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Apollo
Model SL40
VHF COMM Transceiver
Installation Manual
September 1999 560-0956-02a
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1999 by II Morrow Inc. All rights reserved.
Printed in the USA
No part of this document may be transmitted, reproduced, or copied in any form or by any means
without the prior written consent of II Morrow Inc. Due to II Morrow’s commitment to
constantly improve the quality and performance of our products, information contained in this
document is subject to change without notice.
NAVNET and Flybrary are trademarks of II Morrow Inc.
II Morrow and Apollo are registered trademarks of II Morrow Inc.
II Morrow Inc. 2345 Turner Rd., SE
PO Box 13549 Salem, OR 97302
Salem, OR 97309 USA
Phone (503) 581-8101
1-800-525-6726
In Canada 1-800-654-3415
FAX (503) 364-2138
Page 3
HISTORY OF REVISIONS
Revision Date Description
-- 12/18/96 Initial release.
00A 1/30/97 Modified selectivity value to 7 kHz.
-01 3/14/97 Change recommended coax from RG-58 to RG-142B
-02 6/26/98 New software version
-02a 9/22/99 Added new connector pins and crimping tools
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 user/installer
documents an acceptable installation and is approved by the Administrator.”
Source: FAA TSO-C37d, TSO-C38d, and TSO-C128
ORDERING INFORMATION
To receive additional copies of this publication, order part # 560-0956-02a, Apollo SL40 VHF
COMM Installation Manual.
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NOTES
Page 5
Table of Contents
TABLE OF CONTENTS
SECTION 1 - INTRODUCTION.................................................................................................1
ABOUT THIS MANUAL......................................................................................................................1
APOLLO SL40 DESCRIPTION.............................................................................................................1
FEATURES.........................................................................................................................................1
EGULATORY COMPLIANCE .............................................................................................................2
R
U
NPACKING THE EQUIPMENT............................................................................................................3
PACKAGE CONTENTS........................................................................................................................3
OTHER REQUIRED MATERIALS .........................................................................................................4
SPECIAL TOOLS REQUIRED...............................................................................................................4
LICENSE REQUIREMENTS..................................................................................................................4
SECTION 2 - INSTALLATION..................................................................................................5
RE-INSTALLATION INFORMATION....................................................................................................5
P
I
NSTALLATION OVERVIEW................................................................................................................5
INSTALLATION CONSIDERATIONS......................................................................................................5
MOUNTING CONSIDERATIONS.................................................................................................................................... 5
M
INIMUM SYSTEM CONFIGURATION .........................................................................................................................5
EQUIPMENT MOUNTING....................................................................................................................5
ELECTRICAL CONNECTIONS..............................................................................................................7
POWER ......................................................................................................................................................................7
S
PEAKER AND HEADPHONE OUTPUTS ....................................................................................................................... 7
M
ICROPHONE INPUTS ................................................................................................................................................ 7
T
RANSMIT KEY INPUT...............................................................................................................................................7
I
NTERCOM SELECTOR SWITCH .................................................................................................................................. 7
S
ERIAL INTERFACE .................................................................................................................................................... 8
ANTENNA INSTALLATION AND CONNECTIONS ..................................................................................8
POST INSTALLATION CHECKOUT.....................................................................................................12
SECTION 3 - SPECIFICATIONS.............................................................................................15
ELECTRICAL ...................................................................................................................................15
PHYSICAL .......................................................................................................................................15
NVIRONMENTAL ...........................................................................................................................15
E
RECEIVER PERFORMANCE...............................................................................................................16
T
RANSMITTER PERFORMANCE........................................................................................................16
INTERCOM PERFORMANCE..............................................................................................................17
ONTROL INPUTS............................................................................................................................17
C
ANTENNA REQUIREMENTS..............................................................................................................17
S
ERIAL INTERFACE .........................................................................................................................17
REAR CONNECTOR PINOUT.............................................................................................................17
SECTION 4 - LIMITATIONS...................................................................................................19
INSTALLATION ................................................................................................................................19
OPERATIONAL ................................................................................................................................19
APPENDIX A - TROUBLESHOOTING..................................................................................21
ONTACTING THE FACTORY FOR ASSISTANCE................................................................................21
C
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Table of Contents
APPENDIX B - PERIODIC MAINTENANCE ....................................................................... 23
EQUIPMENT CALIBRATION ............................................................................................................. 23
REFERENCE OSCILLATOR.........................................................................................................................................23
CLEANING THE FRONT PANEL........................................................................................................ 23
APPENDIX C - ENVIRONMENTAL QUALIFICATIONS.................................................. 25
APPENDIX E - SERIAL INTERFACE SPECIFICATIONS................................................. 27
RS-232 INPUTS.............................................................................................................................. 27
RS-232 OUTPUTS........................................................................................................................... 29
LIST OF TABLES
TABLE 1 PACKAGE CONTENTS........................................................................................................ 3
TABLE 2 CONNECTOR PINOUT....................................................................................................... 18
TABLE 3 TROUBLESHOOTING GUIDE............................................................................................. 21
LIST OF ILLUSTRATIONS
FIGURE 1 SL40 FRONT PANEL ........................................................................................................ 2
FIGURE 2 MOUNTING FRAME ASSEMBLY........................................................................................ 6
FIGURE 3 CABLE ROUTING.............................................................................................................. 6
FIGURE 4 COAX CONNECTOR ASSEMBLY........................................................................................ 9
FIGURE 5 SL40 STANDALONE WIRING DIAGRAM ......................................................................... 10
FIGURE 6 SL40 TYPICAL AUDIO PANEL CONNECTIONS ................................................................ 11
FIGURE 7 UNIT DIMENSIONS ......................................................................................................... 16
ii Apollo SL40 Installation Manual
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Introduction
SECTION 1 - INTRODUCTION
ABOUT THIS MANUAL
This manual describes the installation of the Apollo SL40 Comm . It is intended for use by
persons certified by the Federal Aviation Administration (FAA) to install aircraft navigation
devices. It includes installation and checkout procedures for the SL40 unit to standards
described in FAA advisory circular AC 20-67B.
Section 1
Section 2
Section 3
Section 4
Appendix A
Appendix B
Appendix C
Appendix E
Provides an introduction to the Apollo SL40 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 specifications.
APOLLO SL40 DESCRIPTION
The Apollo SL40 is a 760 channel VHF Comm transceiver. It is one member of the Apollo
slimline series, which includes the SL40 Comm, the SL50 GPS, and the SL60 GPS/Comm.
FEATURES
The features of the SL40 Comm include:
• 760 channels
• Frequency range of 118.000 to 136.975MHz
• Active and standby frequency display
• 16 character high-intensity alphanumeric LED display
• Automatic display intensity
• Back-lit buttons
• Transmit status indicator
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Introduction
• Frequency memory and recall functions
• Weather channels
• Frequency monitor function
• Built-in intercom function
• Stuck mic time-out
• Two microphone inputs
• Internal non-volatile memory - no battery required
• Full range input supply voltage
• 12 watt audio amplifier
− from remote source
− eight last used
− eight user stored
Figure 1 SL40 Front Panel
REGULATORY COMPLIANCE
The Apollo SL40 is designed and tested to meet the following TSOs:
FAA TSO-C37d for transmit
FAA TSO-C38d for receive
FAA TSO-C128 for unintentional transmission (stuck mic)
The Apollo SL40 complies with the FCC requirements specified in:
CFR 47, Part 87, Aviation Services, Subpart D, Technical Requirements
CFR 47, Part 15, Radio Frequency Devices, Subpart B, Unintentional Radiators
The Apollo SL40 software is designed and tested to RTCA/DO-178B, level C.
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Introduction
The Apollo SL40 meets the additional standards as detailed in the Declaration of Conformity
included on page 31.
Note: Unauthorized changes or modifications to the SL40 may void the compliance to
required regulatory agencies and authorization for continued equipment usage.
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 II Morrow factory, the Apollo SL40 package includes most necessary
items for installation other than supplies normally available at the installation shop, such as
wire and cable ties, and required input and output equipment. The items included in the
package are listed in Table 1.
Table 1 Package Contents
Part # Description Qty
Comm unit
430-6040-2xx Apollo SL40 Comm Transceiver 1
Apollo SL40 Installation Kit, Part # 424-2006-2xx
162-0100 or
162-1575
162-1008 Right angle coax plug 1
202-0001 Cable tie 2
204-2100 Shoulder bushing 2
221-0400 4-40 x 1/4 SS pan head Phillips machine screw with lock washer 8
224-0404 4-40 x 1/4 SS flat head Phillips machine screw 2
245-0022 or
245-0027
310-5181-00 Mounting frame 1
310-5187-00 Connector mounting plate 1
998-0048 3/32 hex driver 1
204-0037 Edge grommet 6”
Apollo SL40 Manual Kit, Part # 564-0064-2xx
560-0954-xx SL40 User’s manual 1
560-0956-xx SL40 Installation manual 1
15 pin dsub connector shell 1
Crimp contact for dsub, 20 to 24 awg wire 15
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Introduction
OTHER REQUIRED MATERIALS
The SL40 is intended for use with standard aviation accessories. The following items are
required for the installation:
• comm antenna with cables
• a microphone
• a speaker or headphone
These items may be installed dedicated to the SL40 comm or by connections to an audio
panel.
SPECIAL TOOLS REQUIRED
Crimp Tool
A crimp tool meeting MIL specification M22520/1-01 and a positioner/locater are required to
ensure consistent, reliable crimp contact connections for the rear d-sub connectors. These tools
are available from:
For pin p/n 245-0022
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
For pin p/n 245-0027
ITT Cannon Phone (714) 261-5300
1851 E. Deere Ave. Fax (714) 575-8324
Santa Ana, CA 92705-6500
Insertion tool: ITT part # 274-7006-000 (Desc. CIET-20HD)
Regular duty Crimp tool: ITT part #995-0001-585 (Desc. M22520/1-01)
Regular duty Locator tool: ITT part #995-0001-244 (Desc. TH25)
Heavy duty Crimp tool: ITT part #995-0001-584 (Desc. M22520/2-01)
Heavy duty Locator tool: ITT part #995-0001-604 (Desc. M22520/2-08)
LICENSE REQUIREMENTS
An aircraft radio station license is required for operation of the transmitter once installed in
the aircraft. An application must be submitted on FCC Form 404, which may be obtained
from the FCC in Washington, DC, or any of its field offices. Procedures for applications are in
CFR 47, Part 87, Aviation Services, Subpart B, Applications and Licenses.
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Installation
SECTION 2 - INSTALLATION
This section describes the installation of the Apollo SL40 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) 43.131A, 43.13-2A, and AC 20-67B, or later FAA approved revisions of these documents.
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 checkout 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 SL40, antenna mounting, connections to microphones, speakers,
and headphones, cable routing, and other required modifications. Once the mounting location
has been determined, prepare the mounting frame for installation. It may be easier to complete
the wiring harness and attach the connectors to the mounting frame before installing the
mounting frame.
INSTALLATION CONSIDERATIONS
MOUNTING CONSIDERATIONS
The SL40 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 a 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 connectors and cables.
For typical installations, the SL40 does not require external cooling. When mounting the
SL40, leave a clearance of 1/8 to 1/4 inch between avionics to allow for circulation.
MINIMUM SYSTEM CONFIGURATION
The SL40 requires connections to the following equipment as a minimum:
• power input
• speaker or headphone output
• microphone input
• an antenna
EQUIPMENT MOUNTING
Once the cable assemblies have been made, attach the 15 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 shield grounds
directly to the connector mounting plate.
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Installation
Figure 2 Mounting Frame Assembly
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 instrument panel. Be sure to use low profile
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Installation
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.
To install the unit 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 unit 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 SL40 installation kit includes a 15 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. A wiring diagram is included as Figure 5.
POWER
The SL40 is internally fused at 7 amps. A separate 5 amp (maximum) circuit breaker or fuse
should be installed for downline overload or short circuit protection. Make the power
connections to the SL40 using 20 awg wire.
Note: Circuits should be protected in accordance with guidelines in AC 43.13-1A, chapter 11,
section 2, paragraph 429.
SPEAKER AND HEADPHONE OUTPUTS
Connect the speaker and headphones to the output pins on the rear connector.
MICROPHONE INPUTS
Microphone input connections should be made using a twisted pair shielded cable. Attach the
signal ground to the mic ground pin on the rear connector and connect the shield to the rear
connector plate.
TRANSMIT KEY INPUT
The TxKey input on the rear connector must be pulled low to ground to enable the transmitter.
This input should be connected to a microphone or yoke mounted momentary push button
switch.
INTERCOM SELECTOR SWITCH
The SL40 includes an intercom function that can be enabled by an external control switch.
This is an optional connection.
When making connection for the intercom selection, connect the intercom selection input to a
remote mounted normally open switch. A momentary toggle or alternate action switch can be
used. Connect the other terminal of the switch to ground. The intercom function is enabled
when the input is pulled low to ground.
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Installation
SERIAL INTERFACE
The SL40 includes an RS232 serial port, which can be used for inputting frequency and
function control commands and outputting transceiver status. This is an optional connection.
When making serial connections to the SL40, use a shielded three conductor cable. Make the
RxD, TxD, and ground connections on the 15 pin connector. Connect the shield to the rear of
the mounting frame on the connector plate.
The SL40 can be connected to the RS-232 serial data outputs on the Apollo 2001GPS
(requires software version 5.1 or later), the SL50, SL60, GX50, GX55, GX60, or the 360
Map/GPS for receiving remote frequency information from the GPS navigation data base.
Refer to the installation manuals for those units for connections and serial data output
selections.
Complete serial interface specifications are included in Appendix E.
ANTENNA INSTALLATION AND CONNECTIONS
The SL40 requires a standard 50Ω vertically polarized antenna. Follow the antenna
manufacturer’s installation instructions for mounting the antenna.
The antenna should be mounted on a metal surface or a ground plane with a minimum area of
18 x 18 inches. The antenna should be mounted a minimum of 24 inches away from GPS
antennas.
The comm antenna should also be mounted as far apart as practical from the ELT antenna,
preferably one on top and the other on the bottom of the aircraft fuselage. Some ELTs have
exhibited re-radiation problems generating harmonics that may interfere with GPS signals.
This can happen when the comm (SL40 or any other comm) is transmitting on certain
frequencies such as 121.15 or 121.175 MHz, which may cause the ELT output circuit to
oscillate from the signal coming in on the ELT antenna coax.
The antenna coax cable should be made of RG-142B or a comparable quality 50Ω coax.
Assembly instructions for the rear coax connector are included in Figure 4.
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Step 1.
0.031
Clamp Nut
Slit 1/4" (2X)
0.125
0.375
Installation
- Slide clamp nut over coax.
- Strip coax as illustrated.
- Cut two 1/4" slits in jacket 180
degrees apart.
Step 2.
Step 3.
Assembly instructions for right angle connector part #162-1008
Braid Clamp
Cap
Solder Center
Conductor
Figure 4 Coax Connector Assembly
- Slide braid clamp over end of coax and
under the braid.
- Insert coax with braid clamp into
connector and tighten clamp nut securely.
- Solder the center conductor of the coax
to the contact as illustrated.
- Attach the cap and secure tightly.
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Figure 5 SL40 Standalone Wiring Diagram
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Installation
Figure 6 SL40 Typical Audio Panel Connections
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Installation
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.
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 no
interference.
Receiver / Transmitter Operation
Tune the unit to a local frequency and verify the receiver output produces a clear and
understandable audio output. Verify the transmitter by contacting another station and getting a
report of reliable communications.
Antenna Check
The antenna VSWR can be checked using an inline watt meter in the antenna coax using
frequencies near both ends of the band. The VSWR should be < 2:1, and is not to exceed 3:1.
A VSWR of 2:1 will cause a drop in output power of approximately 12%, and 3:1 causes
approximately a 26% drop.
Interference Check
Check the SL40 while operating the other avionics and electrical systems on the aircraft to
verify that no significant interference exists, and that the SL40 does not cause significant
interference with other systems. Performance should be checked using low, high, and mid
band frequencies. Repeat during the flight test for equipment that is not checked on the
ground.
Sidetone Level Adjustment
The sidetone volume was preset at the factory to what should be an acceptable level. The level
can be adjusted in the System Functions mode. To adjust the sidetone level:
1. Press and hold the MON button for about two seconds. This will access the System
Functions mode.
2. Rotate the LARGE knob to display the SIDETONE LVL page.
3. Rotate the S
MALL knob to change the level number. The range of the number is 000 to
255, with 128 producing one half of full rated output. A setting of 000 slaves the level to
the Volume knob.
4. Press any key to exit the Setup Functions mode.
5. Select an appropriate frequency, key the transmitter, and talk into the microphone to check
the level.
Receiver Squelch Adjustment
Adjustments to the receiver squelch level may be performed by using the RCVR SQELCH page
in the Test Mode. Values may be adjusted between 25 and 100.
1. Press and hold the ⇔ and RCL keys while switching the unit on.
2. Turn the LARGE knob to the RCVR SQELCH page.
3. Press the ⇔ key to start selection (the number will flash).
4. Turn the S
MALL knob to change the value. Press MEM to store the value.
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Installation
5. Turn the unit off to exit the Test Mode.
Mic Level Adjustment
Those units with audio board p/n 415-7008-01, or later, have the ability to make adjustments
to microphone sensitivity by using the M
IC 1 LEVEL and MIC 2 LEVEL pages in the Test
Mode.
1. Press and hold the ⇔ and R
CL keys while switching the unit on.
2. Turn the LARGE knob to the MIC 1 LEVEL and MIC 2 LEVEL pages.
3. Press the ⇔ key to start selection (the number will flash).
4. Turn the SMALL knob to change the value. Press MEM to store the value.
5. Turn the unit off to exit the Test Mode.
Display Test
It is possible to perform a simple test to observe all segments of the display for a quick
checkout of the display functions.
1. Press and hold the ⇔ and RCL keys while switching the unit on.
2. Turn the LARGE knob to the DISPLAY TEST page.
3. Press MEM to perform the test. A series of “#” symbols will advance across the display
testing each LED.
4. Turn the unit off to exit the Test Mode.
Mic Squelch
Adjustments to the squelch levels for Mic1 and Mic2 are available in the System Functions
mode. To adjust the Microphone Squelch level:
1. Press and hold the MON button for about two seconds. This will access the System
Functions mode.
2. Rotate the LARGE knob to display the MIC1 OR MIC2 SQLCH pages.
3. Rotate the SMALL knob to change the level number. The range of the number is 000 to
127.
4. Press any key to exit the Setup Functions mode.
5. Select an appropriate frequency, key the transmitter, and talk into the microphone to check
the level.
Transmit Mic
The Transmit Microphone page allows you to control which microphone is permitted to
transmit. You may choose Mic 1, 2, or both. To adjust the Transmit Mic control:
1. Press and hold the M
ON button for about two seconds. This will access the System
Functions mode.
2. Rotate the
LARGE knob to display the TRANSMIT MIC page.
3. Rotate the SMALL knob to select MIC1, MIC2, or MIC1+MIC2.
4. Press any key to exit the Setup Functions mode.
5. Select an appropriate frequency, key the transmitter, and talk into the microphones to
check for the intended operation.
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Installation
Flight Test Check
A flight test is recommended as a final installation verification. The performance may be
verified by contacting a ground station at a range of at least 50 nm while maintaining an
appropriate altitude and over all normal flight attitudes. Performance should be checked using
low, high, and mid band frequencies.
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Specifications
SECTION 3 - SPECIFICATIONS
This section includes detailed electrical, physical, environmental, and performance
specifications for the Apollo SL40.
ELECTRICAL
Input voltage.............................................10 VDC to 40 VDC, reverse polarity protected
Input current..............................................300 mA typical, 2 A max. at 13.75 VDC, receive
140 mA typical, 900 mA max. at 27.5 VDC, receive
2.1A typical, 3.2A max. at 13.75 VDC, transmit
1.0 A typical, 1.4 A max. at 27.5 VDC, transmit
Note: receive max. at full receive audio, transmit
max. at 90% modulation at 1000Hz
Input power...............................................4 watts typical, receive
28 watts typical, transmit
Internal fuse..............................................7 amp fast blow, soldered in board
Power control connection.........................Pulled low to turn unit ON; floating (high) for unit
OFF
PHYSICAL
Height .......................................................1.30 inches (3.30 cm)
Width........................................................6.25 inches (15.88 cm)
Depth ........................................................11.452 inches (29.09 cm) behind panel, including
mounting frame and connectors
Weight (with mounting frame).................2.1 lb. (0.953 kg)
ENVIRONMENTAL
The Apollo SL40 unit is designed and tested to meet appropriate categories of RTCA/DO160C. 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.....................................35,000 feet
Cooling .....................................................Not required
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Specifications
Figure 7 Unit Dimensions
RECEIVER PERFORMANCE
Class......................................................... D
Frequency range....................................... 118.000 to 136.975 MHz, 760 channels
Sensitivity................................................. 1µV (2µV hard) for 6 dB S+N/N with 30%
modulation at 1000Hz
Selectivity................................................. < 6 dB variation at ± 7 kHz, > 60 dB at ± 22 kHz
Speaker audio output level....................... 12 watts into 4Ω, 8 watts into 8Ω
Headphone audio output level.................. 280mW into 100Ω, 120mW into 500Ω
Distortion.................................................. < 5% at rated output at 1000Hz
AGC characteristics.................................. < 3 dB variation in audio output from 5µV to
100mV input, 15% to 90% modulation
Squelch control......................................... Automatic squelch with manual override
TRANSMITTER PERFORMANCE
Class......................................................... 4
Output power............................................ 8 watts minimum carrier at >12VDC input,
6 watts minimum at 10VDC input
(transmit is locked out below 9 volts input)
Frequency range....................................... 118.000 to 136.975 MHz, 760 channels
Frequency tolerance..................................±15ppm from -20°C to +70°C
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Specifications
Microphone input .....................................Two inputs, standard carbon or dynamic mic with
integrated preamp providing minimum 70mv rms
into 1000Ω load
Modulation capability...............................85% with 100mv to 1000mv rms microphone input
at 1000 Hz
Audio frequency distortion.......................< 10% at 85% modulation at 350 to 2500 Hz
Audio frequency response ........................< 4db variation with 350 to 2500 Hz, 85%
modulation
Carrier noise level.....................................> 35 dB down
Sidetone output.........................................up to 280mW into 100Ω, 120mW into 500Ω
Duty cycle.................................................100%
Stuck mic time-out....................................35 second time-out, reverts to receive
INTERCOM PERFORMANCE
Microphone input .....................................Two inputs, standard carbon or dynamic mic with
integrated preamp providing minimum 70mv rms
into 1000Ω load
Headphone audio output level..................280 mW into 100Ω, 120 mW into 500Ω
AGC characteristic....................................output varies < 3 dB with input of 100mv rms to
1000mv rms
CONTROL INPUTS
Transmit key.............................................Input pulled low to ground to enable the transmitter
Intercom select..........................................Input pulled low to ground to enable the intercom
function
ANTENNA REQUIREMENTS
The Apollo SL40 requires an antenna meeting the following specifications.
Standard 50Ω vertically polarized antenna with a VSWR < 2.5:1.
SERIAL INTERFACE
RS-232......................................................Defined in Appendix E - Serial Interface
Specifications
REAR CONNECTOR PINOUT
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Specifications
Table 2 Connector Pinout
Pin # I/O Connection Function
1 I Power + main DC power input
2 I Reserved Do not connect
3 O TxD RS232 serial data output
4 I TxKey transmit enable key, pulled low to transmit
5 -- NC Do not connect
6 O Speaker speaker terminal output
7 I Mic ground microphone input ground connection
8 I Mic 1 microphone input #1
9 I Power ground main power ground input
10 I RxD RS232 serial data input
11 O Serial ground RS232 signal ground
12 I Intercom select intercom function select, pulled low to turn on the intercom
function
13 O Audio ground speaker and headphone ground connection
14 O Headphone headphone terminal output
15 I Mic 2 microphone input #2
18
915
Viewed from rear of unit
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Limitations
SECTION 4 - LIMITATIONS
INSTALLATION
Installations are to be made in accordance with AC 20-67B or other appropriate FAA
approved guidelines.
OPERATIONAL
An aircraft radio station license is required for transmitting.
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Limitations
NOTES
20 Apollo SL40 Installation Manual
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Troubleshooting
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 SL40 does not power on. T he unit is not getting power. Check power connections, breakers,
and main avionics switch.
The unit does not transmit. The TxKey input is not being pulled
low.
A weather channel is selected. Select a different frequency, the unit
The input voltage is too low. Increase input supply voltage to > 9
Mic Sensitivity varies Mic Levels need adjustment See the Mic Level Adjustment on
The sidetone and intercom
levels are too low or high.
The intercom doesn’t function. Control input not connected. The intercom select input must be
Wrong type of headsets, or level
needs adjustment.
Check the TxKey (mic key) input,
pulled low for transmit.
will not transmit on a weather
channel.
volts DC.
page 13
See the Sidetone Level Adjustment on
page 12.
pulled to ground to turn on the
intercom function.
No voice activation, or have to talk
too loud.
Change the intercom squelch
threshold using the setup function
described in the user’s manual.
CONTACTING THE FACTORY FOR ASSISTANCE
If the Apollo SL40 unit fails to operate despite troubleshooting efforts, contact the II Morrow
factory for assistance.
II Morrow Inc.
2345 Turner Rd. SE
Salem, Oregon 97302
USA
Phone (503) 581-8101 or 1-800-525-6726
http://www.iimorrow.com
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 version
• Description of problem
• Efforts made to isolate the problem
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Troubleshooting
NOTES
22 Apollo SL40 Installation Manual
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Periodic Maintenance
APPENDIX B - PERIODIC MAINTENANCE
EQUIPMENT CALIBRATION
The SL40 design requires very few adjustments or calibration to be made. In fact, there are no
internal manual adjustments.
REFERENCE OSCILLATOR
The reference oscillator frequency should be checked approximately every 3 to 5 years to
ensure the units transmit frequency is within allowable tolerance.
The oscillator frequency can be checked by connecting the transmitter output through an
appropriate load to a calibrated frequency counter. The transmit frequency should be within
15ppm of the selected channel frequency. Contact the II Morrow factory for instructions on
adjusting the frequency if 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. Care should be taken to avoid
scratching the surface of the display.
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Periodic Maintenance
NOTES
24 Apollo SL40 Installation Manual
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Environmental Qualifications
APPENDIX C - ENVIRONMENTAL QUALIFICATIONS
The Apollo SL40 has been tested to the following environmental categories per procedures
defined in RTCA/DO-160C.
Environmental Qualification Form
Nomenclature: SL40
Part No.: 430-6040-200
TSO No.:
Conditions Section Description of Conducted Tests
Temperature and Altitude 4.0 Equipment tested to Category C1 with
In-flight Loss of Cooling 4.5.4 No cooling required
Altitude 4.6.1 Equipment tested to 35,000 feet
Overpressure 4.6.3 Equipment tested for overpressure
Temperature Variation 5 .0
Humidity 6.0 Equipment tested to Category A, standard humidity
Operational Shocks and Crash
Safety
Vibration 8.0 Equipment tested without shock mounts to Categories B, M,
Explosion Proofness 9.0 Equipment identified as Category X, no test required
Waterproofness 10.0 Eq uipment identified as Category X, no test required
Fluids Susceptibility 11.0 Equipment identified as Category X, no test required
Sand and Dust 1 2.0 Equipment identified as Category X, no test required
Fungus Resistance 13.0 Equipment identified as Categor y 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 Eq uipment tested to Categories A & B
Voltage Spike 17.0 Equipment tested to Category A
Audio Frequency Cond ucted
Susceptibility - Power Inputs
Induced Signal Susceptibility 19.0 Equipment tested to Category Z
Radio Frequency Susceptibility
(Radiated and Conducted)
Emission of Radio Frequency
Energy
Lightning Induced Transient
Susceptibility
Lightning Direct Effects 23.0 Equipment identified as Category X, no test required
Icing 24.0 Equipment identified as Category X, no test required
Remarks:
7 Equipment tested for both operational and crash safety
18.0 Equipment tested to Categories A & B
20 Equipment tested to Category V for conducted, Category U
21 Equipment tested to Category Z
22.0 Equipment tested to Categories A3 and B2.
Manufacturer:
II Morrow Inc.
2345 Turner Road SE
Salem, Oregon 97302
Equipment tested to Category C, 2°C/min
environment
shocks. (Equipment operated normally after the crash safety
shocks.)
& N
for radiated.
RS-232 input/output tested to A3 and B1.
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Environmental Qualifications
NOTES
26 Apollo SL40 Installation Manual
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Serial Data Specifications
APPENDIX E - SERIAL INTERFACE SPECIFICATIONS
This appendix includes the interface specifications for the RS-232 serial port. The RS-232
port can be used to input active and standby frequencies, and is used to input frequencies from
a remote source, such as the SL50 and 2001GPS. The interface format conforms to NMEA
0183 message format specifications.
The format of the RS-232 serial port is as follows:
Baud rate............................................9600
Data bits.............................................8
Stop bits.............................................1
Parity..................................................none
The data format is as follows:
$PMRRC<msg_id><msg_data><chksum><cr>
The checksum is computed by an 8 bit addition of the msg_id and msg_data characters,
ignoring carry if any. The resulting 8 bit checksum is converted to two ascii characters by
taking the upper and lower nibbles, adding 30h to each, and placing the most significant
character first in the data message.
RS-232 INPUTS
SET ACTIVE FREQUENCY
Message Format
$PMRRC00mka<chksum><cr>
00.......message id
mk......active frequency:
m = desired frequency in MHz in hexadecimal, where m = desired frequency 30h , with desired frequency in range of 118 to 136 MHz, or 162 MHz.
k = desired frequency in kHz where k = (desired frequency / 25 kHz) + 30h, with
desired frequency in range of 000 to 975 kHz in 25 kHz steps, or 0 to 39.
a .........transceiver function:
N = normal receive operation
M = enable monitor function
0 = no change
Example Message
$PMRRC00G4N29<cr>
Set the active frequency to 119.100MHz, normal receive mode. “G” = 119d - 30h = 77h -
30h = 47h, or an ascii “G”; “4” = 100 kHz/25 kHz + 30h = 4 + 30h = 34h, or an ascii “4.”
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Serial Data Specifications
SET STANDBY FREQUENCY
Message Format
$PMRRC01mka<chksum><cr>
01....... message id
mk...... standby frequency:
m = desired frequency in MHz in hexadecimal, where m = desired frequency 30h , with desired frequency in range of 118 to 136 MHz, or 162 MHz.
k = desired frequency in kHz where k = (desired frequency / 25 kHz) + 30h, with
desired frequency in range of 000 to 975 kHz in 25 kHz steps, or 0 to 39.
a......... transceiver function:
N = normal receive operation
M = enable monitor function
0 = no change
Example Message
$PMRRC01LFM40<cr>
Set the standby frequency to 124.550 MHz, monitor function selected
REMOTE IDENT INPUT
This message is used to input a new ident, and reset the remote frequency input pointer.
Message Format
$PMRRC04tiiii<chksum><cr>
04....... message id
t.......... list type, input 1
iiii...... ident, four character ascii
Example Message
$PMRRC041SLE<space>99<cr>
Set the remote frequency ident to “SLE.”
REMOTE FREQUENCY LIST INPUT
This message is used to input frequencies for the remote recall function. Up to 10 frequencies
are accepted.
Message Format
$PMRRC05tfmk<chksum><cr>
05....... message id
t.......... list type, input 1
f ......... frequency type:
0 = TWR, tower frequency 8 = CTF, common traffic advisory frequency
1 = GND, ground frequency 9 = DEP, departure
2 = ATS, for ATIS : (3Ah) = FSS, flight service station
3 = ATF, air traffic frequency ; (3Bh) = RFS, for remote flight service station
4 = APP, for approach < (3Ch) = UNI, for unicom
28 Apollo SL40 Installation Manual
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5 = ARR, for arrival = (3Dh) = MF, mandatory frequency
6 = AWS, automatic weather station > (3Eh) = not defined, do not use
7 = CLR, clearance/delivery ? (3Fh) = undefined, for other frequency types
mk......frequency:
m = desired frequency in MHz in hexadecimal, where m = desired frequency 30h , with desired frequency in range of 118 to 136 MHz, or 162 MHz.
k = desired frequency in kHz where k = (desired frequency / 25 kHz) + 30h, with
desired frequency in range of 000 to 975 kHz in 25 kHz steps, or 0 to 39.
Example Message
$PMRRC0511IT64<cr>
Input a ground frequency type, 121.900 MHz.
REQUEST OUTPUT MESSAGE
This message is used to request data output messages.
Message Format
$PMRRC06iidda<chksum><cr>
06.......message id
ii.........requested message ident:
03 = software version message
dd.......set to 00
a .........set to 0
Serial Data Specifications
Example Message
$PMRRC060300059<cr>
This message requests the software version message to be output.
RS-232 OUTPUTS
TRANSCEIVER STATUS
This message is used to output the current transceiver frequencies and status.
Message Format
$PMRRC01mkmkas<chksum><cr>
01.......message id
mk......active frequency (first mk):
m = frequency in MHz in hexadecimal, where m = frequency - 30h , with
frequency in range of 118 to 136 MHz, or 162 MHz.
k = frequency in kHz where k = (frequency / 25 kHz) + 30h, with frequency in
range of 000 to 975 kHz in 25 kHz steps, or 0 to 39.
mk......standby frequency (second mk):
m = frequency in MHz in hexadecimal, where m = frequency - 30h , with
frequency in range of 118 to 136 MHz, or 162 MHz.
k = frequency in kHz where k = (frequency / 25 kHz) + 30h, with frequency in
range of 000 to 975 kHz in 25 kHz steps, or 0 to 39.
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Serial Data Specifications
a......... transceiver status:
R = normal receive
M = monitor selected
T = transmit enabled
S = stuck mic
s......... squelch test setting:
0 = automatic
1 = test selected
Example Message
$PMRRC01G4LFR0F0<cr>
The active frequency is 119.100 MHz, the standby frequency is 124.550 MHz, normal
receive function, automatic squelch selected.
This message is output once/second.
SOFTWARE VERSION
This message is used to output the com software version.
Message Format
$PMRRC03vvvv<chksum><cr>
03....... message id
vvvv... software version
Example Message
$PMRRC03010024<cr>
The software version is 01.00.
This message is output once at power up and by request.
30 Apollo SL40 Installation Manual
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Declaration of Conformity
Manufacturer’s name: II Morrow Inc.
Manufacturer’s address: 2345 Turner Rd. SE
Salem, Oregon, 97302 USA
declares that the following product:
Type of equipment: VHF Comm transceiver for aircraft
Product name: Apollo SL40 Comm
Part number: 430-6040-2xx
conforms to the following Directives and Standards:
Application of Council Directives: 89/336/EEC, 93/68/EEC
Standards: EN50081-1, EN50082-1
Quality Department
II Morrow Inc.
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