AEM SM59 AMS43 User manual

SPECIAL NOTICE
This product is now licensed to Anodyne Electronics Manufacturing (AEM) from Northern
Airborne Technology (NAT). AEM is responsible for all matters related to this product, including
sales, support and repair services.
Please note the transition to convert product manuals and supporting documentation is an
ongoing process and is being addressed on an ‘as needed’ basis.
All references to NAT product part numbers (and associated images) are equivalent to AEM
product part numbers.
Contact info:
Anodyne Electronics Manufacturing Corp.
#15-1925 Kirschner Road
Kelowna B.C. Canada
V1Y 4N7
Email: [e-mail]
Toll Free: 1-888-763-1088
Phone: [phone]
Fax: [phone]
www.aem-corp.com

CONFIDENTIAL AND PROPRIETARY TO ANODYNE ELECTRONICS MANUFACTURING CORP.
INSTALLATION AND OPERATION MANUAL
Rev: 2.00 April 22, 2012
Anodyne Electronics Manufacturing Corp.
15-1925 Kirschner Road
Kelowna, BC, Canada.
V1Y 4N7
Telephone [phone]
Facsimile [phone]
Website: www.aem-corp.com
© 2012 Anodyne Electronics Manufacturing Corp. (AEM),
All Rights Reserved
SM59
AMS43
Single Channel Audio Controller

AMS43 Single Channel Audio Controller
SM59 Installation and Operation Manual
Installation and Operation Manual Page ii
ENG-FORM: 820-0100.DOTX
CONFIDENTIAL AND PROPRIETARY TO ANODYNE ELECTRONICS MANUFACTURING CORP.
IMPORTANT INFORMATION
This manual has been produced to provide information unique to the AMS43 Single
Channel Audio Controller. Some of this information has been published previously in the
SM01 Service manual (AA90/AMS40 Series Audio Controllers).
Earlier versions of the AMS43 may not be covered by the information in this manual.
Please refer to SM01, or contact the Technical Support Department at AEM.
COPYRIGHT STATEMENT
© 2012 Anodyne Electronics Manufacturing Corp. (AEM), All Rights Reserved
This publication is the property of AEM and is protected by Canadian copyright laws. No part of
this document may be reproduced or transmitted in any form or by any means including electronic,
mechanical, photocopying, recording, or otherwise, without the prior written permission of AEM.

AMS43 Single Channel Audio Controller
SM59 Installation and Operation Manual
Installation and Operation Manual Page iii
ENG-FORM: 820-0100.DOTX
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Prepared By:
Checked By:
Approved By:
The status of this installation and operation manual is controlled by issue shown on the title page. The
status of each section is controlled by revision shown in the footer of each page. All revisions affecting
sections of this manual have been incorporated into the latest issue.
ISSUE/REVISION RECORD
Manual Issue
Number
Section
Revision Number
Revision Description
Issue Date
4.00 N/A N/A Nov 10, 200
3
4.01 Section
1 Rev: 1.00
Section 2 Rev: 1.00
Section 3 Rev: 1.00
Rewritten in latest format.
Newest drawings added. Sep 23
, 2008
AEM MANUAL REVISIONS
Section
Revision Number
Revision Description
Date
All Rev: 2.00 Updated drawings
and format
April 22
, 2012
Tony Pearson
Designer
A
pr 22, 2012
Loen Clement
Designer
May 24/12
Tom Betzelt
Product Support
Manager
May 28, 2012

AMS43 Single Channel Audio Controller
SM59 Installation and Operation Manual
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Table of Contents
Section Title Page
1.0 Description
1.1 Introduction 1-1
1.2 Purpose of Equipment 1-1
1.3 Design Features 1-1
1.4 Specifications 1-2
1.4.1 Electrical Specifications 1-2
1.4.2 Physical Specifications 1-3
1.4.3 Environmental Specifications 1-4
2.0 Installation
2.1 Introduction 2-1
2.2 Unpacking and Inspection 2-1
2.2.1 Warranty 2-1
2.3 Continued Airworthiness 2-1
2.4 Installation Procedures 2-1
2.4.1 Warnings 2-1
2.4.2 Cautions 2-2
2.4.3 Cabling and Wiring 2-2
2.4.4 Post Installation Checks 2-2
2.5 Adjustments and Connections 2-3
2.5.1 Left Side panel adjustments 2-4
2.5.2 Right Side Panel Adjustments 2-4
2.5.3 In-line PTT Drop Cords 2-5
2.6 Accessories Required But Not Supplied 2-6
2.7 Installation Drawings 2-7
3.0 Operation
3.1 Introduction 3-1
3.2 General Information 3-1
3.3 Controls and Indicators 3-1
3.3.1 Receive Audio Select Switches 3-1
3.3.2 Transmit Selector Switch 3-2
3.3.3 ICS Functions 3-3
3.4 Emergency Operation 3-4
3.5 Audio Alerting Functions 3-4
3.5.1 Direct Audio 3-4
3.5.2 Internal Alerting 3-4

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April 22, 2012 Rev: 2.00 Page 1-1
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Section 1.0 Description
1.1 Introduction
Information in this section consists of product description, design features and specifications for the
AMS43 Single Channel Audio Controller. All derivative product information shall be contained in the
applicable manual supplement, which may be obtained from AEM as required.
Review all notes, warning and cautions.
1.2 Purpose of Equipment
The AMS43 provides control of aircraft audio, allowing selection of transmit (TX) and receive (RX) audio, LIVE,
KEYED, or voice activated (VOX) intercom, interface for an additional hand-held transmit microphone (hand
mic), and pilot isolation/emergency (ISO/EMR) operation.
TX and PA functions are controlled with a single rotary switch. RX audio, intercom (ICS) operations and tape
audio are controlled with toggle switches. RX volume, ICS volume and ICS VOX squelch are individually
adjusted with rotary controls. Sidetone (S/T) level is adjustable internally.
1.3 Design Features
The AMS43 is a Dzus rail mounted unit with a backlit faceplate. Transceiver interfacing is accomplished
through directly switched microphones. To ensure maximum radio compatibility, it has a ground
referenced keyline that does not incorporate diodes or other steering components.
Independent control is provided for S/T, ICS audio, and RX audio.
Boom mic support is provided for the pilot and co-pilot, with both ICS and TX functions via cyclic or yoke
switching. Live (Hot Mic) and VOX ICS allow immediate transmission without additional control panel
switching, with immediate return to ICS operation on completion. The ICS function is achieved using
dynamic noise reduction and active filtering. This provides the clearest possible ICS audio under high
ambient noise conditions by rejecting airframe and wind noise, and passing only voiceband information.
All audio, except the S/T of the radio in use and DIRECT AUDIO 2 input signals, is muted during TX for
clarity. ICS operation allows TX during any ICS mode by using the TX push-to-talk (PTT) switch.
All external interconnect, switches and relay contacts are gold plated for maximum reliability. Switches
and relays are sealed. G10-FR flame-retardant circuit boards are postcoated for maximum moisture
resistance and corrosion prevention.
Relays are sealed, high vibration rated (50g shock), dry nitrogen filled units.

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1.4 Specifications
1.4.1 Electrical Specifications
Input Power 27.5 Vdc Nominal 0.50 A Max.
Lighting Voltage 27.5Vdc@160mA
Alert Power 27.5 Vdc Nominal 150 mA Max.
Input Signals
Quantity 13 Receive channels.
7Micchannels
1 ICS tie channel
2 direct channels
Audio level 2.5V rms for receiver inputs.
0.25Vrmsformicinputs.
0.34V rms for ICS tie input.
2.5V rms for direct audio inputs.
Impedance 1k:± 10% for receive inputs.
1k:± 10% for mic inputs.
1.8k:± 10% for ICS tie input.
1.3k:± 10% for Direct Audio 1 input.
100:± 10% for Direct Audio 2 input.
Circuitry Type All are Single ended inputs.
Coupling < -50 dB
Key lines Pilot & Copilot Transmit PTT.
Rear Hand mic Transmit PTT
Pilot & Copilot ICS PTT.
3 Alerts - active low.
Output Signals
Quantity 6 Headset outputs.
6Transmittermicoutputs.
5 Transmitter keyline outputs.
Rated level
Headset 7.7 Vrms or 100 mW (20 dBm) into 600 :
Direct Audio1 10 mW (10 dBm) into 600 :
Direct Audio 2 0.1 mW (-10 dBm) 0.25 Vrms into 600 :
Alert level 90mV rms ±10% into 600 :
Impedance 65 :Max
Circuitry Type Single-ended, except for phones, which are balanced.
Freq. Response
Sidetone <3 dB from 650 Hz to 1750 Hz

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Receive inputs <3 dB from 500 Hz to 2200 Hz
Intercom < 3 dB from 550 Hz to 2400 Hz.
Alert 1 1.5kHz + 20%
Alert 2 Same tone as Alert #1 but swept @ 2 cycles/sec.
Alert 3 Approx. same as Alert 2 but on for 2 sec.
Distortion < 10% THD @ rated power output
Audio Noise Level: < -50 dB
Coupling < -50 dB
Output Regulation < 10% distortion and <3 dB max. of rated load output
power at 400% and 75% of rated load
Annunciators Green LED will light for transmit operation.
1.4.2 Physical Specifications
Height 1.90” (48.3 mm)
Depth 6.82” (173.2 mm)
Width 5.00” (125.0 mm) behind panel
Weight 2.1 lbs (955g)
Mounting Dzus rail
Faceplate Engraved acrylic edge lit panel
Material/Finish Chassis & cover are 5052-H32 brushed aluminum with
conversion coating finish
Connectors Male 50 pin & 37 pin D-submin connectors with slide locks

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1.4.3 Environmental Specifications
DO-160C Env. Cat. B1-CANXXXXXXABABBBBXXX
Operating Temperature -20qC. to +55qC
Survival Temperatures -55qC. to +85qC
Vibration/Shock DO-160C Cat. N
Humidity 95%
Altitude 25,000 feet max
End of Section 1.0

AMS43 Single Channel Audio Controller
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April 22, 2012 Rev: 2.00 Page 2-1
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CONFIDENTIAL AND PROPRIETARY TO ANODYNE ELECTRONICS MANUFACTURING CORP.
Section 2.0 Installation
2.1 Introduction
Information in this section consists of unpacking and inspection procedures, installation procedures, post-
installation checks and installation drawings for the AMS43 Single Channel Audio Controller.
Review all notes, warnings and cautions.
2.2 Unpacking and Inspection
Unpack the equipment carefully. Inspect the unit visually for damage due to shipping and report all such
claims immediately to the carrier involved. Check that all items listed below are present before proceeding
and report any shortage immediately to your supplier:
- AMS43 Single Channel Audio Controller
- Product Information Card
- Certificate of Conformity or Release Certification
2.2.1 Warranty
All Anodyne Electronics Manufacturing Corp. (AEM) products are warranted for 2 years. See the website
www.aem-corp.com/warranty for complete details.
2.3 Continued Airworthiness
Maintenance of the AMS43 Single Channel Audio Controller is ‘on condition’ only. Periodic maintenance
of this product is not required.
2.4 Installation Procedures
2.4.1 Warnings
WARNING:
High volume settings can cause hearing damage.
Set the headset volume control to the minimum volume setting prior to
conducting tests, and slowly increase the headset volume to a
comfortable listening level.

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2.4.2 Cautions
CAUTION:
Do
not bundle any lines from this unit
with transmitter coax feed lines. Do not
bundle any logic, audio, or DC power lines from this unit with 400 Hz synchro
wiring or AC power lines. Do not position this unit next to any device with a
strong alter
nating magnetic field such as an inverter, motor or blower, or
significant audio interference will result.
In all installations, use shielded cable exactly as shown, and ground only as
indicated. Significant problems may result from not following these guidelines.
Failure to follow the installation and wiring instructions provided in this manual
for power and ground connections, including the rating of the circuit breaker,
may lead to damage in the power input circuitry of the unit.
2.4.3 Cabling and Wiring
All wire shall be selected in accordance with the original aircraft manufacturer's Maintenance Instructions
or AC43.13-1B Change 1, Paragraphs 11-76 through 11-78. Unshielded wire types shall qualify to
MIL-W-22759 as specified in AC43.13-1B Change 1, Paragraphs 11-85, 11-86, and listed in Table 11-11.
For shielded wire applications, use Tefzel MIL-C-27500 shielded wire with solder sleeves (for shield
terminations) to make the most compact and easily terminated interconnect. Follow the connector map in
Section 2.7 as required.
Allow 3" from the end of the shielded wiring to the shield termination to allow the connector hood to be
easily installed. Reference the interconnect drawing in Section 2.7 for shield termination details. Note that
the hood is a "clamshell" hood, and is installed after the wiring is complete. Aircraft harnessing shall
permit the unit to be removed from the panel for easy access to all side adjustments. Do NOT mount the
unit until all adjustments have been performed.
Maintain wire segregation and route wiring in accordance with the original aircraft manufacturers
Maintenance Instructions.
Unless otherwise noted, all wiring shall be a minimum of 22 AWG, except power and ground lines, which
shall be a minimum of 20 AWG. Reference the Interconnect drawing for additional specifications. Check
that the ground connection is clean and well secured, and that it shares no path with any electrically noisy
aircraft accessories such as blowers, turn and bank instruments or similar loads. Power to this unit must
be supplied from a separate circuit breaker or fuse (fast blow), and not attached to any other circuit
breaker without additional protection. Verify that the selected circuit breaker size and wire gauge are
adequate for the installation using the techniques specified in AC43.13-1B Change 1, Paragraphs 11-47
through 11-51 and 11-66 through 11-69.
2.4.4 Post Installation Checks
Perform any required adjustments of preset levels, and ensure that the audio controller is properly
mounted and secured prior to flight.

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2.4.4.1 Voltage/Resistance Checks
Do not attach the AMS43 until the following conditions are met.
Check the following:
a) P101 pins <16> and <17> for +28 Vdc relative to ground.
b) P101 pin <34> for continuity to ground (below 0.5 ).
c) P102 pin <19> for +28 Vdc lights bus voltage.
d) Check all Mic, phone, music and key lines for shorts to ground or adjacent pins.
2.4.4.2 Power On Checks
Power up the aircraft’s systems and confirm normal operation of all functions of the AMS43. Refer to
Section 3 (Operation) for specific operational details.
Start with only the pilot's headset installed. Check for correct Intercom(ICS), radio, and transmit (TX)
operation. Do not proceed until the radios are functioning correctly. The S/T trimpot accessible through the
left side of the controller and the transceiver internal trimpot may have to be adjusted for correct balance for
the pilot. Adjustment of the individual radio receive (RX) levels should be set first with the AMS43 in PILOT
ISO/EMR (Pilot isolate/emergency) mode, then adjust the AMS43 front panel RX master volume control level
in NORMAL mode.
Unusual buzzes, hums or other background audio are symptomatic of multiple grounds or noisy external
systems sharing the same wire bundle. Incorrect jack wiring is a common fault, especially for passenger
stations, and may cause loss of audio, a tone on the headset lines, or other problems. Failure to key or
correctly modulate a transceiver may be caused by missing grounds on the radio or audio controller.
Plug in the hand mic and test for correct operation. Wiring faults for this accessory may cause peculiar
loss of ICS or TX functions because it has over-riding priority in the system.
Plug in the remaining headsets and check for proper operation. An incorrect drop cord or improper jack
wiring may cause a wide range of problems from loss of audio to a tone heard in the headset. For further
information, see section 2.5.3 below.
Check levels and operation of all functions in flight to ensure proper adjustments and settings have been
made.
Upon satisfactory completion of all performance checks, make all required log book entries, electrical
load, weight and balance amendments and other documentation as required by your local regulatory
agency before releasing the aircraft for service.
2.5 Adjustments and Connections
The unit ships from the factory with all internal adjustments set to the normal test levels. Once installed in
the aircraft, it may be desirable to change some of these settings to best suit the local operating
environment.
The internal adjustments are located on the sides of the unit and are as follows:

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2.5.1 Left Side panel adjustments
The trimpots on the left side panel are used to adjust the levels of audio in the user’s headphones. Rotating the
trimpots clockwise (cw) increases the level, and counterclockwise (ccw) reduces it.
The ALERT LEVEL trimpot is used to adjust the levels for the three internally generated Alert signals.
Other parameters relating to these signals are adjusted from the right side panel (see section 2.3.4.2.)
The S/T LEVEL trimpot adjusts the internal gain of the sidetone (S/T) of the selected transceiver (from the
front panel) in the user’s headphones.
The VOX LEVEL trimpot sets the sensitivity level for the front panel VOX control (the level of audio
required to activate microphones).
The POWER ON LED will illuminate to indicate that the unit is connected to the power supply.
2.5.2 Right Side Panel Adjustments
A variety of different signals can be selected to trigger the internal Alert signals. The trimpots on the right
side panel are used to adjust the characteristics of the audible signals that the user will hear.
Audio Alert 1 is a single tone signal and Audio Alerts 2 and 3 are two-tone signals. The pitch of the
signals can be adjusted using the relevant TONE trimpot, and the cycling rate of the two-tone signals can
be adjusted using the RATE trimpots. The duration of Audio Alert 3 can be adjusted from one to three
seconds using the TIME trimpot.
The DIR AUD LEVEL trimpot is used to adjust the audio level of the devices connected to the DIR AUD 1 input.

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2.5.3 In-line PTT Drop Cords
2.5.3.1 General
In-line, push-to-talk (PTT) drop cords (also known as cordsets) can be used to create/provide PTT capability
for the user headsets that do not have yoke or cyclic mounted PTT switches. For headsets connected to
the PILOT or COPILOT inputs/outputs of the AMS43, ICS and TX keylines are needed to properly activate
the associated PTT circuitry inside the AMS43. For headsets connected to the PASSENGER inputs/outputs
of the AMS43, a method of controlling the microphone on the headset is needed because of the 'hot mic'
circuitry. This is best accomplished with a 'mic interrupt' switch in the PTT drop cord.
There are numerous manufacturers of in-line PTT drop cords, offering many 'electrical' variations to
accomplish different functions. To meet the operational requirements for headset stations supported by
the AMS43, AEM recommends the dual switch type: a 3-position (momentary/center-off/locking) slider
switch for the ICS functions, and a momentary, push-button switch for the TX functions. Both switches
provide a ‘mic interrupt’ function. The 3-position ICS switch will allow the user to change the switch
settings to match the operational intercom mode that has been selected at the AMS43 (e.g., LIVE,
KEYED or VOX). The cable should have 6 conductors, with the MIC and PHONE pairs shielded (MIC
wires must be shielded as a minimum). To ensure proper shielding, the shield(s) should be terminated to
the MIC LO connection at the airframe connector of the PTT drop cord. See the drawing below for
details.
PTT Cord for Use with AEM Audio Controllers
(XMIT and ICS)
To avoid complications in the aircraft, it is recommended that the same type of PTT drop cord is used for
all headset locations in the aircraft. It is not good practice to create a situation where a specific drop cord
is needed for the copilot, which might cause operational errors if moved to a passenger location.

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2.5.3.2 Cautions
CAUTION:
Although in-line PTT drop cords can be used to conveniently address a
number of requirements for microphone and PTT control, they can also
be a source of trouble if incorrectly configured, or improperly shielded.
Many in-line PTT drop cords use the PHONE LO connection as the
ground reference for the ICS and TX PTT keylines. The PHONE LO
connection in the AMS43 is floating, which will lead to incorrect keying of
the intercom and radio systems if this type of drop cord is used.
In-line PTT drop cords can be a very real source for crosstalk if the MIC
wire pair in the drop cord is not shielded. The source of the crosstalk is
the high level Phones audio being coupled on to the MIC HI/LO pair in
the in-line PTT drop cord, because of the lack of shielding for this wire
pair. Once the mic line is contaminated, the undesired audio can be
sent into the audio system as ‘mic audio’, then processed and distributed
to all other audio controllers via the ICS Tie Line.
2.6 Accessories Required But Not Supplied
Installation kit AA90-IKC (Alt. part No. D50S37SL-IKC) is required to complete the installation. The
kit consists of one 50-Pin D-min Female Crimp Kit (D50SL-IKC) and one 37-Pin D-min Female Crimp
Kit (D37SL-IKC).
D50SL-IKC consists of
Quantity Description AEM Part #
1 D-min 50 Socket Housing 20-21-050
50 MS Crimp Socket 20-26-901
1* Jack Screw Set 20-27-002
1* Lock Clip Set 20-27-004
1 50 Pin Connector Hood 20-29-051
D37SL-IKC consists of
Quantity Description AEM Part #
1 D-min 37 Socket Housing 20-21-037
37 MS Crimp Socket 20-26-901
1* Jack Screw Set 20-27-002
1* Lock Clip Set 20-27-004
1 37 Pin Connector Hood 20-29-038
* Use as required.

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2.7 Installation Drawings
DRAWING
REV.
DESCRIPTION
TYPE
SERIAL No.
AMS43\403-0
1.12
Audio Controller
Interconnect
2580 and up
AMS43\403-1
1.12
Audio Controller
Interconnect
2580 and up
AMS43\403-2
1.12
Audio Controller
Interconnect
2580 and up
AMS43\405-0
1.00
Audio Controller
Connector Map
2580 and up
AMS43\905-0
2.00
Single Channel Audio Controller
Faceplate
2580 and up
AMS43\922-0
1.01
Audio Controller
Mech. Installation
2580 and up
Section 2.0 ends following the above documents