performance
standards. It is the responsibility of those desiring to install this article on or within a specific
type or class of aircraft to determine that the aircraft operating conditions are within TSO
standards. The article may be installed only if further evaluation by the applicant documents
an acceptable installation and is approved by the Administrator.
ORDERING INFORMATION
To receive additional copies of this publication, order part # 560-0402, Apollo SL70 Mode
A/C Transponder Installation Manual.
REFERENCE PUBLICATIONS
Following are other publications referenced in this guide.
NOTES
Table of Contents
Apollo SL70 Installation Manual i
TABLE OF CONTENTS
SECTION 1 - INTRODUCTION.................................................................................................1
ABOUT THIS MANUAL......................................................................................................................1
APOLLO SL70 DESCRIPTION.............................................................................................................1
FEATURES.........................................................................................................................................2
REGULATORY COMPLIANCE .............................................................................................................2
UNPACKING THE EQUIPMENT............................................................................................................3
PACKAGE CONTENTS........................................................................................................................3
OTHER REQUIRED MATERIALS .........................................................................................................3
SPECIAL TOOLS REQUIRED ...............................................................................................................4
SECTION 2 - INSTALLATION..................................................................................................5
PRE-INSTALLATION INFORMATION....................................................................................................5
INSTALLATION OVERVIEW................................................................................................................5
INSTALLATION CONSIDERATIONS......................................................................................................5
MOUNTING CONSIDERATIONS.................................................................................................................................... 5
MINIMUM SYSTEM CONFIGURATION ......................................................................................................................... 5
ALTITUDE INPUT........................................................................................................................................................ 5
ANTENNA .................................................................................................................................................................. 6
EQUIPMENT MOUNTING....................................................................................................................6
UNIT INSTALLATION / REMOVAL ............................................................................................................................... 7
ELECTRICAL CONNECTIONS..............................................................................................................7
POWER ...................................................................................................................................................................... 8
ALTITUDE INPUT........................................................................................................................................................ 8
SERIAL INTERFACE .................................................................................................................................................... 8
DISCRETE INPUTS ...................................................................................................................................................... 8
ANTENNA INSTALLATION AND CONNECTIONS ..................................................................................9
POST INSTALLATION CHECKOUT.....................................................................................................12
TEST MODE CHECKOUT AND SETUP........................................................................................................................ 12
OPERATION / PERFORMANCE CHECKOUT ................................................................................................................ 13
SECTION 3 - SPECIFICATIONS.............................................................................................15
ELECTRICAL ...................................................................................................................................15
PHYSICAL .......................................................................................................................................15
ENVIRONMENTAL ...........................................................................................................................16
ALTITUDE INPUT.............................................................................................................................16
DISCRETE INPUTS ...........................................................................................................................16
SERIAL INTERFACE .........................................................................................................................16
TRANSPONDER PERFORMANCE.......................................................................................................17
ANTENNA REQUIREMENTS..............................................................................................................17
SECTION 4 - LIMITATIONS...................................................................................................19
INSTALLATION ................................................................................................................................19
OPERATIONAL ................................................................................................................................19
APPENDIX A - TROUBLESHOOTING..................................................................................21
CONTACTING THE FACTORY FOR ASSISTANCE................................................................................22
Table of Contents
ii Apollo SL70 Installation Manual
APPENDIX B - PERIODIC MAINTENANCE ....................................................................... 23
BIENNIAL CHECK ........................................................................................................................... 23
CLEANING THE FRONT PANEL ........................................................................................................ 23
APPENDIX C - ENVIRONMENTAL QUALIFICATIONS.................................................. 25
APPENDIX E - SERIAL DATA PROTOCOL........................................................................ 27
ALTITUDE INPUT / OUTPUT ......................................................................................................................................27
LIST OF TABLES
TABLE 1 PACKAGE CONTENTS ........................................................................................................ 3
TABLE 2 REAR CONNECTOR PINOUT............................................................................................. 18
TABLE 3 TROUBLESHOOTING GUIDE............................................................................................. 21
TABLE 4 ALTITUDE DATA FORMAT............................................................................................... 27
LIST OF FIGURES
FIGURE 1 SL70 FRONT PANEL ........................................................................................................ 2
FIGURE 2 MOUNTING FRAME ASSEMBLY........................................................................................ 6
FIGURE 3 CABLE ROUTING.............................................................................................................. 7
FIGURE 4 COAX CABLE ASSEMBLY................................................................................................. 9
FIGURE 5 WIRING DIAGRAM - GRAY CODE ALTITUDE INPUT ....................................................... 10
FIGURE 6 WIRING DIAGRAM - SERIAL ALTITUDE INPUT................................................................ 11
FIGURE 7 UNIT DIMENSIONS ......................................................................................................... 15
Introduction
Apollo SL70 Installation Manual 1
SECTION 1 - INTRODUCTION
ABOUT THIS MANUAL
This manual describes the installation of the Apollo SL70 transponder . It is intended for use
by persons certified by the Federal Aviation Administration (FAA) to install aircraft avionics.
Provides an introduction to the Apollo SL70 unit. TSO certification information
is also included in this section.
Includes installation and checkout procedures.
Includes complete specifications.
Includes limitations for the equipment and installation.
Includes troubleshooting information.
Includes periodic maintenance requirements.
Includes the environmental qualification form.
Includes serial data protocol specifications.
APOLLO SL70 DESCRIPTION
The Apollo SL70 is a TSO-C74c, Class A2, mode A/C transponder. The SL70, in addition to
providing replies to ATC interrogations, includes an altitude display and altitude hold function
and user-friendly interface features including rotary knob squawk code selection, a VFR
button, and built-in self-test and diagnostics.
Section 1
Section 2
Section 3
Section 4
Appendix A
Appendix B
Appendix C
Appendix E
Introduction
2 Apollo SL70 Installation Manual
Figure 1 SL70 Front Panel
FEATURES
• small size 1.3” panel height
• full range input supply voltage
• high brightness LED display
• altitude display
• altitude hold function
• gray code or RS-232 serial data altitude input
• RS-232 altitude data output
• built-in self-test and diagnostics
REGULATORY COMPLIANCE
The Apollo SL70 is designed and tested to meet the following TSO:
• FAA TSO-C74c, Class A2
The SL70 complies with the FCC requirements specified in:
• CFR 47, Part 87, Aviation Services, Subpart D, Technical Requirements
The SL70 software is designed and tested to RTCA/DO-178B, level C.
Note: Un-authorized changes or modifications to the SL70 may void the
compliance to regulatory agency requirements and authorization for continued
equipment usage.
Introduction
Apollo SL70 Installation Manual 3
UNPACKING THE EQUIPMENT
Carefully unpack the equipment. Visually inspect the package contents for any evidence of
shipping damage. Retain all shipping containers and packaging material in case reshipment is
necessary.
PACKAGE CONTENTS
As shipped from the UPS Aviation Technologies factory, the Apollo SL70 package includes
most necessary items for installation other than supplies normally available at the installation
shop, such as wire and coax cable, the antenna, or any optional switches. The items included
in the package are listed in Table 1.
Table 1 Package Contents
Part # Description Qty
Apollo SL70 Installation Kit, Part # 424-0306-xx
162-0103 37 pin dsub connector shell 1
162-0043 Right angle coax plug 1
202-0001 Cable tie 2
204-0037 Edge grommet 6”
221-0400 4-40 x ¼ SS pan head Phillips machine screw with lock
washer 10
224-0404 4-40 x ¼ flat head Phillips machine screw 2
240-0008 9/16 OD flat washer 1
245-0022 Crimp contact for dsub, 20 to 24 awg wire 37
265-0007 7/16” retaining ring 1
310-2295-00 Connector mounting bracket 1
310-5181-00 Mounting frame 1
998-0048 3/32 hex driver 1
Apollo SL70 Manual Kit, Part # 564-0072-xx
560-0401-00 SL70 User’s Manual 1
560-0402-00 SL70 Installation Manual 1
OTHER REQUIRED MATERIALS
In addition to the materials supplied with the SL70, the following is required.
• a suitable 2A circuit breaker
• an altitude data source – either gray code or RS232
• a standard transponder antenna
Introduction
4 Apollo SL70 Installation Manual
SPECIAL TOOLS REQUIRED
Crimp Tool
A crimp tool meeting MIL specification M22520/1-01 and a positioner are required to ensure
consistent, reliable crimp contact connections for the rear 37 pin dsub connector. These tools
are available from:
Astro Tool Corp. Phone (503)642-9853
21615 SW TV Highway Fax (503)591-7766
Beaverton, OR 97006
Crimp tool: Astro Tool part #615708
Positioner: Astro Tool part #616356
Installation
Apollo SL70 Installation Manual 5
SECTION 2 - INSTALLATION
This section describes the installation of the Apollo SL70 including mounting, wiring, and
connections. A post installation check-out procedure is included at the end of this section.
PRE-INSTALLATION INFORMATION
Always follow good avionics installation practices per FAA Advisory Circulars AC 43.13-1B,
43.13-2A, or current FAA guidance.
Follow the installation procedure in this section as it is presented for a successful installation.
Read the entire section before beginning the procedure. Perform the post installation check-
out before closing the work area in case problems occur.
INSTALLATION OVERVIEW
A successful installation should start with careful planning including determination of
mounting location for the SL70, antenna location and mounting, connections to an altitude
data source, power, cable routing, and other required modifications.
Once the mounting location has been determined, prepare the mounting frame for installation.
If may be easier to complete the wiring harness and attach the connectors to the mounting
frame prior to installing the mounting frame in the aircraft.
INSTALLATION CONSIDERATIONS
MOUNTING CONSIDERATIONS
The SL70 is designed to mount in the avionics stack in the aircraft instrument panel within
easy view and reach of the pilot. The standard package includes the mounting frame for ease
of mounting, connections, and service of the unit. Allow an additional one inch clearance to
the rear of the mounting frame for connections and cables.
For typical installations, the SL70 does not require external cooling. When mounting the unit,
leave a clearance of 1/8 to 1/4 inch between avionics to allow for air circulation.
MINIMUM SYSTEM CONFIGURATION
The SL70 requires connections to the following equipment as a minimum:
• power input
• altitude data – gray code or RS232
• a standard transponder antenna
ALTITUDE INPUT
The SL70 can use either a standard altitude gray code input from an encoding altimeter or an
RS-232 input from a serial encoder. For new installations, a serial encoder is recommended
because it simplifies the wiring and is more reliable. The SL70 can detect failures on the RS-
232 input, thereby eliminating erroneous mode C altitude replies.
Installation
6 Apollo SL70 Installation Manual
The altitude source must be accurate to within ±125 feet, 95% probability, and have a
resolution of 100 feet (the serial input resolution may be better than 100feet).
ANTENNA
The antenna shall be a standard transponder quarter wave monopole antenna, such as the TED
#104-12 or Comant CI-101.
EQUIPMENT MOUNTING
Once the cable assemblies have been made, attach the 37 pin dsub and coaxial cable
connectors to the rear connector mounting plate and the mounting frame as illustrated in
Figure 2 and Figure 3. Route the wiring bundle as appropriate. The rear connector plate should
be attached to the mounting frame before installing the frame in the instrument panel. The rear
connector plate can be used to tie down the cable assemblies. Connect the shields on any
shielded cables directly to the connector mounting plate.
Figure 2 Mounting Frame Assembly
Installation
Apollo SL70 Installation Manual 7
Figure 3 Cable Routing
Once the cable assemblies are complete and the connectors are attached to the mounting
frame, install the mounting frame assembly in the aircraft instrument panel. Be sure to use low
profile head screws so the unit will slide in and out freely. Attach the front of the mounting
frame to the instrument panel. Use support brackets to attach the rear of the frame to the
aircraft.
UNIT INSTALLATION / REMOVAL
To install the SL70 in the mounting frame, make sure the cam lock is rotated so the rear part
is up, then slide the unit into the frame and tighten with the 3/32 hex tool. The unit will be
pulled into the frame by the cam lock and the connectors will fully engage.
To remove the SL70 from the mounting frame, use the hex tool and turn the tool CCW. The
unit will be pushed out of the frame by the cam lock assembly. No special extraction tools are
required.
ELECTRICAL CONNECTIONS
The SL70 installation kit includes a 37 pin dsub shell and crimp contacts. The crimp contacts
are specified for 20 to 24 AWG wire. Make the crimp connections with a crimp tool as
specified in the Special Tools Required section on page 4. All wires should be 20 to 24 AWG
unless otherwise specified. Wiring diagrams are included on pages 10 and 11.
Installation
8 Apollo SL70 Installation Manual
POWER
The SL70 is internally fused at 3 amps. A separate 2 amp circuit breaker or fuse should be
installed for downline overload or short circuit protection. Make the power connections to the
SL70 using 20 AWG wire.
Note: Circuits should be protected in accordance with guidelines in AC 43.13-1B, chapter 11,
section 4.
ALTITUDE INPUT
If using the gray code altitude input, connections can be made directly from the SL70 to the
altitude source. Isolation diodes are included within the SL70. Make sure a common ground
connection exists, or connect a ground wire between the source and the SL70.
If using the RS-232 serial altitude input, make the connections as described in the following
section.
SERIAL INTERFACE
The SL70 includes an RS-232 serial port which can be used for inputting or outputting
altitude data. This is an optional connection if the altitude gray code input is used.
When making serial connections to the SL70, use a shielded two or three conductor cable.
Make the RxD, TxD, and serial ground connections on the 37 pin dsub connector. Connect the
shield to the rear of the mounting frame on the connector plate.
Complete serial interface specifications are included in Appendix E.
DISCRETE INPUTS
Remote Ident
The ident input can be connected to a remotely mounted momentary switch to initiate the
ident function the same as using the front panel IDENT button.
When using the ident input, connect it to a remotely mounted momentary switch, and connect
the other terminal of the switch to ground.
Remote Standby
The standby input is for use when the installation includes more than one transponder. When
two transponders are installed, connect the standby input to a two position selector switch,
with the common on the switch connected to ground. The SL70 will be in standby when the
input is pulled low to ground.
Suppresion Input
The suppress input is used when installed with a DME that includes a suppression output. The
transponder will be suppressed, or will not generate replies, when the input is driven high
from the DME (or other source). To use the suppression input, connect it to the suppression
output on a DME (or other appropriate suppression source).
Installation
Apollo SL70 Installation Manual 9
ANTENNA INSTALLATION AND CONNECTIONS
The antenna should be mounted in a vertical position in an area on the bottom of the aircraft
away from other antennas or landing gear.
The antenna coax cable should be a double shielded low loss cable and must have a cable loss
of < 3 dB, including connectors. A typical installation should have a cable loss of 1½ to 2 dB.
Several suitable coaxes are RG142B and RG400.
The assembly of the rear panel coax connector included with the installation kit is illustrated
in the following figure.
0.125
Insulation
1.000
STEP 1
Cable
Shrink
Tube
Matching Ring
Cap
STEP 3
STEP 4
-Slide shrink tube over cable.
-Strip cable as shown.
Solder Center
Conductor
-Solder cap into place, 2 Places.
-Shrink tube as shown.
Solder Cap
2 Places
STEP 2
.125
Shield 0.250
-Flare Outer Shield as Shown
Solder Outer Shield
to Connector -Place cable in connector as shown placing inner
shield inside connector.
-Flatten outer shield against connector.
-Solder outer shield to connector.
-Solder center conductor
-Slide matching ring into connector and around
conductor.
-Attach cap.
Figure 4 Coax Cable Assembly
Installation
10 Apollo SL70 Installation Manual
1
2
Power
Ground
C4
C2
C1
B4
B2
B1
A4
A2
A1
D4
15
34
16
32
14
33
12
31
13
35
30Ground
Standby
Ident
Suppress
Ground
Ground
TxD
RxD
C4
C2
C1
B4
B2
B1
A4
A2
A1
D4
Ground
SL70
Transponder
10
29
19
37
5
4
3
Chassis Ground
Avionics
Power
+
-
2A Breaker
Altitude
Encoder or
Digitizer
Shielded Cable
Remote
Ident
(Optional)
To Antenna
Coax Cable
RS-232 Serial Altitude
Output (Optional)
Note 2 (Optional)
Note 3 (Optional)
Notes:
2. Use standby input to select between two transponders using a selector switch.
Unit is in standby when input switched to ground.
3. Suppression input, typically connected to DME suppression output. Transponder is
suppressed when input is high.
RxD
Ground
Chassis Ground
GPS Unit
1. Select the gray code input in the setup mode when using the parallel gray code
altitude input.
Suppress return
Figure 5 Wiring Diagram - Gray Code Altitude Input
Installation
Apollo SL70 Installation Manual 11
1
2
Power
Ground
C4
C2
C1
B4
B2
B1
A4
A2
A1
D4
15
34
16
32
14
33
12
31
13
35
30Ground
Standby
Ident
Suppress
Ground
Ground
TxD
RxD
SL70
Transponder
10
29
19
37
5
4
3
Chassis Ground
Avionics
Power
+
-
2A Breaker
Shielded Cable
Remote
Ident
(Optional)
To Antenna
Coax Cable
RS-232 Serial Altitude Input
Note 2 (Optional)
Note 3 (Optional)
Notes:
2. Use standby input to select between two transponders using a selector switch.
Unit is in standby when input switched to ground.
3. Suppression input, typically connected to DME suppression output. Transponder is
suppressed when input is high.
TxD
Ground
Chassis Ground
1. Select altitude input in the setup mode when using RS-232 serial altitude input.
Altitude
Encoder or
Serializer
Suppress return
Figure 6 Wiring Diagram - Serial Altitude Input
Installation
12 Apollo SL70 Installation Manual
POST INSTALLATION CHECKOUT
Once the unit is installed, complete the checkout procedure to verify proper operation. Refer
to the user’s guide for operating instructions.
The steps that are not applicable to a particular installation may be skipped. A checkout log
sheet is included on page 14 to fill out during the checkout procedure. Make a photocopy of
the log sheet for ease of use if desired.
Mounting / Wiring Check
Verify that all cables are properly secured and shields are connected to the rear of the
mounting frame. Check the movement of the aircraft controls to verify that there is not
interference.
TEST MODE CHECKOUT AND SETUP
The SL70 has a built-in setup mode to simplify the checkout. To operate the SL70 in the setup
mode, hold down the “IDENT” and “ALT” buttons while switching on the power. To return to
normal operation, switch the power off, then back on.
Altitude Input Source Selection
The SL70 altitude input type must be selected. To select the altitude input type:
1. In test mode, rotate the LARGE knob to the “SL70 CONF” (SL70 Configuration) page,
then rotate the SMALL knob to the “ASRC” (Altitude source) page.
2. Press IDENT (the altitude type field will start to flash), rotate the SMALL knob to select
the altitude type, then press IDENT to save the selection.
The altitude types that can be selected are:
GRAY ..................................... to use the parallel gray code input
SER ........................................ to use the RS-232 serial altitude input
RS-232 Baud Rate Selection
If using the RS-232 serial interface, the baud rate must be selected to match the connected
equipment. To select the baud rate:
1. In test mode, rotate the LARGE knob to the “SL70 CONF” (SL70 Configuration) page,
then rotate the SMALL knob to the “BAUD” (baud rate) page.
2. Press IDENT (the baud rate field will start to flash), rotate the SMALL knob to select the
desired baud rate, then press IDENT to save the selection.
The baud rates available are 1200, 2400, 4800, 9600, and 19200.
VFR Code Selection
The VFR code used by the SL70 when pressing the “VFR” button can be selected as
appropriate for the aircraft’s operating area. To change the VFR code:
1. In test mode, rotate the LARGE knob to the “SL70 CONF” (SL70 Configuration) page,
then rotate the SMALL knob to the “VFR” (VFR code selection) page.
2. Press IDENT (the first VFR code character will start to flash).
Installation
Apollo SL70 Installation Manual 13
3. Rotate the SMALL knob to change the character, rotate the LARGE knob to move the
cursor.
4. Press IDENT to save the selection.
OPERATION / PERFORMANCE CHECKOUT
Self Test
The SL70 includes a self test that is executed every time the unit is turned on that checks the
receiver and transmitter operation as well as other internal functions.
Verify that the unit does not display a failure indication when turned on.
Altitude Input
Verify that the displayed altitude matches the altimeter pressure altitude (at 29.92).
External Inputs
If the external ident or standby inputs are connected, verify operation by:
a) Verify that the unit goes to standby when the external standby input is pulled low.
b) Verify that the ident LED turns on when the external ident button is pressed (must be in
the “ON” or “ALT” modes).
Performance (Ramp) Test
After installation, the transponder should be tested as specified in Appendix F of CFR 14 part
43, to AC 43-6A, and/or other appropriate regulations. The test is typically done as a ramp test
using a transponder ramp test set, such as the IFR ATC-600A. The ramp test includes checks
as follows.
Reference part 43 Appendix F:
a) reply frequency
b) suppression
c) receiver sensitivity
d) reply RF output power
Reference AC 43-6A:
• altitude reporting
Installation
14 Apollo SL70 Installation Manual
APOLLO SL70 POST-INSTALLATION CHECKOUT LOG Date: ___/___/___
By: _______________
CONFIGURATION INFORMATION:
Apollo SL70 430-6090-____ Mod ___
Serial #_______________
TEST MODE CHECKOUT AND SETUP:
Self Test:
[ ] Pass
[ ] Fail
Altitude source: RS-232 baud rate: _________
[ ] Gray code (GRAY)VFR Code: ________
[ ] Serial RS-232 (SER)
OPERATION / PERFORMANCE CHECK:
Altitude data (on display): Performance verification:
[ ] Pass [ ] Pass
External inputs:
[ ] Remote ident checked [ ] N/A
[ ] External standby [ ] N/A
COMMENTS:
Specifications
Apollo SL70 Installation Manual 15
SECTION 3 - SPECIFICATIONS
This section includes detailed electrical, physical, environmental, and performance
specifications for the Apollo SL70.
ELECTRICAL
Input voltage .............................................10VDC to 35VDC, reverse polarity protected
Input current..............................................500mA typical, 1.4A max at 14VDC
270mA typical, 660mA max at 28VDC
Input power...............................................7 watts typical (8 pulse reply, 200 replies / second)
20 watts max (12 pulse reply, 1200 replies / second)
5.8 watts standby
Internal fuse ..............................................3 amp slow blow (UPS Aviation Technologies
#S172-0007-012)
Memory backup........................................Internal EEPROM
PHYSICAL
Height .......................................................1.30 inches (3.30 cm)
Width ........................................................6.25 inches (15.88 cm)
Depth ........................................................11.452 inches (29.09cm) behind panel, including
mounting frame and connectors
Weight (with mounting frame).................2.64 lb. (1.2 kg)
Required clearance....................................Allow 3 inches behind unit for connector and cable
clearance
Mounting Holes (8x)
3.6250.375
10.420
11.4520.648
1.6251.7503.025
6.250
1.300
0.219
1.3000.862
1.038
Figure 7 Unit Dimensions
Specifications
16 Apollo SL70 Installation Manual
ENVIRONMENTAL
The Apollo SL70 is designed and tested to meet appropriate categories of RTCA/DO-160D.
The Environmental Qualification Form is included in Appendix C.
Operating temperature.............................. -20°C to +55°C
Storage temperature.................................. -55°C to +85°C
Temperature variation .............................. 2°C per minute
Humidity................................................... 95% at 50°C for 6 hours (2 day cycle)
Maximum altitude .................................... 25,000 feet
Cooling..................................................... Not required
ALTITUDE INPUT
10 bit gray code........................................ Uses 10 bit gray code altitude data, includes
isolation diodes.
Range: -1000feet to 63,000 feet
On: <= 3.5 volts, Off: open
Serial input ............................................... Uses RS-232 serial data input (See Appendix E –
Serial Interface Specifications)
Note: The altitude data input type must be selected using the setup function during the post
installation checkout.
DISCRETE INPUTS
Remote Ident ............................................ Input pulled low momentarily to initiate ident
transmission (same function as front panel button)
On: <= 3.5 volts, Off: open
Standby input............................................ Input pulled low to disable the transponder (will not
generate replies)
On: <= 3.5 volts, Off: open
Suppression input..................................... Input pulled high to initiate suppression – typically
connected to DME suppression output
Suppressed: >= 5.0 volts;
Not suppressed: < 2.5 volts (or open)
SERIAL INTERFACE
RS-232...................................................... Defined in Appendix E – Serial Interface
Specifications
Specifications
Apollo SL70 Installation Manual 17
TRANSPONDER PERFORMANCE
TSO...........................................................TSO-C74c
TSO Class.................................................2A
Warm-up...................................................none required
Receiver Frequency ..................................1030 MHz
Sensitivity (MTL) .....................................–72 dBm
Dynamic Range.........................................> 50 dB
Side Lobe Suppression .............................2 pulse (P1,P2)
Transmitter Frequency..............................1090 MHz +/- 120 kHz
Transmitter Power ....................................250 watts minimum, 325 watts typical
Reply rate..................................................1200 / second
Mode A Capability ...................................4096 codes plus SPI ident pulse
Mode C Capability....................................-1000 to 63,000 feet, 100 foot increments, from
either gray code or RS-232 serial inputs
ANTENNA REQUIREMENTS
The SL70 requires a standard transponder quarter wave monopole antenna, such as the TED
#104-12 or Comant CI-101.
Specifications
18 Apollo SL70 Installation Manual
Table 2 Rear Connector Pinout
Pin # I/O Connection Function
1 I Power + main DC power input
2 I Power ground main DC power ground
3 O Serial ground RS-232 serial ground
4 I RxD RS-232 serial data input
5 O TxD RS-232 serial data output
6 O reserved
7 O reserved
8 I reserved
9 I reserved
10 I Ident remote ident input
11 -- NC no connection
12 I A4 A4 altitude gray code input
13 I A1 A1 altitude gray code input
14 I B2 B2 altitude gray code input
15 I C4 C4 altitude gray code input
16 I C1 C1 altitude gray code input
17 -- reserved
18 -- reserved
19 I Suppress remote suppression input
20 O NC no connection
21 I reserved
22 O reserved
23 -- NC no connection
24 -- Ground
25 I reserved
26 I reserved
27 -- Ground
28 -- Ground
29 I Standby remote standby input
30 -- Ground
31 I A2 A2 altitude gray code input
32 I B4 B4 altitude gray code input
33 I B1 B1 altitude gray code input
34 I C2 C2 altitude gray code input
35 I D4 D4 altitude gray code input
36 -- reserved
37 -- Ground
1
20
19
37
Viewed from rear of unit
Limitations
Apollo SL70 Installation Manual 19
SECTION 4 - LIMITATIONS
INSTALLATION
Aircraft installation must be made in accordance with this installation manual and applicable
FAA FARs and ACs.
OPERATIONAL
The SL70 must be operated within the limitations as follows, or by other regulatory guidance
as appropriate.
1. The altitude should be verified by comparing the pressure altitude display to the aircraft
altimeter relative to barometric setting of 29.92.
2. The transponder is to be operated in compliance with CFR 14 section 91.215 for ATC
transponder and altitude reporting equipment.
3. The transponder must be tested as specified in CFR 14 section 91.413 within the previous
24 months.
Limitations
20 Apollo SL70 Installation Manual
NOTES
Troubleshooting
Apollo SL70 Installation Manual 21
APPENDIX A - TROUBLESHOOTING
This appendix provides information to assist troubleshooting if problems occur after
completing the installation. Use Table 3 to assist in troubleshooting.
Table 3 Troubleshooting Guide
Problem Cause Solution
The SL70 does not power on. The unit is not getting power. Check power connections, breakers,
and main avionics switch.
The altitude is not correct. The unit is not getting the correct
altitude. If the gray code inputs are used,
check all connections from the
altitude source and/or verify the
altitude source.
If the serial altitude input is used,
check for the correct baud rate and
connections to the altitude source.
The altitude display is “---“ The unit is not getting an altitude, or
the altitude is invalid. Check the connections to the altitude
source.
Check the altitude source to make
sure it is operating correctly.
The unit fails the start-up test. TX fails. Check antenna connections.
Other failure. The unit may need repair.
The unit does not generate
replies. The unit is in standby. The unit must be in either the “On” or
“Alt” modes to generate replies.
The unit is not receiving interrogation
signals. Check the antenna connections. If the
unit does not “Fail” the receive test,
then check antenna connections.
No interrogation signal available. Need to either use a ramp test set or
climb to altitude where ATC radar
service is available.
Troubleshooting
22 Apollo SL70 Installation Manual
CONTACTING THE FACTORY FOR ASSISTANCE
If the Apollo SL70 unit fails to operate despite troubleshooting efforts, contact the UPS
Aviation Technologies factory for assistance.
UPS Aviation Technologies
2345 Turner Rd. S.E.
Salem, Oregon 97302
U.S.A.
Phone (503)581-8101 or 1-800-525-6726
Be prepared to offer the following information about the installation:
• Installation configuration (accessories, antenna, ...)
• Model number, part number with mod levels, and serial number
• Software versions (The software versions can be displayed in the setup mode by
rotating the LARGE knob to the “SW VER” page, and rotating the SMALL knob to
display the microcontroller and FPGA versions.)
• Description of problem
• Efforts made to isolate the problem
Periodic Maintenance
Apollo SL70 Installation Manual 23
APPENDIX B - PERIODIC MAINTENANCE
The Apollo SL70 is designed to not require any regular general maintenance except as
included in this section.
BIENNIAL CHECK
The transponder must be tested within the previous 24 months as specified in 91.413 of the
FAA regulations.
No other periodic maintenance is required.
CLEANING THE FRONT PANEL
The front bezel, keypad, and display can be cleaned with a soft cotton cloth dampened with
clean water. DO NOT use any chemical cleaning agents. Extreme care must be taken to avoid
scratching the surface of the display.
Periodic Maintenance
24 Apollo SL70 Installation Manual
NOTES
Environmental Qualifications
Apollo SL70 Installation Manual 25
APPENDIX C - ENVIRONMENTAL QUALIFICATIONS
The Apollo SL70 has been tested to the following environmental categories per procedures
defined in RTCA/DO-160D.
Environmental Qualification Form
Nomenclature: Apollo SL70
Part No.: 430-6090-xxx
TSO No.: TSO_C74c
Manufacturer:
UPS Aviation Technologies
2345 Turner Road S.E.
Salem, Oregon 97302
Conditions Section Description of Conducted Tests
Temperature and Altitude 4.0 Equipment tested to Category B1 with .......
In-flight Loss of Cooling 4.5.4 No cooling required
Altitude 4.6.1 Equipment tested to 25,000 feet
Decompression 4.6.2 Equipment tested for decompression to 35,000 feet
Overpressure 4.6.3 Equipment tested for overpressure
Temperature Variation 5.0 Equipment tested to Category C, 2°C/min
Humidity 6.0 Equipment tested to Category A, standard humidity
environment
Operational Shocks and Crash
Safety 7 Equipment tested for both operational and crash safety
shocks. (Equipment operates normally after both the crash
safety shocks.)
Vibration 8.0 Equipment tested without shock mounts to Categories S(M)
Explosion Proofness 9.0 Equipment identified as Category X, no test required
Waterproofness 10.0 Equipment identified as Category X, no test required
Fluids Susceptibility 11.0 Equipment identified as Category X, no test required
Sand and Dust 12.0 Equipment identified as Category X, no test required
Fungus Resistance 13.0 Equipment identified as Category X, no test required
Salt Spray 14.0 Equipment identified as Category X, no test required
Magnetic Effect 15.0 Equipment is Class Z
Power Input 16.0 Equipment tested to Categories A (28volt systems) & B (14
and 28 volt systems)
Voltage Spike 17.0 Equipment tested to Category A
Audio Frequency Conducted
Susceptibility – Power Inputs 18.0 Equipment tested to Categories A & B
Induced Signal Susceptibility 19.0 Equipment tested to Category Z
Radio Frequency Susceptibility
(Radiated and Conducted) 20 Equipment tested to Category V
Emission of Radio Frequency
Energy 21 Equipment tested to Category M
Lightning Induced Transient
Susceptibility 22.0 Equipment tested to A3 and B2
Lightning Direct Effects 23.0 Equipment identified as Category X, no test required
Icing 24.0 Equipment identified as Category X, no test required
Electrostatic Discharge (ESD) 25.0 Equipment tested to Category A
Remarks:
Environmental Qualifications
26 Apollo SL70 Installation Manual
NOTES
Serial Data Protocol
Apollo SL70 Installation Manual 27
APPENDIX E - SERIAL DATA PROTOCOL
This appendix includes the RS-232 serial port interface specifications.
ALTITUDE INPUT / OUTPUT
The SL70 will output altitude data whenever it is available, either from the gray code or serial
input.
The SL70 will accept altitude input data when the serial altitude data source is selected.
The format for the altitude input and output data is as follows.
Baud rate................................1200 to 19200
Data bits.................................8
Stop bits.................................1
Parity......................................none
Message length ......................17 characters
Expected input rate................once per second
Output rate.............................once per second
Table 4 Altitude Data Format
Byte Data Format Description
1 “#” ASCII “#” (023h)
2 “A” ASCII “A” (041h)
3 “L” ASCII “L” (04Ch)
4 “ “ ASCII space (020h)
5 “+” or “-“ Altitude sign: ASCII “+” or “-“ (02Bh or 02Dh)
6-10 ddddd Altitude in feet, right justified, with leading zeros
11 “T” ASCII “T” (054h)
12 “+” or “-“ Temperature sign: ASCII “+” or “-“ (02Bh or 02Dh)
13-14 dd Altimeter temperature
15-16 dd Checksum of bytes 1 through 14, computed in hex, output is
ASCII format (i.e., “FA” hex)
17 <CR> ASCII carriage return (0Dh)
The SL70 will interpret several altitude input codes as status or error codes, in the place of the
altitude data, as follows.
“-09980” ................................Encoder heater not ready, expected during encoder warm-
up or if there is a loss of signal from the encoder. The SL70
will reply with only framing pulses to mode C
interrogations.
Serial Data Protocol
28 Apollo SL70 Installation Manual
“-09981”................................ Possible hardware problem, expected from the encoder
indicating a temperature above normal. The SL70 will reply
with only framing pulses to mode C interrogations.
“-09982”................................ Altitude out of range, expected from the encoder indicating
that the altitude is out of a valid range. The SL70 will reply
with only framing pulses to mode C interrogations.
When the gray code input is selected, the SL70 will output the “-09982” error code in place of
the altitude data if an undefined altitude input is detected on the gray code input.
Serial Data Protocol
Apollo SL70 Installation Manual 29
NOTES
