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823 McTavish Road NE, Calgary, Alberta, Canada T2E 7G9 Tel: 800 564 6469

P139-HD

DIGITAL AUDIO SYSTEM

AS350 / AS355 INSTALLATION

MDL GA182 Rev M STC SR00521SE

LEGAL NOTICE The information contained in this document is provided solely under the condition that the Recipient of this document agrees to the terms and conditions of the Non-Disclosure and Proprietary Rights Agreement listed below. By accessing this document past this page, you are agreeing to be bound by this Non-Disclosure and Proprietary Rights Agreement.

Non-Disclosure and Proprietary Rights Agreement Recipient recognizes and acknowledges that Eagle Copters USA and its affiliates (“Eagle”) possess certain Proprietary information and materials, which constitute a valuable, special, and unique asset of Eagle. As used herein, the term “Proprietary information and materials” includes, withoutlimitation, all information and materials belonging to, used by, or in the possession of Eagle relating to its products, processes, technology, inventions, patents, developments, and trade secrets of every kind and character, but shall not include:

(1) Information that was already in the public domain, (2) Information that subsequently becomes public domain through no act or omission by the Recipient.

Recipient hereby acknowledges that all of the Proprietary information and materials are and shall continue to be the exclusive property of Eagle, whether or not disclosed to or entrusted to the custody of Recipient. Recipient further hereby acknowledges that all Proprietary information and materials have been disclosed or made available to him solely for the purpose of assisting him in incorporating, using, or maintaining equipment provided by Eagle.

Recipient hereby agrees not to disclose, or allow to be disclosed, any Proprietary information or material of Eagle, in whole or in part, to any person or entity, for any reason or purpose whatsoever. Recipient further agrees that Recipient shall not use any Proprietary information or materials of Eagle for Recipient’s own purposes or for the benefit of any other person or entityexcept Eagle, whether such use consists of duplication, removal, oral use or disclosure, the transfer of any Proprietary information or materials in any manner, or any other unauthorized use, unless given prior written consent by Eagle.

Recipient further agrees that Recipient will not allow the reverse engineering of any Eagle products.

Recipient further agrees that Recipient shall use information provide, for installation or application, to one aircraft only for each product purchased, unless the purchase agreement specifically authorizes the use on more than one aircraft.

Continuing past this page constitutes acceptance of the above agreement.

(End of Agreement)

Page 1 of 1

of 7 GA182 Rev M.doc

Eagle Copters Ltd.

AUDIO SYSTEM STC: SR00521SE

MASTER DRAWING LIST GA182

Revision M June 13, 2013

NOTE: X IN LR COLUMN INDICATES CHANGE FROM LAST REVISION LEVEL. DOCUMENTS WITH MULTIPLE PAGES, THAT USE A SEPARATE REVISION LEVEL FOR EACH PAGE, ARE LISTED BY INDIVIDUAL PAGE ON THIS LIST.

LR DRAWING NO.

SHEET REV REV DATE TOTAL SHT

DESCRIPTION

GA182-2 -- H 10/15/12 9 Installation Instructions GA182-4 -- B 9/5/98 3 Electrical Power Consumption GA182-5 -- -- 8/15/05 2 Installation Instructions Bell 206/407 GA182-7 -- C 10/15/12 13 P139-HD Installation Instructions, AS350/355 GA182-8 -- C 10/15/12 12 P139-HD Installation Instructions, Bell 206/407

X GA182-11 -- C 6/13/13 15 P139-HD EC135 Installation Manual GA1-2TP -- C 5/13/12 7 EMI Test Procedure G10063 -- A 7/29/04 1 Voltage Converter – P118 G11261 1 D 10/9/02 1 Audio System Overview G11261 2 B 10/9/02 1 Audio System Overview G11262 1 D 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 2 D 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 3 D 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 4 D 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 5 -- 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 6 D 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 7 -- 9/5/98 1 Wire Routing AS350/AS355 Audio System G11262 8 -- 9/5/98 1 Wire Routing AS350/AS355 Audio System G11268 -- -- 3/14/03 1 Backplane G11269 -- F 9/30/08 1 Headset Control Cable G11287 -- A 7/24/98 1 SWIF 12 Switch Interface G11306 1 C 9/5/98 1 Switch, Connector Mounting Details G11306 2 C 10/07/08 1 Switch, Connector Mounting Details G11306 3 -- 9/5/98 1 Switch, Connector Mounting Details G11306 4 -- 9/5/98 1 Switch, Connector Mounting Details G11306 5 -- 9/5/98 1 Switch, Connector Mounting Details G11306 6 -- 9/5/98 1 Switch, Connector Mounting Details G11306 7 -- 9/5/98 1 Switch, Connector Mounting Details G11306 8 -- 9/5/98 1 Switch, Connector Mounting Details G11306 9 -- 9/5/98 1 Switch, Connector Mounting Details G11306 10 -- 9/5/98 1 Switch, Connector Mounting Details G11321 -- -- 9/5/98 1 IC-R100 Tray G11322 -- -- 9/5/98 1 Scanner IC-R100 G11326 -- A 6/16/98 1 FM Transceiver VHF 150-174MHz G11327 -- A 6/16/98 1 FM Transceiver UHF 450-470MHz G11328 -- C 7/29/04 1 Control Assembly G11350 1 -- 9/5/98 1 Instrument Panel Installation Instructions

Master Drawing List GA182

Page 2 of 7 GA182 Rev M.doc

LR DRAWING NO.


DESCRIPTION

G11350 2 -- 9/5/98 1 Instrument Panel Installation Instructions G11426 -- F 10/07/08 1 Audio Router Assembly G11426-1 -- E 7/29/04 1 Router Case G11426-2 -- D 7/29/04 1 Router Side Cover G11426-3 -- D 7/29/04 1 Router Side Cover G11426-4 -- E 10/07/08 1 Router Cover Plates G11426-12 -- -- 7/29/04 1 Router Cover Plate, COM1 Direct Relay G11426-579 -- A 10/07/08 1 Router Case, Ventilated G11427 -- -- 3/14/03 1 COM1 Direct Board G11428 -- -- 3/14/03 1 Audio Board G11429 -- -- 3/14/03 1 ICS Audio Board G11430 -- -- 3/14/03 1 Audio Expander G11431 -- C 08/16/06 1 Audio/Video Panel Assembly G11432 -- B 10/07/08 1 Audio Attenuator G11435 -- -- 9/5/98 1 JC DIM 2 G11437 -- -- 7/29/04 1 COM1 Direct Relay Board G11460 -- C 6/10/03 1 Control Panel G11461 -- -- 6/10/03 1 Control Panel G11462 -- -- 6/10/03 1 Control Panel G11470 -- A 6/10/03 1 Control Panel G11471 -- -- 6/10/03 1 Control Panel G11472 -- -- 6/10/03 1 Control Panel G11473 -- -- 6/10/03 1 Control Panel G11474 -- -- 6/10/03 1 Control Panel G11475 -- -- 6/10/03 1 Control Panel G11480 -- A 7/29/04 1 Control Panel G11481 -- -- 6/10/03 1 Control Panel G11482 -- -- 6/10/03 1 Control Panel G11490 -- -- 7/29/04 1 Control Panel G11694 -- A 6/17/98 1 FM Antenna Interface G11695 -- D 10/07/08 1 Aft Audio Connector Box G11695-1 -- E 10/07/08 1 Aft Audio Box Top G11695-2 -- D 10/07/08 1 Aft Audio Box Bottom G11697 1 C 9/5/98 1 ENG System Panel Layout G11697 2 -- 9/5/98 1 ENG System Panel Layout 350 G11697 3 -- 9/5/98 1 ENG System Panel Layout 355 G11708 -- -- 9/5/98 1 Scanner Antenna Installation Details G11710 -- -- 9/5/98 1 Johnson 8600 LTR 800MHz Radio G11780 -- -- 9/5/98 1 Instrument Panel Hole Cutouts G11781 -- -- 9/5/98 1 Monitor Rack Support and Stop Angle G12000 1 A 6/16/98 1 Cable, Pilot audio/keying G12000 2 A 6/16/98 1 Cable, Pilot audio/keying G12001 1 A 6/16/98 1 Cable, Co-pilot audio/keying G12001 2 A 6/16/98 1 Cable, Co-pilot audio/keying G12002 -- C 05/09/06 1 Cable, Passenger Audio And Keying

G12005 -- C 05/09/06 1 Cable, Com 1 Direct To Audio Control Interconnect

G12006 -- B 05/09/06 1 Cable, Audio Control J2 To Audio Expander J3

G12007 -- C 05/09/06 1 Cable, Audio Expander To Backplane Interconnect

G12008 -- C 05/09/06 1 Cable, Radio To Backplane Interconnect



LR DRAWING NO.


DESCRIPTION

G12009 -- A 10/09/07 1 Cable, Bulkhead XLRs To/From Audio Backplane

G12010 -- B 05/09/06 1 Cable, Audio, Receive Audio To Backplane G12011 -- B 05/09/06 1 Cable, Audio, Scanner G12012 -- A 10/09/07 1 Cable, Inline XLR3F To Audio Backplane G12013 -- B 05/09/06 1 Cable, Audio To Backplane G12014 -- B 05/09/06 1 Cable, Audio, Backplane J17 G12015 -- B 05/09/06 1 Cable, Audio G12016 -- A 10/09/07 1 Cable, From Backplane To Bulkhead XLR3M G12017 -- B 05/09/06 1 Cable, Audio G12018 -- C 05/09/06 1 Cable, Power, Audio Router G12019 -- C 05/09/06 1 Cable, GNET, Standard

G12020 -- A 10/09/07 1 Cable, GNET Non-Standard D9F To D9F And D9M

G12021 -- A 10/09/07 1 Cable, GNET Non-Standard, D9F to D9F power only

G12022 -- B 05/09/06 1 Cable, GNET, Non-Standard, Data Only G12032 -- B 05/09/06 1 Cable, GNET, Non-Standard, Two Device G12033 -- C 05/09/06 1 Cable, Power G12036 -- C 05/09/06 1 Cable, Pilot Isolate G12038 -- B 05/09/06 1 Cable, GNET, Non-Standard, Male End G12041 -- A 05/09/06 1 Cable, Power, Scanner G12046 -- A 05/09/06 1 Cable, Antenna, Coax

G12047 -- A 10/9/07 1 Cable, GNET, Non-Standard, Triple D9F Data Only

G12048 -- B 05/09/06 1 Cable, Shielded G12050 -- C 1/29/09 1 Footswitch, Audio, TX or ICS Keying

G12063 -- C 10/09/07 1 Cable, GNET Non-Standard D9F To D9F And D9M, Data Only

G12064 -- A 10/10/07 1 Cable, GNET Non-Standard D9F To D9F Data only, External Power

G12088 -- C 05/09/06 1 Cable G12092 -- B 10/31/07 1 Cable, External Jumper, 12V Power G12096 -- B 05/09/06 1 Cable, Antenna, FM Radio Pigtail G12099 -- B 05/09/06 1 Cable, Antenna, Triax G12100 -- D 11/21/07 3 Connector And Wire Part List G12101 -- B 05/09/06 16 Cable Assembly Detail G12260 -- -- 9/23/03 1 SWIF12T G12262 -- B 10/07/08 18 Audio System Installation Manual G12263 -- D 11/20/07 1 Cable, Audio, Pilot/Copilot G12264 -- C 11/20/07 1 Cable, Audio, Passenger G12265 -- A 05/09/06 1 Cable, Power, Audio Router G12266 -- -- 3/14/03 1 Dimmer Interface G12268 -- A 2/25/03 1 Audio Board Headset Interface G12291 -- A 2/25/03 3 Audio System Schematic G12296 -- A 05/09/06 1 Cable, Audio, PA G12297 -- A 05/09/06 1 Cable, Audio, Receive Only G12299 -- A 05/09/06 1 Cable, Audio, Auxiliary In G12305 -- -- 3/9/01 1 Crouzet Cyclic Grip Customer Switch Selection G12306 -- -- 8/7/02 1 Cable, Antenna Coax G12320 -- B 10/07/08 1 8 Slot Audio Router Assembly



LR DRAWING NO.


DESCRIPTION

G12321 -- B 11/21/07 1 Com1Direct Wiring Diagram for G12407 Relay Module

G12322 -- -- 9/23/03 1 Speaker Amplifier Module Wiring Diagram G12340 -- -- 11/29/01 1 Angle Bracket G12347 -- -- 3/14/03 1 Auxiliary Control Module G12351 -- -- 3/14/03 1 GNET Terminal G12355 -- -- 3/14/03 1 USB Interface G12358 -- -- 3/14/03 1 Headset Expander Board G12360 -- A 05/09/06 1 Cable, GNET, Terminal G12361 -- A 05/09/06 1 Cable, Headset Expander To Audio G12370 -- -- 6/10/03 1 8 Slot Backplane G12371 -- A 7/29/04 1 Case, 8 Slot Router G12371-579 -- A 10/07/08 1 8 Slot Router Case Ventilated G12407 -- A 5/17/06 1 Relay Module G12408 -- -- 9/18/03 1 Speaker Amplifier Module G12416 -- -- 7/29/04 1 Codec Module G12467 -- B 11/09/07 1 Cable, Audio, D9F To XLR3F G12468 -- A 05/09/06 1 Cable, Audio, Dual Auxiliary Input G12475 -- A 11/08/07 1 Audio Wiring, Rear Passengers’

G12538 -- A 10/02/08 1 GNET Config Port Assembly G12538-1 -- -- 10/02/08 1 GNET Config Port Cable G12583 -- A 7/09/09 1 Cable, Audio, Inline XLR3M to inline XLR3F G12584 -- B 10/01/08 1 Copilot’s Audio Switching & Audio Connections

G12589 -- B 07/12/06 1 Cable, Audio, MW Audio Ctrl To MW Expander And Troll

G12590 -- B 10/10/07 1 Cable, Audio, MW Expander Out To BrightEye 30 Analog In

G12597 -- B 11/09/07 1 Cable, Audio Expander J2 To VU Meter G12598 -- B 10/24/07 1 Cable, BE54 Audio Out to Audio Backplane G12467 -- B 11/09/07 1 Cable, Audio, D9F To XLR3F G12603 -- A 9/30/08 1 Bell 206/407 Aft Passenger Audio G12604 -- -- 8/17/05 1 Passenger Audio Control and Dimmer System G12606 -- -- 7/28/05 1 Removable ENG Cabinet Internal Wiring

Diagram G12628 -- A 05/09/06 1 Cable, Audio, VTR To VTR Audio Control J2 G12633 -- -- 8/18/05 1 Cable, Bell 206/407 ICS Foot Switch G12634 -- -- 8/28/05 1 Cable, Audio, Strata MW Transmitter to Audio

System

G12635 -- A 05/09/06 1 Cable, Audio, Strata MW Receiver To Audio System

G12637 -- -- 9/20/05 1 Bell 407 Copilot’s Cyclic/Foot Switch Wiring G12640 -- A 10/24/07 1 VU Meter Assembly And Test Cable G12654 -- -- 10/24/05 1 Bell 407 RH/LH Nav Antenna Splitter

G12655 -- A 05/09/06 1 Cable, Audio, Strata MW Receiver To Audio System

G12656 -- B 11/09/07 1 Cable, Audio, Strata MW Transmitter G12703 -- -- 09/20/06 1 Pilot’s Cyclic Grip Layout and Wiring Diagram

G12719 -- C 11/08/07 1 Pilot’s Headset Jack, Stereo/Mono Installation

G12737 -- B 10/24/07 1 Cable, GNET, Non-Standard, Triple D9F Data Only Pigtail

G12741-5 -- A 9/25/08 1 Mounting Plate, VU Meter



LR DRAWING NO.


DESCRIPTION

G12805 -- B 10/24/07 1 Cable, MW Audio Expander to BE30-D and MWTX Audio

G12850 -- B 6/17/09 1 NAT SM274 Audio Mixing Amplifier Wiring Diagram

G12869 -- B 10/24/07 1 Cable, GNET, Non-Standard, Four D9F G12871 -- A 10/30/07 1 Cable, Audio System, Dual Foot Switch G12885 -- A 9/29/08 1 VU Meter Installation G12885-1 -- A 9/25/08 1 Mounting Plate G12885-2 -- -- 9/29/08 1 VU Meter Legend

G12910 -- A 11/08/07 1 Cable, Audio, Bulkhead XLR3F to inline XLR3M

G12911 -- D 9/30/08 1 Pilot’s Headset Jack Installation

G12912 -- A 11/08/07 1 Cable, Audio, MWTX Audio Monitor Port G12913 -- -- 10/30/07 1 Component Location Guide, AS350 G12914 -- -- 10/30/07 1 Cable, Audio, Backplane J17 G12915 -- A 10/30/07 1 Repeater Audio Board Jumper Plug G12998 -- -- 10/20/08 2 Cable, Bose Powered Headset Jack G12999 -- -- 10/20/08 1 Cable, Dual XLR3F to Link L1050 Encoder G13000 -- D 11/30/12 1 P139-HD Router G13004 -- F 12/03/12 13 P139-HD Audio System Wiring Diagrams G13005 -- A 10/07/09 1 P139-HD AS350 Installation

X G13005-1 -- A 4/08/13 1 Hat Section G13005-2 -- A 10/07/09 1 Back Plate Assembly G13005-3 -- -- 10/30/08 1 Shim G13005-4 -- A 10/07/09 1 Back Plate G13005-5 -- A 10/07/09 1 Clip G13006 -- A 4/11/12 1 P139-HD Bell 206/407 Installation G13006-2 -- B 1/13/12 1 Clip G13006-4 -- A 1/13/12 1 Doubler G13009 -- -- 1/13/12 1 Tray Assy G13009-1 -- A 4/11/12 1 Tray G13009-2 -- A 4/11/12 1 Brace G13009-3 -- -- 1/13/12 1 Shim G13010 -- -- 10/20/08 1 Cable, Link L2000 Receiver Audio XLR5F to

Dual XLR3M G13011 -- -- 10/20/08 1 Cable, Audio Expander to Dual XLR3M G13012 -- -- 10/07/08 1 Aft Audio Box Installation G13012-1 -- -- 10/07/08 1 Doubler G13012-2 -- -- 10/07/08 1 Bracket G13115 -- A 10/15/12 1 Control Panel G13116 -- A 10/15/12 1 Control Panel G13028 -- -- 5/19/09 1 Pilot Mic MW Transmit Disable Switch

Installation G13031 -- -- 7/09/09 1 Cable, Audio, Bulkhead XLR3F to Inline XLR3F G13033 -- -- 7/15/09 1 Cable, Audio, MW Expander to BE71 G13034 -- -- 7/15/09 1 Cable, SWIF12-T J2 G13045 -- -- 10/14/09 1 Audio Mixing Amplifier G13046 -- A 11/03/09 3 Audio Mixing Amplifier Installation G13130 -- -- 5/13/12 2 Router Installation EC135 G13130-1 -- -- 5/13/12 1 Mounting Plate Assy G13130-2 -- -- 5/13/12 1 Support Plate Detail



LR DRAWING NO.


DESCRIPTION

G13130-3 -- -- 5/13/12 1 MUX Plate

LOG OF REVISIONS

REVISION LEVEL

DATE OF REVISION

PAGES DESCRIPTION OF CHANGE APPROVAL

Initial Release 4/3/98 All Pages GLH A 4/27/98 All Pages TO CORRECT G11262, G11695

REVISION LEVELS GLH

B 6/18/98 All Pages except: G12100

TO CORRECT REVISION LEVELS. DRAWING G11251 CONSOLIDATED INTO G11426B; G11332 CONSOLIDATED INTO G11262B; CORRECTED TYPOS ON G12101 SHTS 3 AND 6.

GLH

C 6/25/98 G182 SHTS 1-3

ADDED “SHEET” COLUMN TOMDL TO ENABLE TRACKING OF REVISIONS BY SHEET No.

DCF

D 7/10/98 G11262, All pages; G11306, Sht 1; G11697, Sht 1.

CORRECTED REFERENCE DESIGNATORS;CLARIFIED WIRE ROUTING DESCRIPTIONS; STA. No.’S; LOCATION OF SWIF 12 MODULE; POSITION OF CO-PILOT’S HEADSET JACKS.

GLH

E 10/21/98 ALL Revised GA182-2, GA182-4, GA1-2TP, G10063, G11261, G11262, G11306, and G11697;

Added new: GA1-8TP, GA1-9TP, G10063, G11306, G11321, G11322, G11350, G11435, G11708, G11780, G11781, G12041, G12046, G11281, G11710

GLH

F June 3, 1999

GA182-2 Added more detail to Installation Instructions

GLH

G 10/24/2005 All Incorporated ECO’s 1082, 1090, 1104, 1107, 1112, & 1117.

Added Bell 206/407 to AML and GA182-5, GA182-6, G12467, G12468, G12546, G12584, G12589, G12597, G12603, G12604, G12606, G12628, G12633, G12634, G12635, G12637, G12640, G12654, G12655, & G12656

CLB



REVISION LEVEL

DATE OF REVISION


H 2/9/2009 ALL Incorporated ECO’s 1144, 1428 & 1432 Adding new P139-HD Digital Audio System, added ICA182-2 & ICA182-3

CLB

J 8/11/2011 ALL Revised RFMS GA182-3, GA182-6 & GA1-9TP for EASA approval; Incorporated ECO’s 1448, 1453, 1471 & 1483

CLB

K 5/15/2012 ALL Removed ICA’s and RFMS’ from MDL as these are approved independently from the MDL; Incorporated ECO-1495 and ECO-1498 adding the EC135 and EC145 models to the AML

CLB

L 12/03/2012 ALL Incorporated ECO-1442 adding the Bell 204 / 205 / 212 / 214 / 412 models to the AML; Incorporated ECO-1503

CLB

M 6/13/2013 ALL Removed EC145 Model and Bell 204 / 205 / 212 / 214 / 412 models from STC by: Revising GA182-11 &-12, Removed ICA182-4 &-6, G13008. Corrected typo on G13005-1

CLB

823 McTavish Road NE, Calgary, Alberta, Canada T2E 7G9 Tel: 800 564 6469 ECO-1514 GA182.doc Page 1 of 1

ENGINEERING CHANGE ORDER

Date: 2/03/2014

ECO No: ECO- 1514 Rev: --

STC: SR00521SE MDL: GA182 Rev: M

STC Title: Audio System

Effective for: Production; or Listed Aircraft Only:

Primary Document Effected: See list below

Description of Change: Adds Audio Mixer G13120 to STC

Detailed Explanation:

This ECO adds Audio Mixer G13120 to the STC as an optional device used to mix audio signals from up to 8 sources into 3 outputs. The first two inputs and outputs are considered essential, and will remain functional even when the mixer is not powered or detects an internal fault due to the failsafe relays and detection internal to the mixer. See drawing G13121 for more information about the operation and installation of the mixer.

ECO DOCUMENT LIST

NOTE: X in CH (change) column indicates change from last revision level. Documents with multiple pages, that have a different revision level on some pages, are listed by individual pages on this list.

CH DOC No. PAGES REV DATE DESCRIPTION X G13120 1 -- 1/13/14 Audio Mixer X G13121 3 -- 1/27/14 Audio Mixer Installation Instructions

ECO LOG OF REVISIONS

REVISION LEVEL

DATE OF REVISION


- 2/03/2014 ALL Initial Release CLB



Date: 3/26/2014






Description of Change: Minor changes to drawings listed


This ECO corrects minor changes to the drawings listed.

G13004: Rewrote EMERG/NORMAL notes on sht 13 for clarity.

G13115: Revised labeling notes to engineering standards.

G13116: Revised labeling notes to engineering standards.

G13121: Corrected part number on back shell on sht 2.

ECO DOCUMENT LIST


CH DOC No. PAGES REV DATE DESCRIPTION X G13004 13 G 3/26/14 P139-HD Audio System Wiring Diagrams X G13115 1 B 3/26/14 Audio Control Panel X G13116 1 B 3/26/14 Audio Control Panel X G13121 3 A 3/26/14 Audio Mixer Installation Instructions


REVISION LEVEL

DATE OF REVISION





Date: 5/08/2014






Description of Change: Adds audio system configurations STC


This ECO defines three audio system configurations as follows:

P139-HD (D) Uses Router G13000 in a “Dual-board” configuration. This is the standard audiosystem that was previously specified in the STC and is shown in the diagrams. The G13000is the primary router used throughout the instructions.

P139-HD (S) has been added as an optional system configuration. It uses Router G13000 ina “Single-board” configuration that uses the same case as the dual-board router, but with onlyone audio board installed. These two routers share the same installation and wiring drawings.

P139-HD (T) has been added as an optional system configuration. It uses Router G13160and is a “Three board” router. This installation replaces wiring drawing G13004 with drawingG13162. Installation of this router is performed the same as the others two routers with slightchanges in the mounting hardware as noted in the instructions. The G13160 router supportsmore radios, control panels and headsets than what the G13000 provides.

This change is considered a minor change since the primary functionality of the system has not changed; there is negligible change to weight, balance and power consumption; and there are no changes required for the RFMS.

To support this change:

GA182-7 , GA182-8 & GA182-11 have been revised to: add Section 1.3 defining the configurations; Revised the wording throughout the manual to define the installation differences between the different configurations. Updated the control panels section to show just the current panels offered. Figures throughout the manual have been updated for continuity.

G13004 has been updated to change the headset numbering scheme and to add external power for additional control panels.

G13160 Router drawing has been added for the three board router.

G13161 Tray has been added to be used in place of Tray G13009 for the G13160 Router.

G13161-1, -2, -3, -4 &-5 detail drawings have been added.


G13162 wiring diagrams have been added to be used in place of G13004 for the G13160 Router.

ECO DOCUMENT LIST


CH DOC No. PAGES REV DATE DESCRIPTION X GA182-7 17 D 4/23/14 P139-HD Installation Instructions, AS350/355 X GA182-8 16 D 4/23/14 P139-HD Installation Instructions, Bell 206/407 X GA182-11 18 D 4/23/14 P139-HD Installation Instructions, EC135 X G13004 13 H 4/24/14 P139-HD Audio System Wiring Diagrams X G13160 1 -- 12/9/13 P139-HD 3-Board Router X G13161 1 -- 12/12/13 Wide Tray Assy X G13161-1 1 -- 12/12/13 Wide Tray X G13161-2 1 -- 12/12/13 Wide Brace X G13161-3 1 -- 12/12/13 Wide Shim X G13161-4 1 -- 12/12/13 Wide Clip X G13161-5 1 -- 12/12/13 Doubler X G13162 13 -- 3/27/14 P139-HD Audio System Wiring Diagrams


REVISION LEVEL

DATE OF REVISION





Date: 8/13/2014






Description of Change: Updates Routers


This ECO updates Audio Routers G13000 and G13160 to change the operating voltage from 10 – 30 VDC to 14 – 32 VDC.

ECO DOCUMENT LIST


CH DOC No. PAGES REV DATE DESCRIPTION X G13000 1 E 8/13/14 P139-HD Router X G13160 1 A 8/13/14 P139-HD 3 Board Router


REVISION LEVEL

DATE OF REVISION





Date: 4/10/2015






Description of Change: Added keylines to drawing. Added notes on signal shielding and Gnet bus wiring. Connector part number changes.


Both the G13000 and G13160 audio routers have been modified to provide additional spare keylines for user-defined functions. The G13004 and G13162 wiring drawings have been updated to show these new connections.

In addition, the following changes were made to both documents:

An additional note has been added to sheet 1 giving directions to the installer on the approved grounding of shielded wires.

Part numbers for D-Subminiature screw locks, and the D9M connector have been updated.

The notes on Gnet bus connections on sheet 12 have been clarified with respect to not needing a terminal block in busses with a single Gnet device, appropriate device ID numbering and allocation of devices among Gnet busses.

ECO DOCUMENT LIST


CH DOC No. PAGES REV DATE DESCRIPTION X G13004 13 I 4/10/2015 P139-HD Audio System Wiring Diagrams X G13162 13 A 4/10/2015 P139-HD Audio System Wiring Diagrams


REVISION LEVEL

DATE OF REVISION



Eagle Copters Ltd. www.eaglecopters.com

GA182-7 Rev D P139-HD Digital Audio System 1 of 17

GA182-7 Revision D, 4/23/2014

P139-HD Digital Audio System AS350/355 Installation Manual



1.0 INTRODUCTION

1.1. This document provides general information and instructions for the installation of the Eagle Audio P139-HD Digital Audio System, under STC SR00521SE.

1.2. Installation is to be accomplished in accordance with Eagle Copters Ltd. instructions. Throughout the installation of this product it is necessary to utilize proper aviation practices. Be sure that the installation of this product is in compliance with the aircraft manufacturer’s limitations and also that itis done in accordance FAA publication, AC 43.13-1B, Acceptable Methods, Techniques and Practices, Aircraft Inspection and Repair. These rules from the AC apply :

A. All wire to be 22 AWG unless otherwise specified. B. Unshielded wire per MIL-W-22759/16; Shielded wire per MIL-

M27500-xxTGxT14 ; xx- indicates wire gauge, x- indicates number of conductors.

C. Route and support wiring harness IAW AC 43.13-1b, Chapter 11 Section 8, Paragraph 11-96.

D. Clamp wiring harness IAW AC 43.13-1b, Chapter 11, Section 11, Paragraph 11-146.

E. Clamp and route wiring harness around movable controls IAW AC 43.13-1b, Chapter 11, Section 9, Paragraph 11-125.

F. Wiring and harness to be separated IAW AC 43.13-1b, Chapter 11, Section 8, Paragraph a 11-105 & 11-106.

G. Install service loops at harness terminations IAW AC 43.13-1b, Chapter 11, Section 9, Paragraph 11-139.

H. Install grounding connections and bonding IAW AC 43.13-1b, Chapter 11, Section 15, Paragraph 11-186 & 11-189.

Before installing any of the components, first read through all of the documentation to become familiar with the installation requirements. This installation requires a completed FAA Form 337 and appropriate log book entries.

Prior to installing each component, record weight and mounting location in the aircraft’s weight and balance record.

This product is provided with an FAA STC for certain aircraft models. If your installation is not covered by one of the models listed on the STC, then you may need to obtain a field approval from your local FAA Flight Standards District Office (FSDO).



The P139-HD Digital Audio Router contains no user serviceable internal components. Do not disassemble router or the factory warranty will be voided. For service, return the unit to Eagle Copters Ltd.

1.3. There are three types of P139-HD Audio Systems that the installer may choose to install at their discretion.

1.3.1. P139-HD (D) Uses Router G13000 in a “Dual-board” configuration and is shown in the diagrams and is the router used throughout the instructions.

1.3.2. P139-HD (S) Uses Router G13000 in a “Single-board” configuration that uses the same case as the dual-board router, but with only one audio board installed. These two routers share the same installation and wiring drawings.

1.3.3. P139-HD (T) uses Router G13160 and is a “Three board” router. This installation replaces wiring drawing G13004 with drawing G13162. Installation of this router is performed the in the same manner as the other two routers with slight changes in the mounting hardware as noted in the instructions.

1.4. Prior to installation of this system, it is the responsibility of the installer to confirm by analysis or measurement, that the additional power requirement will not exceed the capacity of the avionics bus or the aircraft’s electrical system. Power consumption for this audio system is 5 amps at 28 volts. The system is designed to use redundant power sources, both coming from the master avionics bus. For each supply line, use a separate 5 amp fuse or circuit breaker on a 28 volt aircraft and separate ground lines to two separate ground points. Refer to G13004 for wire harness details. The system will support supply voltages of 14 – 32 VDC.

1.5. The internal power supply of the router is sufficient to power six audio control panels. If the installation calls for more than six panels, the additional panels must be powered from a separate circuit breaker to the Router. Refer to G13004 sheet 12 for more information.

1.6. The FAA requirement regarding the securing of wire bundles using nonmetallic clamps is addressed by the use of nylon cable ties. The part numbers and description of these ties is as follows:

Following the guidelines in AC43.13-1B, cable ties are attached at a maximum of 4” spacing and ties are attached to nylon cable tie anchors, as necessary.



Cat.No. UPC

Body Width

In. Length

In.

Max. Wire

Bundle Dia. In.

Military Standard Part No.

Tensile Strength

Lb. TY23M 82436 .091 3.62 .625 MS3367-4 18 TY24M 82447 .140 5.50 1.125 MS3367-5 40 TY25M 82457 .184 7.31 1.750 MS3367-1 50

1.7. The aircraft into which this product will be installed may be a new aircraft or an aircraft that has been in service. The configuration of the wiring and cabling will vary from aircraft to aircraft. The installation of the Eagle Audio System should use existing wire and cable runs when possible as it will not interfere with the existing aircraft wiring.

1.8. These instructions call out cables by reference to the drawing that defines the cable construction details. The installer may, at the installer’s discretion, substitute connectors, wire type, and connection details, so long as the final installations operate correctly and meets FAA standards.

1.9. The Router features a COM1 Isolate mode that automatically connects the pilot’s headset and mic switches directly to COM1 in the event of power loss or failure of the Audio Router. The pilot may also activate the COM1 Direct mode using the EMERG/NORMAL switch on the G13115 and G13116 control panels. This feature may also be set up for the Copilot to activate a COM2 Isolate mode using the EMERG/NORMAL switch on the copilot control panel.

1.10. For Non-Pilot positions, Control Panels G13115NS or G13116NS may be used. The panels do not have an internal COM1, COM2 isolate switch. For these panels, do not connect to the COM1 or COM2 circuits shown in wiring diagrams G13004.



2.0 System Overview

Figure 1 Digital Audio System Overview

2.1. The schematic shown in Figure 1 is a typical system. The installer may, at the installer’s discretion, add or remove radios, control panels, headset groups, or ICS and Transmit PTT switches as needed.

2.2. Control Panels G13115 and G13116 may be used interchangeably, depending on the control functions desired and number of radios installed.

2.3. It is the installer’s responsibility to document the system configuration as installed for maintenance purposes.



3.0 Component Installation & Hookup

J6 NETWORK PORT

J7 MEMORY PORT

J3

J1

J4

J2

J5

Figure 2 G13000 Router Connector Layout



3.1. G13000 Router Connections (see Figure 2)

3.1.1. J1 is used to connect COM1 and radios XCVR3 – XCVR11.

3.1.2. J2 is used to connect COM2 and radios XCVR12 – XCVR20.

3.1.3. J3 is used to connect the Pilot’s control panel, Pilot’s headset group,headset groups 3 – 7 and passenger control panels.

3.1.4. J4 is used to connect the Copilot’s control panel, Copilot’s headsetgroup, headset groups 8 – 12 and additional passenger control panels.

3.1.5. J5 is used to connect power, ground, Pilot’s COM1 Isolate, andCopilot’s COM2 Isolate.

3.1.6. J6 is a network port used for system configuration adjustment.

3.1.7. J7 is a memory card slot used for storing system configuration data onto removable media.

3.1.8. The Router contains no user serviceable internal components. Do not disassemble router or the factory warranty will be voided. Return the unit to Eagle Copters Ltd. for service.



J8 NETWORK PORT

J9 MEMORY PORT

J6

J5

J2

J1

J7

J3

J4

Figure 3 G13160 Router Connector Layout



3.2. G13160 Router Connections (see Figure 3)

3.2.1. J1 is used to connect radios COM1 and radios XCVR3 – XCVR11.

3.2.2. J2 is used to connect the Pilot’s control panel, Pilot’s headset group, headset groups 3 – 7 and passenger control panels.

3.2.3. J3 is used to connect radios COM2 and radios XCVR12 – XCVR20.

3.2.4. J4 is used to connect the Copilot’s control panel, Copilot’s headsetgroup, headset groups 8 – 12 and additional passenger control panels.

3.2.5. J5 is used to connect radios XCVR21 – XCVR30.

3.2.6. J6 is used to connect headset groups 13 – 18 and additional passenger control panels.

3.2.7. J7 is used to connect power, ground, Pilot’s COM1 Isolate, andCopilot’s COM2 Isolate.

3.2.8. J8 is a network port used for system configuration adjustment.

3.2.9. J9 is a memory card slot used for storing system configuration data onto removable media.

3.2.10. The Router contains no user serviceable internal components. Do not disassemble router or the factory warranty will be voided. Return the unit to Eagle Copters Ltd. Aviation for service.



3.3. Component Installation & Hookup

Router Installation in Aft Baggage Compartment

3.3.1. Refer to drawing G13005 for installing the Router into the Aft Baggage compartment. Router G13000 is shown in drawing G13005 and in the figure above. Router G13160 may be installed in place of G13000 using the same methods and hardware define in drawing G13005.



Figure 4

3.3.2. Optional: The installer may install the Router onto an avionics shelf or bay with a 5 lb. minimum load rating. Install using hardware shown in Figure 4.

3.3.3. Note: for the G13160 Router replace in Figure 3 the following items: G13009 with G13161; G13009-3 with G13161-3; G13006-2 with G13161-4 and use (3) MS24693S51 screws to install; use (2) NAS622CE2 Support Hooks.

3.3.4. For Router G13000, refer to drawing G13004 for the detailed wiring schematic used in this installation. For Router G13160, refer to drawing G13162 for the detailed wiring schematic used in this installation.

3.3.5. Be sure to carefully document the Radios and Control panels as installed and their related connections for future maintenance and troubleshooting purposes.



3.4. Control Panels

3.4.1. The Control Panels mount onto standard DZUS rails and should be mounted in locations designed for standard avionics mounting. The control panels connect to the router via the 4-wire GNET bus.

3.4.2. There can be more than one of these control panels in any combination connected to the system. Each audio board has two GNET ports giving 2, 4, 6 GNET ports for the P139 (S)/(D)/(T) routers respectively. If the configuration calls for more control panels than there are available GNET ports on the router, connect J1 of each control panel to a GNET port in parallel for pins 1 – 4. Pins 5 – 9 will be unique ID for each control panel connector. See G13004 sheet 9 for details.

3.4.3. The pilot control panel also controls the COM1 Isolate function. Optionally the copilot control panel controls the COM2 isolate function. See Section 1.8 for more information.

3.5. Control Panels G13115 & G13115NS

3.5.1. The G13115 & G13115NS Control panels provide separate transmit, receive and volume controls for up to 16 radios or other devices, as well as crew intercom functions and optionally installer-defined special functions. The G13115NS version does not have an EMERG/NORMAL switch and must not be used as a pilot or copilot primary panel.



3.6. Control Panels G13116 & G13116NS

3.6.1. The G13116 & G13116NS Control panels provide separate transmit, receive and volume controls for up to 8 radios or other devices, as well as crew intercom functions and optionally installer-defined special functions. The G13116NS version does not have an EMERG/NORMAL switch and must not be used as a pilot or copilot primary panel.

3.7. Headset Ports

3.7.1. The Pilot and Copilot Headset Group consists of the headset jack, ICS switch and transmit switches on the cyclic and/or foot switches.

3.7.2. For each passenger, a unique Passenger Headset Group is needed. The Passenger Headset Group consists of the passenger’s headset jack, an ICS switch and a transmit switch.



3.8. COM1, COM2 and other radio ports

3.8.1. The G13000 digital audio router supports up to 20 radios and the G13160 router supports up to 30 radios. Each radio should be installed in accordance with the manufacturer’s instructions.

3.8.2. For the G13000 the following connections are available:

3.8.2.1. The COM1 radio connects to J1 on the Router along with radios XCVR3 - XCVR11 (refer to G13004 sheet 4).

3.8.2.2. The COM2 radio connects to J2 on the router along with radios XCVR12 - XCVR20 (refer to G13004 sheet 5).

3.8.3. For the G13160 the following connections are available:

3.8.3.1. The COM1 radio connects to J1 on the Router along with radios XCVR3 - XCVR11 (refer to G13162 sheet 5).

3.8.3.2. The COM2 radio connects to J3 on the router along with radio ports XCVR12 - XCVR20 (refer to G13162 sheet 6).

3.8.3.3. Radios XCVR21 - XCVR30 connect to J5 on the router (refer to G13162 sheet 7).

3.8.4. While the term radio is used throughout this document, any type of audio device can be connected, such as tape recorders, scanners, telephones, hand-held radios, etc.

There is normally no need for any type of universal radio adapter between an audio device and the router.



4.0 Functional Check

4.1. Perform a check of all power and ground leads to confirm they are connected properly before applying power to the system. Incorrect wiring may cause damage to the units.

4.2. Connect headset adapter cables, headsets and switches. Apply power to audio system, radios and related accessories. Activate ICS and confirm proper operation. Place ‘PILOT EMERG/NORMAL’ switch in ‘EMERG’ position. Key transmit switch and confirm proper operation of COM1.

4.3. Place the ‘PILOT EMERG/NORMAL’ switch in ‘NORMAL’ position andcheck all transceivers, receivers and audio devices.

4.4. If the system is equipped with a ‘COPILOT EMERG/NORMAL’ switch,repeat the steps in sections 4.2 and 4.3 for Copilot position and COM2 respectively.

4.5. Check all pilot, copilot and passenger audio control panels for proper audio levels and operation. Should adjustments be required, follow the instructions in document GA063-3.



5.0 Load Analysis

5.1. At the completion of the installation of the audio system, the installer shall perform a load analysis test of the electrical branch circuit that powers the audio system, and also the entire aircraft electrical load, to confirm that the addition of the audio system will not cause an overload to the electrical branch circuit or the aircraft generator.

5.2. The current shall be measured using a properly calibrated ammeter. A clamp-on amp meter, such as Amprobe Instrument model number ACDC-600A, or equivalent will make this job easier.

5.3. Perform the branch circuit load analysis test by powering up all equipment that is intended to be operated at the same time on the branch circuit that the audio system is connected to. Additionally, key the three highest power communication transmitters at the same time, if possible, while the current measurements are being taken.

5.4. Measure the current of the branch circuit powering the audio system, by clamping the meter around the branch circuit wire near its origin. Confirm that the current draw during the above described test conditions is less than the current limiter (fuse or circuit breaker) rating for that branch circuit.

5.5. If the current draw is greater than the current limiter rating, it becomes the installer's responsibility to re-distribute some of the other equipment powered by this branch circuit to another suitable branch circuit, in order to reduce the load on the audio system's branch circuit to less than the current limiter rating.

5.6. Once the branch circuit loads are within limits, test the current load for the entire aircraft while all power for the aircraft is being supplied by the aircraft generator, battery, or external power source. Perform this load analysis test by powering up all equipment on the aircraft that is intended to be operated at the same time as the audio system. Additionally, key the three highest power communication transmitters at the same time, if possible, while the current measurements are being taken. Clamp the ammeter around the power source. Confirm that the current draw during the above described test is less than the generator rating.

5.7. Upon satisfactory completion of these load analysis tests, make an aircraft logbook entry that these tests have been performed satisfactorily in accordance with this STC.



6.0 Interference Test Procedure

6.1. Perform electrical interference test using GA1-2TP test procedure.

7.0 Final Inspection

7.1. Perform final inspection of installation confirming:

7.1.1. There are no chaffing issues.

7.1.2. There are no mechanical interference issues.

7.1.3. Security of fasteners.

7.1.4. Removal of all tools.

7.1.5. Chips, shavings and other debris are removed.

7.1.6. Proper reassembly of aircraft.

7.1.7. Aircraft is airworthy prior to returning to service.

8.0 FAA Requirements

8.1. Amend the weight and balance records and make the necessary log book entry. Complete an FAA form 337 showing the installation of this equipment in accordance with the STC instructions and submit one copy to the FAA and one copy to the aircraft owner. File all data and a copy of the STC with the aircraft records.

LOG OF REVISIONS

REVISION LEVEL

DATE OF REVISION


-- 11/05/08 All Pages Initial Release CLB A 1/13/12 All Revised Figure 3 showing new

style tray CLB

B 6/25/12 ALL Updated 1.7, & 3.3 for G13115 & G13116

CLB

C 10/15/12 3, 9 Added 1.8; Added G13115NS and G13116NS to 3.3

CLB

D 4/23/14 ALL Added G13160 3-Board Router CLB

GA1-2TP Rev C

GA1-2TP REV: C

5/13/2012

EMI Test Procedure

823 McTavish Road NE, Calgary, Alberta, Canada T2E 7G9 Tel: 800 564 6469 Page

1 of 7

GA1-2TP Rev C Page 2 of 7

LOG OF REVISIONS

REVISION LEVEL

DATE OF REVISION


- 8/08/1997 ALL Initial Release GLH A 9/08/1997 2 Added “LIST OF REVISIONS” Page GLH B 10/16/1998 3, 4 Added coverage for FADEC aircraft

under Scope. Revised procedure under Transponder test.

GLH

C 5/13/2012 ALL Revised Scope to remove FADEC references; Revised FAR references to CFR; Updated checklist for “other” equipment; Updated format of document to current standards;

CLB


Scope This document is a test plan to be used to establish that newly installed electrical equipment does not interfere with essential aircraft equipment in any way that would impair safety of flight of the aircraft. Satisfactory completion of this test plan confirms that the newly installed equipment satisfies the EMI requirements of the Federal Aviation Administration. This test plan is applicable to FAR part 29 Rotorcraft.

Applicable Documents CFR 29.1309(c), 29.1351(b)(1), 29.1351(b)(2) and AC25-10 Paragraph 5, sections: (m)(4) & (n).

Witnessing of EMI Test This test shall be witnessed by someone who is authorized by the FAA to return the aircraft to service. This would include an FAA licensed Avionics Technician, A&P Mechanic, Inspector of Airworthiness, or the Repair Station’s Director of Maintenance. In addition, an FAA representative, such as a DAR or DER may witness the test.

Equipment Under Test The newly installed Equipment Under Test (EUT) by this test plan shall be in proper working order throughout the test. If the EUT fails during this test, then this test shall be repeated with the EUT in proper working order.

Test Procedure Testing shall normally be conducted with the aircraft running on the ground, or with battery or external ground power where appropriate. In the event that an aircraft system or component can only be evaluated for the effects of interference with the aircraft in flight, then the evaluation of that system or component shall be conducted with the aircraft in flight. Testing conducted with the aircraft in flight shall be performed with safety of flight in mind and with only necessary personnel on board.

Testing shall be conducted on the aircraft with all aircraft systems and equipment operating normally, and cycled as necessary to conduct the test. The EUT shall be operated normally. The EUT shall be cycled on and off. The EUT shall also be cycled through all of its operating modes.

Each aircraft system or component being evaluated for the effects of EMI will be observed as the EUT is cycled. A transient motion or flicker is acceptable provided no permanent deviation is established. There can be no stand-off conditions displayed on an instrument. In the case of audio equipment being evaluated for the effects of EMI, a change in the audio (such as background noise) that does not interfere with the intended purpose of the audio is acceptable.

For each aircraft system or component being evaluated for the effects of EMI, mark the item as PASS or FAIL based upon the outcome of this test procedure.

If an aircraft system or component being evaluated for the effects of EMI Fails this test procedure, then corrective action must be taken to reduce the interference to an acceptable level which allows the aircraft system or component being evaluated for the effects of EMI to PASS this test. When re-testing after corrective action, the only tests to be repeated are the tests that Failed previously. Items that previously Passed do not need to be re-tested, unless the method of corrective action results in changes to the EUT, which might cause the EUT to Fail previously Passed items. Mark the N/A __ field on the re-test test plan for the items that previously Passed and are not being re-tested.


Items To Evaluate The following is a list of aircraft systems or components that must be evaluated for the effects of EMI if they are installed and are to be used at the same time as the EUT. If the item listed below is not installed or otherwise not applicable, then mark the N/A __ field.

Engine Temperature Indicator N/A __ Pass __ Fail __ Engine RPM Indicator N/A __ Pass __ Fail __ Engine Torque Indicator N/A __ Pass __ Fail __ Engine Fuel Control N/A __ Pass __ Fail __ Engine Oil Pressure Indicator N/A __ Pass __ Fail __ Engine Oil Temperature Indicator N/A __ Pass __ Fail __ Rotor RPM Indicator N/A __ Pass __ Fail __ Fuel Quantity Indicator N/A __ Pass __ Fail __ Fuel Pressure Indicator N/A __ Pass __ Fail __ Generator Voltage Indicator N/A __ Pass __ Fail __ Battery Voltage Indicator N/A __ Pass __ Fail __ Directional Gyro / Heading Indicator N/A __ Pass __ Fail __ Attitude Indicator N/A __ Pass __ Fail __ Turn and Bank Indicator N/A __ Pass __ Fail __ Annunciator Indicators N/A __ Pass __ Fail __ Flight Time Hour Meter N/A __ Pass __ Fail __ Warning Horn N/A __ Pass __ Fail __ Outside Air Temperature Indicator N/A __ Pass __ Fail __

Transponder N/A __ Pass __ Fail __ Set controls to mode C code 1200, or other code assigned by ATC. Cycle EUT and confirm proper data transmitted, either by use of transponder ground test equipment, or by confirmation from ATC of proper reception of correct data. Check for proper operation of reply light.

VOR N/A __ Pass __ Fail __ Set Voice/Ident to Voice. Check frequencies for audible interference sounds. Set local VOR frequency for full needle displacement. Adjust course select knob for gradual reduction of needle displacement to half, fourth, and zero. Note stability at each displacement and that zero can be achieved without a standoff.

DME N/A __ Pass __ Fail __ Perform self test with EUT cycled. Note that no skips in miles display occurs. Observe that mile indications do not drift and there is no audible interference in Ident tone.

Magnetic Compass N/A __ Pass __ Fail __ Swing compass and adjust with EUT operating normally. If EUT causes erratic operation of magnetic compass, then mark compass as Fail.


VHF Communications System N/A __ Pass __ Fail __ Tune each comm receiver to a low, middle, and high frequency within its frequency range. Listen for audio interference. Transmit on low, middle, and high frequencies. Listen on an external receiver for audio interference.

GPS Navigation Receiver N/A __ Pass __ Fail __ Check for proper operation. Observe signal to noise ratio readings to determine if reception is interfered with.

Crew Interphone System N/A __ Pass __ Fail __ Check for normal operation of the interphone system. Listen for excessive background noise.

ADF N/A __ Pass __ Fail __ Check for needle offset. Listen for audio interference.

Glide Slope/LOC N/A __ Pass __ Fail __ Check for needle offset. Perform test using TAC/30b or equivalent ground test equipment, or during flight while established on an ILS glide slope.

Radio Altimeter N/A __ Pass __ Fail __ Perform test with appropriate ground test equipment, or check reading in flight.

The space below is provided to include additional systems or devices not listed previously. These would include any Transceivers, Nav Aids, Radar, or Auto Pilot systems. Use the Manufacturers test procedures for each component listed with the EUT operating normally.

Other Equipment: _________________ N/A __ Pass __ Fail __

Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________



Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Describe test: _____________________________________________________

________________________________________________________________


Aircraft Tested:

Model _______________, Registration ___________, Serial Number ______

Location of Test _______________________, Date _____________

Equipment Under Test: List: MODEL, PART NUMBER, SERIAL NUMBER

_________________________________________________________________

_________________________________________________________________

_________________________________________________________________

_________________________________________________________________

__________________________________________________________________

__________________________________________________________________

__________________________________________________________________

__________________________________________________________________

Test performed by ________________________________________________ Name Credentials

Test witnessed by ________________________________________________ Name Credentials

I hereby certify that I have witnessed the above documented test and that the results documented above reflect my observations.

_______________________ _______________________ Signature Date

10.00

8.50

2.63

J2 J1

J5

J4 J3

J6 NETWORK PORT

J7 MEMORY CARD SLOT

OPTIONAL: SUPPORT HOOK (NAS622CE2)

INSTALLED WITH (2) #6-32 X .5FLAT HEAD SCREWS (MS24693S28)

AND NUTPLATES (MS21071L06) OR LOCKNUTS (MS21042L06)

OPTIONAL: CLIP G13006-2


AND NUTPLATES (MS21059L08)E

1:1GA182/212

G13000

P139-HD ROUTER

10/30/08CLB

Sheet 1 of 1

CLB 10/30/08

G13000 P139-HD ROUTERWEIGHT = 5 LBS MAXPOWER = 5 AMPS MAXVOLTAGE = 14 - 32 VDC

OPTIONAL SINGLE AUDIO BOARD CONFIGURATION: J1 AND J3 ARE REPLACED WITH COVER PLATE G13000-9

Title

THIS DOCUMENT INCLUDES INFORMATION PROPRIETARYTO EAGLE COPTERS LTD. AND SHALL NOT BE USED OR DUPLICATED BY

ANYONE WITHOUT THE WRITTEN PERMISSION OF Eagle Copters Ltd.

DATE

CHECKED

Design

Drawing Number

Pro No:

REV

DSIZE

UNLESS OTHERWISE SPECIFIEDDIMENSIONS ARE IN INCHES

TOLERANCES ARE:

FRACTIONS1/8"

DECIMAL.X .050.XX .030.XXX .010

ANGLES2

BREAK SHARP EDGES

REVISIONSREV DESCRIPTION APPROVED/DATE

DRAWN

Approval

A

B

C

123

1234

A

B

C

D

4

D

Scale:

DATE

DATE

DATE

A REVISED LABEL ON J7 5/12/09CLB

ADDED SINGLE BOARD CONFIGURATIONNOTE

6/10/11CLBB

REVISED FRONT SCREWS FOR G13009 TRAY 1/13/12CLBC

D 11/30/12CLB

ADDED OPTIONAL FRONT AND BOTTOM CLIPS FOR TRAY INSTALLATION

VOLTAGE RANGE WAS 10 - 30 VDC 08/13/14CLBE

NOTES:Unless otherwise noted: All wires are 22 awg; all shielded wire is MIL-DTL-27500; all unshielded wire is MIL-W-22759/16.

All Grounding and Bonding will be I/A/W AC 43.13-1B, Chapter 1, Section 15.

Ground the shield return to the metal connector backshell if used, or otherwise to the metal connector housing.

SPARE KEY line function and connections are installer defined and depend on the specific system configuration.

D50M connector assembly consists of: Connector M24308/4-5F; Cinch backshell DD-24661-34; 2ea. Cinch Screwlocks D20420-42. Alternate Backshell: Conec 165X10179X.

D50F connector assembly consists of: Connector M24308/2-5F; Cinch backshell DD-24661-34; 2ea. Cinch Screwlocks D20420-42. Alternate Backshell: Conec 165X10179X.

D9F connector assembly consists of: Connector M24308/2-1F; Cinch backshell DE-24657-30; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec 165X10139X.

2.

1.

When COM1DIR (P5, Pin 10) is not grounded, the Pilot headset is inEMERGENCY mode and the following lines are diverted:HEADSET 1 connects directly to RX1, RX11 (Unswitched Alert Tones) and the emergency intercom. MIC 1 connects directly to TX 1 and the emergency Intercom.XMIT KEY 1 and PLT COM1 KEY connect to TX KEY 1. ICS KEY 1 keys the emergency intercom, if at least one Power Input Circuit Breaker to the G13000 Audio Router has power. TX11 (CVR) transmits HEADSET1, MIC1 and Emergency Intercom if at least one Power Input Circuit Breaker to the G13000 Audio Router has power.

MAKE NO CONNECTION. The pin is not connected to anything internally and therefore shall have no connection externally

DEFINITIONS:N/C:

RESERVED: MAKE NO CONNECTION. Internal circuitry may be added in the future, or may be present and relevant for testing but not relevant to operation for flight.

4

5

6

7

8

9 TERMINAL BLOCK assembly consists of: Deutsch block CTJ122E05E; Deutsch socket contacts CTS-S22/22 or M39029/22-191. A Gnet channel that is connected to only one control panel or other device may be wired directly without using a terminal block.

10 D15F connector preferred assembly consists of: Connector M24308/2-2F; Cinch backshell DA-24658-31; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec P/N: 165X10149X. Splices on 20 AWG wire shall also be 20 AWG, length 3 inches maximum. Alternate assembly consists of: Kobiconn Solder-Cup Connector 156-1315T-E and Cinch backshell DA-24658-31; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec P/N: 165X10149X. Conductors shown with splices may be implemented by soldering the supply wire to both pins after soldering and insulating the adjacent connections.

G13004 I

P139-HD AUDIO SYSTEMWIRING DIAGRAMS - NOTES

GA182 1 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

11 The Audio System works with a range of supply voltages, as specified in the installation instructions. Breaker ratings and wire sizes shown are for 28V systems. For 12V systems, the breaker ratings must be increased to 10A and the size of the shielded supply and ground wires must be increased to 18 AWG. The splice wires at P5 remain at 20 AWG.

The P139-HD can be set up in one of two configurations: -- Dual Audio Board system with 4 audio connectors J1, J2, J3, J4 -- Single Audio Board with 2 audio connectors J2 and J4

Pages 1, 11 and 12 are common to all installations.Wiring diagrams for the Dual Audio Board system are found on pages 2 through 7Wiring diagrams for the Single Audio Board system are found on pages 8 through 10

Wiring Diagram for using physical switches on G13115/G13116 control panels are on page 13.

AUDIO BOARD OPTIONS:

D9M connector assembly consists of: Connector M24308/4-1F; Cinch backshell DE-24657-30; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec 165X10139X.

12

When COM2DIR (P5, Pin 11) is not grounded, the Copilot headset is inEMERGENCY mode and the following lines are diverted:HEADSET 2 connects directly to RX2, RX20 (Unswitched Alert Tones) and the emergency intercom.MIC 2 connects directly to TX 2, and the emergency Intercom.XMIT KEY 2 and CPLT COM2 KEY connect to TX KEY 2.ICS KEY 2 keys the emergency intercom, if at least one Power Input Circuit Breaker to the G13000 Audio Router has power.TX20 (CVR) transmits HEADSET2, MIC2 and Emergency Intercom if at least one Power Input Circuit Breaker to the G13000 Audio Router has power.

The COM1DIR pin MUST be wired to an appropriate switch to control Emergency Mode for the pilot headset. Emergency Mode is mandatory when the G13000 Audio Router is used as the primary audio system. See notes on sheet 13.

13

For EC135 connect alert tone ports to TB9 of factory wiring. See Eurocopter Maint.Manual WDM for detail.For EC145 connect alert tone ports to TB55028 of factory wiring. See Eurocopter Maint. Manual WDM for detail.For Bell 204, 205, 214 and 412 connect alert tone ports to 8Z1P3. See Bell Maint. Manual BHT-xx-MM for detail.

14

3

I

Drawing Redrawn.Added new Spare Keylines.Added note on shield grounding.Clarified notes and instructions.

4/10/15 SJC

THIS DOCUMENT INCLUDES INFORMATION PROPRIETARY TO EAGLE COPTERS LTD. AND SHALL NOT BE USED OR DUPLICATED BY ANYONE

WITHOUT THE WRITTEN PERMISSION OF EAGLE COPTERS LTD.

www.eaglecopters.com

PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

SHIELDING: For shielded wire, the shield must be connected toairframe ground or connector ground as follows:For wire carrying audio signals, the shield must be grounded at one end ONLY. Grounding both ends may lead to audio noise.Audio shield ground connections should be made at the G13000 connectors but may be made at the other end at the installers discretion.For all other shielded wire, e.g. Gnet and power, the shield must be grounded at both ends.

15

TX

1 K

EY

RX

11

HI

TX

11

KE

YR

X 1

1 L

O

TX

1 L

O

TX

1 H

I

RX

1 L

O

RX

1 H

I

3534 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50

18

1 2

19

3

20

4

21

5

22

6

23

7

24

8

25

9

26

10

27

11

28

12

29

13

30

14

31

15

32

16

33

17

TX

10

KE

Y

TX

10

LO

TX

10

HI

RX

10

LO

RX

10

HI

RX

7 L

O

RX

7 H

I

TX

7 H

I

TX

7 L

O

TX

7 K

EY

TX

6 L

O

RX

9 L

OR

X 6

HI

RX

9 H

I

RX

6 L

OT

X 9

HI

TX

6 H

IT

X 9

LO

TX

6 K

EY

TX

9 K

EY

TX

5 L

O

RX

8 L

OR

X 5

HI

RX

8 H

I

RX

5 L

OT

X 8

HI

TX

5 H

IT

X 8

LO

TX

5 K

EY

TX

8 K

EY

RX

3 L

O

RX

3 H

I

TX

3 H

I

TX

3 K

EY

TX

3 L

O

RX

4 L

O

RX

4 H

I

TX

4 H

I

TX

4 K

EY

TX

4 L

O

TX

11

HI

TX

11

LO

TX

18

LO

TX

12

LO

42

TX

17

HI

20

36

RX

17

HI

RX

14

HI

RX

14

LO

RX

17

LO

2

34

18

1

35

19

3

RX

2 L

O

RX

2 H

I

TX

2 H

I

RX

18

HI

TX

14

LO

TX

17

LO

TX

14

HI

TX

17

KE

YT

X 1

4 K

EY

RX

15

LO

RX

15

HI

RX

18

LO

TX

15

HI

TX

18

HI

23

39

5

37

4

21

38

22

6

TX

2 K

EY

TX

2 L

O

RX

12

HI

40

7

24

41

25

8 9

RX

12

LO

TX

12

HI

TX

16

LO

TX

13

KE

Y

15

RX

19

LO

TX

15

KE

YT

X 1

8 K

EY

TX

15

LO

RX

16

HI

RX

19

HI

RX

16

LO

TX

19

HI

TX

16

HI

TX

19

LO

RX

13

LO

12

45

27

43

10

26

44

28

11

TX

12

KE

Y

RX

13

HI

30

46

13

29

47

14

31

TX

13

HI

TX

13

LO

RX

20

HI

TX

16

KE

YT

X 1

9 K

EY

TX

20

KE

YR

X 2

0 L

O

33

4948

32

16

50

17

TX

20

HI

TX

20

LO

D50F

6

6

D50F

NOTE: VIEW IS FROM REAR OF AIRFRAME CONNECTOR

P1

P2

G13004 I

P139-HD AUDIO SYSTEMP1 P2 PLUGS DUAL-BOARD

GA182 2 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

See sheet 1 for revision history




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

XM

IT K

EY

5H

EA

DS

ET

6 H

I

42S

PA

RE

KE

Y 1

1

31

48

SP

AR

E K

EY

9G

NE

T 2

GN

D

GN

ET

2 D

AT

A L

OS

PA

RE

KE

Y 7

16

50

33

17

49

32

15

GN

ET

2 +

28V

SP

AR

E K

EY

5

GN

ET

2 D

AT

A H

I

ICS

KE

Y 7

GN

ET

1 D

AT

A L

OS

PA

RE

KE

Y 3

GN

ET

1 G

ND

XM

IT K

EY

7M

IC 7

LO

MIC

6 L

O

HE

AD

SE

T 7

LO

XM

IT K

EY

6

HE

AD

SE

T 6

LO

ICS

KE

Y 6

28

45

13

47

14

30

46

29

12

GN

ET

1 D

AT

A H

I

GN

ET

1 +

28V

MIC

7 H

I

44

11

27

43

26

10 9

HE

AD

SE

T 7

HI

MIC

6 H

I

HE

AD

SE

T 3

LO

HE

AD

SE

T 3

HI

3

ICS

KE

Y 4

HE

AD

SE

T 5

LO

ICS

KE

Y 5

MIC

5 L

O

MIC

4 L

OX

MIT

KE

Y 4

HE

AD

SE

T 4

LO

XM

IT K

EY

3M

IC 3

LO

ICS

KE

Y 3

MIC

4 H

I

6

39

24

41

8

25

40

23

7

MIC

5 H

I

HE

AD

SE

T 5

HI

21

38

5

22

37

4

20

HE

AD

SE

T 4

HI

MIC

3 H

I

ICS

KE

Y 1

MIC

1 L

OX

MIT

KE

Y 1

HE

AD

SE

T 1

LO

PLT

CO

M1

KE

Y

18

3536

19

2

34

1

MIC

1 H

I

HE

AD

SE

T 1

HI

1317 16 1415 12 11 10 9 48 7 56 3 2 1

2533 32 31 30 2729 28 26 24 23 22 21 1820 19

4650 49 48 47 4445 43 42 3741 40 39 38 3536 34

GN

ET

5 G

ND

SP

AR

E K

EY

10

HE

AD

SE

T 1

0 L

O

ICS

KE

Y 1

2

GN

ET

4 G

ND

GN

ET

5 D

AT

A L

OS

PA

RE

KE

Y 8

SP

AR

E K

EY

12

GN

ET

4 D

AT

A L

OS

PA

RE

KE

Y 4

MIC

12

LO

XM

IT K

EY

12

ICS

KE

Y 1

1

HE

AD

SE

T 1

2 L

OX

MIT

KE

Y 1

1M

IC 1

1 L

O

HE

AD

SE

T 1

1 L

O

MIC

10

LO

ICS

KE

Y 1

0

XM

IT K

EY

10

XM

IT K

EY

2

HE

AD

SE

T 9

LO

XM

IT K

EY

9M

IC 9

LO

ICS

KE

Y 9

ICS

KE

Y 8

MIC

8 L

OX

MIT

KE

Y 8

HE

AD

SE

T 8

LO

CP

LT

CO

M2

KE

Y

ICS

KE

Y 2

MIC

2 L

O

HE

AD

SE

T 2

LO

SP

AR

E K

EY

6

MIC

12

HI

GN

ET

4 +

28V

GN

ET

5 +

28V

GN

ET

5 D

AT

A H

I

GN

ET

4 D

AT

A H

I

HE

AD

SE

T 1

2 H

I

MIC

11

HI

HE

AD

SE

T 1

1 H

I

MIC

10

HI

HE

AD

SE

T 8

HI

HE

AD

SE

T 9

HI

HE

AD

SE

T 1

0 H

I

MIC

9 H

I

MIC

8 H

I

MIC

2 H

I

HE

AD

SE

T 2

HI


D50M

5

5

D50MP4

P3

P5D15F

10

11

3

10

2

9

1

12

4

13

5

14

6

15

7 8

+2

8V

IN

1

DIM

ME

R 1

GN

D

GN

D

GN

D

GN

D

DIM

ME

R 2

+2

8V

IN

2+

28V

IN 2

RE

SE

RV

ED

RE

SE

RV

ED

N/C

CO

M2D

IR

CO

M1D

IR

+2

8V IN

1

G13004 I

P139-HD AUDIO SYSTEMP3 P4 P5 PLUGS DUAL-BOARD

GA182 3 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08





PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

54321RX 1 HI

RX 1 LOTX 1 HI

TX 1 LOTX 1 KEY

6RX 3 HI

TX 3 KEYTX 3 LOTX 3 HI

RX 3 LO

10

89

7

11RX 4 HI


RX 4 LO

15

1314

12

18RX 5 HI


RX 5 LO

22

2021

19

23RX 6 HI


RX 6 LO

27

2526

24

28RX 7 HI


RX 7 LO

32

3031

29

34RX 8 HI


RX 8 LO

38

3637

35

39RX 9 HI


RX 9 LO

43

4142

40

44RX 10 HI


RX 10 LO

48

4647

45

49RX 11 HI


RX 11 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LOTX HIRX LO

TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

COM1

J1 P1

XCVR3

XCVR4

XCVR5

XCVR6

XCVR8

XCVR7

XCVR9

XCVR10

TX KEY11

D50F 6

3

G13004 I

P139-HD AUDIO SYSTEMROUTER J1 DUAL-BOARD

GA182 4 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8

8

UnswitchedAlert Audio

Pilot's


14CVR Out

Pilot's




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

54321RX 2 HI

RX 2 LOTX 2 HI

TX 2 LOTX 2 KEY

6RX 12 HI


RX 12 LO

10

89

7

11RX 13 HI


RX 13 LO

15

1314

12

18RX 14 HI


RX 14 LO

22

2021

19

23RX 15 HI


RX 15 LO

27

2526

24

28RX 16 HI


RX 16 LO

32

3031

29

34RX 17 HI


RX 17 LO

38

3637

35

39RX 18 HI


RX 18 LO

43

4142

40

44RX 19 HI


RX 19 LO

48

4647

45

49RX 20 HI


RX 20 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI


TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

COM2

J2 P2

XCVR12

XCVR13

XCVR14

XCVR15

XCVR17

XCVR16

XCVR18

XCVR19

D50F 6

3

G13004 I


GA182 5 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8

8


14

TX KEY20


Co-Pilot's

CVR OutCo-Pilot's




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

35192

181HEADSET 1 HI

HEADSET 1 LOMIC 1 HI

MIC 1 LOICS KEY 1

W

W/B

W

W/BMIC HI

HEADSET HIHEADSET LO

MIC LOICS KEY

PILOT

J3 P3

36XMIT KEY 1 XMIT KEY

W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 3

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 4

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 5

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 6

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 7

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11

HEADSET 3 HIHEADSET 3 LO

MIC 3 HIMIC 3 LO

ICS KEY 3XMIT KEY 3

XMIT KEY 4ICS KEY 4MIC 4 LOMIC 4 HI

HEADSET 4 LOHEADSET 4 HI







GNET 1 DATA HIGNET 1 DATA LO

GNET 1 +28VGNET 1 GND 31

14

3013

W/O

W/B

W

W/G


GNET 2 GNDGNET 2 +28V

15 W/G

3316

32 W/O

W

W/B

SPARE KEY 3 47

PLT COM1 KEY 34

SEE GNET BRANCH INTERCONNECT DRAWING ON SHEET 12


D50M 5

8

4

3

G13004 I


GA182 6 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8


SPARE KEY 5 17 4

SPARE KEY 7 49 4

SPARE KEY 9 50 4

SPARE KEY 11 48 4




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

35192

181HEADSET 2 HI


MIC 2 LOICS KEY 2

W

W/B

W

W/BMIC HI


MIC LOICS KEY

COPILOT

J4 P4


W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 8

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 9

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 10

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 11

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 12

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11


MIC 8 HIMIC 8 LO

ICS KEY 8XMIT KEY 8











14

3013

W/O

W/B

W

W/G



15 W/G

3316

32 W/O

W

W/B

SPARE KEY 4 47

CPLT COM2 KEY 34

3



D50M 5

8

4

G13004 I


GA182 7 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8


4

4

4

4

SPARE KEY 6 17

SPARE KEY 8 49

SPARE KEY 10 50

SPARE KEY 12 48




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

XM

IT K

EY

3H

EA

DS

ET

4 H

I

42

SP

AR

E K

EY

6

31

48

SP

AR

E K

EY

5G

NE

T 2

GN

D

GN

ET

2 D

AT

A L

OS

PA

RE

KE

Y 4

16

50

33

17

49

32

15

GN

ET

2 +

28V

SP

AR

E K

EY

3

GN

ET

2 D

AT

A H

I

ICS

KE

Y 5

GN

ET

1 D

AT

A L

OS

PA

RE

KE

Y 2

GN

ET

1 G

ND

XM

IT K

EY

5M

IC 5

LO

MIC

4 L

O

HE

AD

SE

T 5

LO

XM

IT K

EY

4

HE

AD

SE

T 4

LO

ICS

KE

Y 4

28

45

13

47

14

30

46

29

12

GN

ET

1 D

AT

A H

I

GN

ET

1 +

28V

MIC

5 H

I

44

11

27

43

26

10 9

HE

AD

SE

T 5

HI

MIC

4 H

I

HE

AD

SE

T 2

LO

HE

AD

SE

T 2

HI

3

ICS

KE

Y 2

HE

AD

SE

T 3

LO

ICS

KE

Y 3

MIC

3 L

O

MIC

2 L

OX

MIT

KE

Y 2

HE

AD

SE

T 2

LO

XM

IT K

EY

2M

IC 2

LO

ICS

KE

Y 2

MIC

2 H

I

6

39

24

41

8

25

40

23

7

MIC

3 H

I

HE

AD

SE

T 3

HI

21

38

5

22

37

4

20

HE

AD

SE

T 2

HI

MIC

2 H

I

ICS

KE

Y 1

MIC

1 L

OX

MIT

KE

Y 1

HE

AD

SE

T 1

LO

PLT

CO

M1

KE

Y

18

3536

19

2

34

1

MIC

1 H

I

HE

AD

SE

T 1

HI


D50M

5

P4

P5D15F

10

11

3

10

2

9

1

12

4

13

5

14

6

15

7 8

+2

8V

IN

1

DIM

ME

R 1

GN

D

GN

D

GN

D

GN

D

DIM

ME

R 2

+2

8V

IN

2+

28V

IN 2

RE

SE

RV

ED

RE

SE

RV

ED

N/C

N/C

CO

M1D

IR

+2

8V IN

1

G13004 I

P139-HD AUDIO SYSTEMP2 P4 P5 PLUGS SINGLE-BOARD

GA182 8 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

TX

1 K

EY

RX

10

HI

TX

10

KE

YR

X 1

0 L

O

TX

1 L

O

TX

1 H

I

RX

1 L

O

RX

1 H

I

3534 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50

18

1 2

19

3

20

4

21

5

22

6

23

7

24

8

25

9

26

10

27

11

28

12

29

13

30

14

31

15

32

16

33

17

TX

9 K

EY

TX

9 L

O

TX

9 H

I

RX

9 L

O

RX

9 H

I

RX

6 L

O

RX

6 H

I

TX

6 H

I

TX

6 L

O

TX

6 K

EY

TX

5 L

O

RX

8 L

OR

X 5

HI

RX

8 H

I

RX

5 L

OT

X 8

HI

TX

5 H

IT

X 8

LO

TX

5 K

EY

TX

8 K

EY

TX

4 L

O

RX

7 L

OR

X 4

HI

RX

7 H

I

RX

4 L

OT

X 7

HI

TX

4 H

IT

X 7

LO

TX

4 K

EY

TX

7 K

EY

RX

2 L

O

RX

2 H

I

TX

2 H

I

TX

2 K

EY

TX

2 L

O

RX

3 L

O

RX

3 H

I

TX

3 H

I

TX

3 K

EY

TX

3 L

O

TX

10

HI

TX

10

LO

D50F

6

P2





PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

54321RX 1 HI

RX 1 LOTX 1 HI

TX 1 LOTX 1 KEY

6RX 2 HI


RX 2 LO

10

89

7

11RX 3 HI


RX 3 LO

15

1314

12

18RX 4 HI


RX 4 LO

22

2021

19

23RX 5 HI


RX 5 LO

27

2526

24

28RX 6 HI


RX 6 LO

32

3031

29

34RX 7 HI


RX 7 LO

38

3637

35

39RX 8 HI


RX 8 LO

43

4142

40

44RX 9 HI


RX 9 LO

48

4647

45

49RX 10 HI


RX 10 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI


TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

COM1

J2 P2

COM2

XCVR3

XCVR4

XCVR5

XCVR7

XCVR6

XCVR8

XCVR9

D50F 6

3

G13004 I

P139-HD AUDIO SYSTEMROUTER J2 SINGLE-BOARD

GA182 9 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8

8


14

TX KEY10


Pilot's

CVR OutPilot's




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

35192

181HEADSET 1 HI


MIC 1 LOICS KEY 1

W

W/B

W

W/BMIC HI


MIC LOICS KEY

PILOT

J4 P4


W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 1

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 2

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 3

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 4

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 5

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11


MIC 2 HIMIC 2 LO

ICS KEY 2XMIT KEY 2











14

3013

W/O

W/B

W

W/G



15 W/G

3316

32 W/O

W

W/B

SPARE KEY 2 47

PLT COM1 KEY 34



D50M 5

8

4

3

G13004 I

P139-HD AUDIO SYSTEMROUTER J4 SINGLE-BOARD

GA182 10 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

8


SPARE KEY 3 17 4

SPARE KEY 4 49 4

SPARE KEY 5 50 4

SPARE KEY 6 48 4




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

15

34

56

2

7

10

11

1314

19

8

P5 D15F 10

RESERVEDRESERVED

COM2DIR

COM1DIR

GND

DIMMER 2

DIMMER 1

GND

GNDGND

SUPPLY +V IN 2SUPPLY +V IN 2

SUPPLY +V IN 1SUPPLY +V IN 1 +28V AVIONICS POWER 1

AUDIOROUTER 1

5A

+28V AVIONICS POWER 2

AUDIOROUTER 2

5A

TO DIMMER BUS 2

TO DIMMER BUS 1

CONNECT THESE TWO GROUND WIRES TO SEPARATE SCREWS

20 AWG

20 AWG

20 AWG

20 AWG

G13004 I

P139-HD AUDIO SYSTEMROUTER J5 CONNECTIONS

GA182 11of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

J5

1111

11

11

11

11

TO PILOT CONTROL PANELSEE SHEET 13

TO COPILOT CONTROL PANELSEE SHEET 13

NOT USED ON SINGLE-BOARD SYSTEMS.

13

8

8




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

W/G

W/O

W

W/B

DATA LO2 DATA HI

GND+28V4

3

1

CONTROL

To Gnet connections on G13000 J3 and J4 (typical for each Gnet bus)

6

87

5

9

PANEL

2

45

3

7

98

6

1 DATA LO

+28VGNDDATA HI

PANELCONTROL

2

45

3

7

98

6

1

ADDR 1

ADDR 3ADDR LO

ADDR 2

DATA LOW

+28VGND

ADDR 0

DATA HI

PANELCONTROL

Additional control panels or other Gnet interface devices as required, up to 15 total per Gnet bus.

AEJN

BFKP

DHMS

CGLR

W T

Y Z

G

RY

L

CH

SZ

M

D

F

PW

K

BE

NT

J

A

W/O

W

W/B

W/G

W/B

W

W/G

W/O

To additional control panel or additional terminal blocks if

required

To additional Control panel if required

W/O

W/B

W

W/G

W/G

W

W/B

W/O

W/G

W/O

W/B

W

W/O

W/B

W

W/G

"5" = 6-8-9"6" = 5-8-9"7" = 8-9"8" = 5-6-7-9

"9" = 6-7-9"A" = 5-7-9"B" = 7-9"C" = 5-6-9

For every control panel or other peripheral device connected to a particular Gnet bus, a unique device address from "1" to "9" or "A" to "F" must be wired into the connector. The address for each device on each Gnet bus is defined in the system configuration software for the specific installation.

Using 24 AWG wire 1.5" long for each jumper, connect the following pins together for Gnet addressing for each connector, as specified in the system configuration requirements. Make no connections to unlisted pins.

The first control panel on any given Gnet bus should be set as address "F" with no jumpers. Additional panels on the same bus should be given addresses in descending order: "E", "D", "C" etc.

ADDRESSSET TO 'F'

(SEE BELOW)

ADDRESSJUMPERS

(SEE BELOW)

ADDRESSJUMPERS

(SEE BELOW)

"1" = 6-7-8-9"2" = 5-7-8-9"3" = 7-8-9"4" = 5-6-8-9

"D" = 6-9"E" = 5-9"F" = NONE

GNET ADDRESS JUMPERS:

3

3

3

D9F 7

D9F 7

D9F 7

9

9

GNET DATA HIGNET DATA LO

GNET +28VGNET GND

G13004 I

P139-HD AUDIO SYSTEMGNET INTERCONNECTS

GA182 12 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

ADDR 0

ADDR 2

ADDR LOADDR 3

ADDR 1

ADDR 0

ADDR 2

ADDR LOADDR 3

ADDR 1


+28V AVIONICS POWER

AUDIOPANEL

5A

AIRFRAME GROUND

TO GNET CONNECTIONS ON J3 AND J4 (TYPICAL FOR EACH GNET CHANNEL)

BF

KP

WGNET DATA HI

GNET DATA LOW

W/B

If the audio system has more than 6 control panels an external power source for the additional panels must be provided. Up to 12 additional control panels may be powered from each external 5A breaker.

GNET EXTERNAL POWER:

A

E

J

N

T

B

F

K

P

W

C

G

L

R

Y

D

H

M

S

Z

Terminal blockinternal

connections9




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

If the number of installed control panels is equal to or less than the number of available Gnet busses (4 for dual-board, 2 for single-board) then each panel should be connected to a separate Gnet bus and terminal blocks are not required.

The pilot's primary control panel should be the first device on Gnet bus 1. The copilot's primary control panel should be the first device on Gnet 3 in a dual-board system and the first device on Gnet 2 on a single-board system.

Additional control panels should be evenly distributed among available Gnet busses.

CONTROL PANEL BUS ASSIGNMENT:

9

15

TERMINAL BLOCK

10

J3 D9M10

COM1DIR

G13004 I

P139-HD AUDIO SYSTEMG13115 PANEL WIRING

GA182 13 of 13

RBH 10/30/08

JSW 10/30/08

CLB 10/30/08

J5


35

36

P3 D50M 5J3

3GND

6 COM ISO

P3

7 GND

8

TX PTT9

ICS PTT

ICS KEY 1

XMIT KEY 1

P5 D15F

TO CYCLIC PTT SWITCHES

Pilot Control PanelG13000 Digital Audio System

G13115 or G13116

12Copilot Pin Assignment

NAME G13115/6 G13000

COM2DIR J3 pin 6 J5 pin 11

GND J3 Pin 7 J5 pin 5

ICS KEY2 J3 pin 8 J4 pin 35

XMIT KEY 2 J3 Pin 9 J4 pin 36

The G13115 and G13116 control panels have two electromechanical toggle switches on the front panel; an EMERG/NORMAL locking toggle switch, and a 3-position momentary switch for ICS/OFF/TX PTT. When each switch is "on" the appropriate pin on the J3 connector is connected to GND, pin 7.

The above wiring diagram illustrates the use of the EMERG/NORMAL switch on the pilot's G13115 or G13116 primary control panel to control the Emergency Mode operation for the pilot headset. The operation of the Digital Audio System in Emergency Mode is detailed in NOTE 8 on G13004 sheet 1.

The pilot's primary control panel MUST be wired to COM1DIR as shown if this is the primary audio system installed. ONLY if the audio system is installed as a secondary may the connection be omitted and the COM1DIR pin on the G13000 be directly connected to ground.

In most installations, the copilot's primary control panel will be wired to COM2DIR, connecting to the appropriate pins as shown in the above table. Exceptions are if the audio system is not the primary audio system or if the HEADSET 2 port is not at a location used by flight crew. In these situations the COM2DIR pin on the G13000 should be directly connected to ground.

On a single-board system there is no copilot Emergency Mode, and the COM2DIR pin is not connected.

The EMERG/NORMAL switch is only connected for the pilot's and copilot's primary control panel. For other control panel locations, a G13115NS or G13116NS panel with the EMERG/NORMAL switch not installed may be used.

The ICS PTT and TX PTT pins on the copilot control panel should be connected in parallel with the appropriate PTT switches on the copilot cyclic and/or foot switches.

In all other crew positions the ICS PTT and TX PTT pins on the associated control panel may be connected in parallel with the appropriate PTT switches for that headset.

AND/OR FOOT SWITCHES




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

HAT SECTION INSTALLATION DETAIL

BACK PLATE INSTALLATION DETAIL

G13005-1G13005-1

4

G13000 ROUTER

5

FS168 BULKHEAD

4

5

2

CLB

DATE

.XXX

ANYONE WITHOUT THE WRITTEN PERMISSION OF EAGLE COPTERS LTD.

DATE

CHECKED

Design

Drawing Number

Pro No:

REV

D

A

TO EAGLE COPTERS LTD. AND SHALL NOT BE USED OR DUPLICATED BY

DIMENSIONS ARE IN INCHES

Title

SIZE

UNLESS OTHERWISE SPECIFIED

THIS DOCUMENT INCLUDES INFORMATION PROPRIETARY

4

TOLERANCES ARE:DATE

D

DATE

Scale:

C

D

FRACTIONS

.010

1/8".030

BREAK SHARP EDGES


DRAWN

Approval

A

B

C

123

1234

A

B

DECIMAL.X .050.XX

ANGLES

10/07/09REVISED FN5

COMPLETED INSTALLATION

3G13000P139-HD ROUTER

3

G13005-2BACKPLATE

3

3

GA182

A

1:1

G13005

P139-HD AS350 INSTALLATION10/30/08CLB

10/30/08CLB

4

FULLY DOWN.SECTIONS INTO SLOTS. BE SURE IT IS SEATED HANG ROUTER/BACKPLATE ASSEMBLY ON HAT

INSTALL #10-32 x .50 SCREW , AN525-10R8

Sheet 1 of 1

1

3

G13005-2 BACK PLATE.

MAINTAIN 2 E/D EDGE MARGIN FOR ALL MOUNTING HOLES.

1

DOES NOT INTERFERE WITH OTHER INSTALLED EQUIPMENT.

TAKE CARE WHEN DRILLING MOUNTING HOLES TO NOT

TOP OF STIFFENING RIBS AS SHOWN. BACKDRILL TWO MOUNTING HOLES IN BULKHEAD AND CLECO IN PLACE. REMOVE BACK PLATE.

DRILL INTO THE FUEL CELL BEHIND THE BULKHEAD.

INSTALLATION INSTRUCTIONS

G13005-2 BACK PLATE TO MAINTAIN PROPER SPACING. LOCATE G13005-1 HAT SECTIONS OVER

FOR EACH HAT SECTION, BACKDRILL BULKHEAD AND

BEFORE INSTALLING HAT SECTIONS, ASSEMBLE WITH

INSTALL (14) #4 RIVETS, MS20470AD4-4 OR USE PULL RIVETS MS20600AD4-2 (CR9163-4-2).

2

REMOVE #10-32 X .5 FLAT HEAD SCREWS (MS24693S272) FROM BACK OF ROUTER AND USE THEM TO MOUNT

THIS INSTALLATION PROVIDES MOUNTING PROVISIONS FOR THE G13000 P139-HD ROUTER IN THE AFT BAGGAGE COMPARTMENT FOR AS350/355 HELICOPTERS.

LOCATION SHOWN IS FOR REFERENCE ONLY, EXACT PLACEMENT IS DEPENDANT ON OTHER PRE-EXISTING INSTALLED EQUIPMENT. IT IS THE INSTALLERS RESPONSIBILITY TO MAKE SURE THIS INSTALLATION

5

WEIGHT OF INSTALLED COMPONENTS INCLUDING ROUTER BOX = 4.9 LBS @ FS 170.6

AFT BAGGAGE COMPARTMENT

FS168BULKHEAD

BL 0.0A/C

G13005-1

FS168 BULKHEAD CL

HAT SECTION

1

FWD

G13005-1HAT SECTION

2

1

DECK

2.55.5

2.960

5.740

1

3.355 2.995

4.950

J2J3 J1

B

NONEGA182

G13115

CONTROL PANEL6/01/12CLB

6/01/12CLB

Sheet 1 of 1

NOTES:

BUTTON LABELS SHOWN ARE FOR REFERENCE ONLY AND ARE INSTALLER DEFINED

POWER: 28 VDC @ 250mA MAX

WEIGHT: 1.50 LBS MAX

OPTIONAL: TEXT MAY BE ENGRAVED, STAMPED ORPRINTED ON PART AS DESIRED

1

P/N G13115 : AS SHOWN

P/N G13115NS : REPLACE SWITCH WITH HEYCO HOLE PLUG #2603

Title



DATE

CHECKED

Design

Drawing Number

Pro No:

REV

DSIZE


TOLERANCES ARE:

FRACTIONS1/8"


ANGLES2

BREAK SHARP EDGES


DRAWN

Approval

A

B

C

123

1234

A

B

C

D

4

D

Scale:

DATE

DATE

DATE

A ADDED P/N G13115NS 10/15/12CLB

3/26/14CLB

REVISED NOTESB

5.740

2.230

1

4.950

2.995 3.355

J1 J2J3

B

NONEGA182

G13116

CONTROL PANEL6/01/12CLB

6/01/12CLB

Sheet 1 of 1

NOTES:

BUTTON LABELS SHOWN ARE FOR REFERENCE ONLY AND ARE INSTALLER DEFINED

POWER: 28VDC @ 250mA MAX

WEIGHT: 1.25 LBS MAX


1

P/N G13116 : AS SHOWN

P/N G13116NS : REPLACE SWITCH WITH HEYCO HOLE PLUG #2603Title



DATE

CHECKED

Design

Drawing Number

Pro No:

REV

DSIZE


TOLERANCES ARE:

FRACTIONS1/8"


ANGLES2

BREAK SHARP EDGES


DRAWN

Approval

A

B

C

123

1234

A

B

C

D

4

D

Scale:

DATE

DATE

DATE

10/15/12CLB

ADDED P/N G13116NSA

3/26/14CLB

REVISED NOTESB

10.00

8.50

3.56

J1 J5

J7

J4J6

J8 NETWORK PORT

J9 MEMORY CARD SLOT

OPTIONAL (2) PLACES:SUPPORT HOOK (NAS622CE2)


J2

J3

OPTIONAL: CLIP G13161-4


A1:1GA182

G13160

P139-HD3 BOARD ROUTER

12/9/13CLB

Sheet 1 of 1

CLB 12/9/13

G13160 P139-HD3 BOARD ROUTERWEIGHT = 5.3 LBS MAXPOWER = 5 AMPS MAXVOLTAGE = 14 - 32 VDC


Title



DATE

CHECKED

Design

Drawing Number

Pro No:

REV

DSIZE


TOLERANCES ARE:

FRACTIONS1/8"


ANGLES2

BREAK SHARP EDGES


DRAWN

Approval

A

B

C

123

1234

A

B

C

D

4

D

Scale:

DATE

DATE

DATE

A VOLTAGE RANGE WAS 10 - 30 VDC 08/13/14CLB

NOTES:Unless otherwise noted: All wires are 22 awg; all shielded wire is MIL-DTL-27500; all unshielded wire is MIL-W-22759/16.

All Grounding and Bonding will be I/A/W AC 43.13-1B, Chapter 11, Section 15.

Ground the shield return to the metal connector backshell if used, or otherwise to the metal connector housing.

SPARE KEY line function and connections are installer defined and depend on the specific system configuration.

D50M connector assembly consists of: Connector M24308/4-5F; Cinch backshell dd-24661-34; 2ea. Cinch Screwlocks D20420-42. Alternate Backshell: Conec 165X10179X.

D50F connector assembly consists of: Connector M24308/2-5F; Cinch backshell dd-24661-34; 2ea. Cinch Screwlocks D20420-42. Alternate Backshell: Conec 165X10179X.

D9F connector assembly consists of: Connector M24308/2-1F; Cinch backshell DE-24657-30; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec 165X10139X.

2.

1.

When COM1DIR (P7, Pin 10) is not grounded, the Pilot headset is inEMERGENCY mode and the following lines are diverted:HEADSET 1 connects directly to RX 1, RX 11 (Unswitched Alert Tones) and the emergency intercom. MIC 1 connects directly to TX 1 and the emergency Intercom.XMIT KEY 1 and PLT COM1 KEY connect to TX KEY 1. ICS KEY 1 keys the emergency intercom, if at least one Power Input Circuit Breaker to the G13160 Audio Router has power. TX 11 (CVR) transmits HEADSET 1, MIC 1 and Emergency Intercom if at least one Power Input Circuit Breaker to the G13160 Audio Router has power.

MAKE NO CONNECTION. The pin is not connected to anything internally and therefore shall have no connection externally

DEFINITIONS:N/C:

RESERVED: MAKE NO CONNECTION. Internal circuitry may be added in the future, or may be present and relevant for testing but not relevant to operation for flight.

4

5

6

7

8

9 TERMINAL BLOCK assembly consists of: Deutsch block CTJ122E05E; Deutsch socket contacts CTS-S22/22 or M39029/22-191. A Gnet bus that is connected to only one control panel or other device may be wired directly without using a terminal block.

10 D15F connector preferred assembly consists of: Connector M24308/2-2F; Cinch backshell DA-24658-31; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec P/N: 165X10149X. Splices on 20 AWG wire shall also be 20 AWG, length 3 inches maximum. Alternate assembly consists of: Kobiconn Solder-Cup Connector 156-1315T-E and Cinch backshell DA-24658-31; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec P/N: 165X10149X. Conductors shown with splices may be implemented by soldering the supply wire to both pins after soldering and insulating the adjacent connections.

G13162 A

P139-HD AUDIO SYSTEMWIRING DIAGRAMS - NOTES

GA182 1 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

11 The Audio System works with a range of supply voltages, as specified in the installation instructions. Breaker ratings and wire sizes shown are for 28V systems. For 12V systems, the breaker ratings must be increased to 10A and the size of the shielded supply and ground wires must be increased to 18 AWG. The splice wires at P7 remain at 20 AWG.

D9M connector assembly consists of: Connector M24308/4-1F; Cinch backshell DE-24657-30; 2ea. Cinch Screwlocks D20419-46. Alternate Backshell: Conec 165X10139X.

12

When COM2DIR (P7, Pin 11) is not grounded, the Copilot headset and Headset 13 are in EMERGENCY mode and the following lines are diverted:HEADSET 2 connects directly to RX 2, RX 20 (Unswitched Alert Tones) and the emergency intercom.MIC 2 connects directly to TX 2 and the emergency Intercom.XMIT KEY 2 and CPLT COM2 KEY connect to TX KEY 2.ICS KEY 2 keys the emergency intercom, if at least one Power Input Circuit Breaker to the G13160 Audio Router has power.TX 20 (CVR) transmits HEADSET 2, MIC 2 and Emergency Intercom if at least one Power Input Circuit Breaker to the G13160 Audio Router has power.

The COM1DIR pin MUST be wired to an appropriate switch to control Emergency Mode for the pilot headset. Emergency Mode is mandatory when the G13160 Audio Router is used as the primary audio system. See notes on sheet 13.

13

For EC135 connect alert tone ports to TB9 of factory wiring. See Eurocopter Maint.Manual WDM for detail.For EC145 connect alert tone ports to TB55028 of factory wiring. See Eurocopter Maint. Manual WDM for detail.For Bell 204, 205, 214 and 412 connect alert tone ports to 8Z1P3. See Bell Maint. Manual BHT-xx-MM for detail.

14

3

AAdded new Spare Keylines.Added note on shield grounding.Clarified notes and instructions.

4/10/15 SJC




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

SHIELDING: For shielded wire, the shield must be connected toairframe ground or connector ground as follows:For wire carrying audio signals, the shield must be grounded at one end ONLY. Grounding both ends may lead to audio noise.Audio shield ground connections should be made at the G13160 connectors but may be made at the other end at the installers discretion.For all other shielded wire, e.g. Gnet and power, the shield must be grounded at both ends.

15

HEADSET 13 connects directly to RX21, RX30 and theemergency intercom.

MIC 13 connects directly to TX21 and the emergency Intercom.XMIT KEY 13 and HS13 TX21 KEY connect to TX KEY 21.ICS KEY 13 keys the emergency intercom, if at least one Power Input Circuit Breaker to the G13160 Audio Router has power.TX30 transmits HEADSET 13, MIC 13 and Emergency Intercom if at least one Power Input Circuit Breaker to the G13160 Audio Router has power.

TX

1 K

EY

RX

11

HI

TX

11

KE

YR

X 1

1 L

O

TX

1 L

O

TX

1 H

I

RX

1 L

O

RX

1 H

I

3534 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50

18

1 2

19

3

20

4

21

5

22

6

23

7

24

8

25

9

26

10

27

11

28

12

29

13

30

14

31

15

32

16

33

17

TX

10

KE

Y

TX

10

LO

TX

10

HI

RX

10

LO

RX

10

HI

RX

7 L

O

RX

7 H

I

TX

7 H

I

TX

7 L

O

TX

7 K

EY

TX

6 L

O

RX

9 L

OR

X 6

HI

RX

9 H

I

RX

6 L

OT

X 9

HI

TX

6 H

IT

X 9

LO

TX

6 K

EY

TX

9 K

EY

TX

5 L

O

RX

8 L

OR

X 5

HI

RX

8 H

I

RX

5 L

OT

X 8

HI

TX

5 H

IT

X 8

LO

TX

5 K

EY

TX

8 K

EY

RX

3 L

O

RX

3 H

I

TX

3 H

I

TX

3 K

EY

TX

3 L

O

RX

4 L

O

RX

4 H

I

TX

4 H

I

TX

4 K

EY

TX

4 L

O

TX

11

HI

TX

11

LO

D50F

6


P1

G13162 A

P139-HD AUDIO SYSTEMP1 P2 PLUGS

GA182 2 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14


XM

IT K

EY

5H

EA

DS

ET

6 H

I

42

SP

AR

E K

EY

5

31

48

SP

AR

E K

EY

4G

NE

T 2

GN

D

GN

ET

2 D

AT

A L

OS

PA

RE

KE

Y 3

16

50

33

17

49

32

15

GN

ET

2 +

28

V

SP

AR

E K

EY

2

GN

ET

2 D

AT

A H

I

ICS

KE

Y 7

GN

ET

1 D

AT

A L

OS

PA

RE

KE

Y 1

GN

ET

1 G

ND

XM

IT K

EY

7M

IC 7

LO

MIC

6 L

O

HE

AD

SE

T 7

LO

XM

IT K

EY

6

HE

AD

SE

T 6

LO

ICS

KE

Y 6

28

45

13

47

14

30

46

29

12

GN

ET

1 D

AT

A H

I

GN

ET

1 +

28

V

MIC

7 H

I

44

11

27

43

26

10 9

HE

AD

SE

T 7

HI

MIC

6 H

I

HE

AD

SE

T 3

LO

HE

AD

SE

T 3

HI

3

ICS

KE

Y 4

HE

AD

SE

T 5

LO

ICS

KE

Y 5

MIC

5 L

O

MIC

4 L

OX

MIT

KE

Y 4

HE

AD

SE

T 4

LO

XM

IT K

EY

3M

IC 3

LO

ICS

KE

Y 3

MIC

4 H

I

6

39

24

41

8

25

40

23

7

MIC

5 H

I

HE

AD

SE

T 5

HI

21

38

5

22

37

4

20

HE

AD

SE

T 4

HI

MIC

3 H

I

ICS

KE

Y 1

MIC

1 L

OX

MIT

KE

Y 1

HE

AD

SE

T 1

LO

PL

T C

OM

1 K

EY

18

3536

19

2

34

1

MIC

1 H

I

HE

AD

SE

T 1

HI

D50M

5

P2




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

1317 16 1415 12 11 10 9 48 7 56 3 2 1

2533 32 31 30 2729 28 26 24 23 22 21 1820 19

4650 49 48 47 4445 43 42 3741 40 39 38 3536 34

GN

ET

4 G

ND

SP

AR

E K

EY

9

HE

AD

SE

T 1

0 L

O

ICS

KE

Y 1

2

GN

ET

3 G

ND

GN

ET

4 D

AT

A L

OS

PA

RE

KE

Y 8

SP

AR

E K

EY

10

GN

ET

3 D

AT

A L

OS

PA

RE

KE

Y 6

MIC

12

LO

XM

IT K

EY

12

ICS

KE

Y 1

1

HE

AD

SE

T 1

2 L

OX

MIT

KE

Y 1

1M

IC 1

1 L

O

HE

AD

SE

T 1

1 L

O

MIC

10

LO

ICS

KE

Y 1

0

XM

IT K

EY

10

XM

IT K

EY

2

HE

AD

SE

T 9

LO

XM

IT K

EY

9M

IC 9

LO

ICS

KE

Y 9

ICS

KE

Y 8

MIC

8 L

OX

MIT

KE

Y 8

HE

AD

SE

T 8

LO

CP

LT C

OM

2 K

EY

ICS

KE

Y 2

MIC

2 L

O

HE

AD

SE

T 2

LO

SP

AR

E K

EY

7

MIC

12

HI

GN

ET

3 +

28

V

GN

ET

4 +

28

V

GN

ET

4 D

AT

A H

I

GN

ET

3 D

AT

A H

I

HE

AD

SE

T 1

2 H

I

MIC

11

HI

HE

AD

SE

T 1

1 H

I

MIC

10

HI

HE

AD

SE

T 8

HI

HE

AD

SE

T 9

HI

HE

AD

SE

T 1

0 H

I

MIC

9 H

I

MIC

8 H

I

MIC

2 H

I

HE

AD

SE

T 2

HI


5

D50MP4

G13162 A

P139-HD AUDIO SYSTEMP3 P4 PLUGS

GA182 3 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14


TX

18

LO

TX

12

LO

42

TX

17

HI

20

36

RX

17

HI

RX

14

HI

RX

14

LO

RX

17

LO

2

34

18

1

35

19

3

RX

2 L

O

RX

2 H

I

TX

2 H

I

RX

18

HI

TX

14

LO

TX

17

LO

TX

14

HI

TX

17

KE

YT

X 1

4 K

EY

RX

15

LO

RX

15

HI

RX

18

LO

TX

15

HI

TX

18

HI

23

39

5

37

4

21

38

22

6

TX

2 K

EY

TX

2 L

O

RX

12

HI

40

7

24

41

25

8 9

RX

12

LO

TX

12

HI

TX

16

LO

TX

13

KE

Y

15

RX

19

LO

TX

15

KE

YT

X 1

8 K

EY

TX

15

LO

RX

16

HI

RX

19

HI

RX

16

LO

TX

19

HI

TX

16

HI

TX

19

LO

RX

13

LO

12

45

27

43

10

26

44

28

11

TX

12

KE

Y

RX

13

HI

30

46

13

29

47

14

31

TX

13

HI

TX

13

LO

RX

20

HI

TX

16

KE

YT

X 1

9 K

EY

TX

20

KE

YR

X 2

0 L

O

33

4948

32

16

50

17

TX

20

HI

TX

20

LO

6

D50FP3




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL


G13162 A

P139-HD AUDIO SYSTEMP5 P6 P7 PLUGS

GA182 4 of 13

GA 3/27/14

SCJ 3/27/14

CLB 3/27/14


TX

28

LO

TX

22

LO

42

TX

27

HI

20

36

RX

27

HI

RX

24

HI

RX

24

LO

RX

27

LO

2

34

18

1

35

19

3

RX

21

LO

RX

21

HI

TX

21

HI

RX

28

HI

TX

24

LO

TX

27

LO

TX

24

HI

TX

27

KE

YT

X 2

4 K

EY

RX

25

LO

RX

25

HI

RX

28

LO

TX

25

HI

TX

28

HI

23

39

5

37

4

21

38

22

6

TX

21

KE

Y

TX

21

LO

RX

22

HI

40

7

24

41

25

8 9

RX

22

LO

TX

22

HI

TX

26

LO

TX

23

KE

Y

15

RX

29

LO

TX

25

KE

YT

X 2

8 K

EY

TX

25

LO

RX

26

HI

RX

29

HI

RX

26

LO

TX

29

HI

TX

26

HI

TX

29

LO

RX

23

LO

12

45

27

43

10

26

44

28

11

TX

22

KE

Y

RX

23

HI

30

46

13

29

47

14

31

TX

23

HI

TX

23

LO

RX

30

HI

TX

26

KE

YT

X 2

9 K

EY

TX

30

KE

YR

X 3

0 L

O

33

4948

32

16

50

17

TX

30

HI

TX

30

LO

6

D50FP5

1317 16 1415 12 11 10 9 48 7 56 3 2 1

2533 32 31 30 2729 28 26 24 23 22 21 1820 19

4650 49 48 47 4445 43 42 3741 40 39 38 3536 34

GN

ET

6 G

ND

SP

AR

E K

EY

14

HE

AD

SE

T 1

6 L

O

ICS

KE

Y 1

8

GN

ET

5 G

ND

GN

ET

6 D

AT

A L

OS

PA

RE

KE

Y 1

3

SP

AR

E K

EY

15

GN

ET

5 D

AT

A L

OS

PA

RE

KE

Y 1

1

MIC

18

LO

XM

IT K

EY

18

ICS

KE

Y 1

7

HE

AD

SE

T 1

8 L

OX

MIT

KE

Y 1

7M

IC 1

7 L

O

HE

AD

SE

T 1

7 L

O

MIC

16

LO

ICS

KE

Y 1

6

XM

IT K

EY

16

XM

IT K

EY

2

HE

AD

SE

T 1

5 L

O

XM

IT K

EY

15

MIC

15

LO

ICS

KE

Y 1

5

ICS

KE

Y 1

4M

IC 1

4 L

OX

MIT

KE

Y 1

4

HE

AD

SE

T 1

4 L

O

HS

13 T

X21

KE

Y

ICS

KE

Y 2

MIC

13

LO

HE

AD

SE

T 1

3 L

O

SP

AR

E K

EY

12

MIC

18

HI

GN

ET

5 +

28V

GN

ET

6 +

28V

GN

ET

6 D

AT

A H

I

GN

ET

5 D

AT

A H

I

HE

AD

SE

T 1

8 H

I

MIC

17

HI

HE

AD

SE

T 1

7 H

I

MIC

16

HI

HE

AD

SE

T 1

4 H

I

HE

AD

SE

T 1

5 H

I

HE

AD

SE

T 1

6 H

I

MIC

15

HI

MIC

14

HI

MIC

13

HI

HE

AD

SE

T 1

3 H

I

5

D50MP6

P7D15FS

10

11

3

10

2

9

1

12

4

13

5

14

6

15

7 8

+2

8V

IN

1

DIM

ME

R 1

GN

D

GN

D

GN

D

GN

D

DIM

ME

R 2

+2

8V

IN

2+

28V

IN 2

RE

SE

RV

ED

RE

SE

RV

ED

N/C

CO

M2D

IR

CO

M1D

IR

+2

8V IN

1




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

54321RX 1 HI

RX 1 LOTX 1 HI

TX 1 LOTX 1 KEY

6RX 3 HI


RX 3 LO

10

89

7

11RX 4 HI


RX 4 LO

15

1314

12

18RX 5 HI


RX 5 LO

22

2021

19

23RX 6 HI


RX 6 LO

27

2526

24

28RX 7 HI


RX 7 LO

32

3031

29

34RX 8 HI


RX 8 LO

38

3637

35

39RX 9 HI


RX 9 LO

43

4142

40

44RX 10 HI


RX 10 LO

48

4647

45

49RX 11 HI


RX 11 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI


TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

COM1

J1 P1

XCVR3

XCVR4

XCVR5

XCVR6

XCVR8

XCVR7

XCVR9

XCVR10

TX KEY11

D50F 6

3

G13162 A

P139-HD AUDIO SYSTEMROUTER J1

GA182 5 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8

8


Pilot's


14CVR Out

Pilot's




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

54321RX 2 HI

RX 2 LOTX 2 HI

TX 2 LOTX 2 KEY

6RX 12 HI


RX 12 LO

10

89

7

11RX 13 HI


RX 13 LO

15

1314

12

18RX 14 HI


RX 14 LO

22

2021

19

23RX 15 HI


RX 15 LO

27

2526

24

28RX 16 HI


RX 16 LO

32

3031

29

34RX 17 HI


RX 17 LO

38

3637

35

39RX 18 HI


RX 18 LO

43

4142

40

44RX 19 HI


RX 19 LO

48

4647

45

49RX 20 HI


RX 20 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI


TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

COM2

J3 P3

XCVR12

XCVR13

XCVR14

XCVR15

XCVR17

XCVR16

XCVR18

XCVR19

D50F 6

3

G13162 A


GA182 6 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8

8


14

TX KEY20


Co-Pilot's

CVR OutCo-Pilot's




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

54321RX 21 HI

RX 21 LOTX 21 HI

TX 21 LOTX 21 KEY

6RX 22 HI


RX 22 LO

10

89

7

11RX 23 HI


RX 23 LO

15

1314

12

18RX 24 HI


RX 24 LO

22

2021

19

23RX 25 HI


RX 25 LO

27

2526

24

28RX 26 HI


RX 26 LO

32

3031

29

34RX 27 HI


RX 27 LO

38

3637

35

39RX 28 HI


RX 28 LO

43

4142

40

44RX 29 HI


RX 29 LO

48

4647

45

49RX 30 HI


RX 30 LO

33

1617

50

W

W/B

W

W/B

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

W/B

W/B

W

W

TX HI

TX HI

TX HI

TX HI

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI


TX HI

TX HI

TX HI

TX HI

TX HI

RX HIRX LO

TX LOTX KEY

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

RX HI

TX KEYTX LO

RX LO

XCVR21

J5 P5

XCVR22

XCVR23

XCVR24

XCVR25

XCVR27

XCVR26

XCVR28

XCVR29

D50F 6

3

G13162 A


GA182 7 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8

8


14

TX KEY30


Headset 13

CVR OutHeadset 13




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

35192

181HEADSET 1 HI


MIC 1 LOICS KEY 1

W

W/B

W

W/BMIC HI


MIC LOICS KEY

PILOT

J2 P2


W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 3

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 4

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 5

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 6

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 7

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11


MIC 3 HIMIC 3 LO

ICS KEY 3XMIT KEY 3











14

3013

W/O

W/B

W

W/G



15 W/G

3316

32 W/O

W

W/B

SPARE KEY 1 47

PLT COM1 KEY 34



D50M 5

8

4

3

G13162 A


GA182 8 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8





PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

SPARE KEY 2 17 4

SPARE KEY 3 49 4

SPARE KEY 4 50 4

SPARE KEY 5 48 4

15

35192

181HEADSET 2 HI


MIC 2 LOICS KEY 2

W

W/B

W

W/BMIC HI


MIC LOICS KEY

COPILOT

J4 P4


W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 8

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 9

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 10

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 11

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 12

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11


MIC 8 HIMIC 8 LO

ICS KEY 8XMIT KEY 8











14

3013

W/O

W/B

W

W/G



15 W/G

3316

32 W/O

W

W/B

SPARE KEY 6 47

CPLT COM2 KEY 34

3



D50M 5

8

4

G13162 A


GA182 9 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8





PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

SPARE KEY 7 17 4

SPARE KEY 8 49 4

SPARE KEY 9 50 4

SPARE KEY 10 48 4

15

35192

181HEADSET 13 HI


MIC 13 LOICS KEY 13

W

W/B

W

W/BMIC HI


MIC LOICS KEY

H/S 13

J6 P6


W/B

W

W/B

W

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 14

W/B

W

W/B

W

HEADSET LO

XMIT KEY

MIC HI

ICS KEYMIC LO

HEADSET HI

H/S 15

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 16

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 17

W

W/B

W

W/B

XMIT KEY

HEADSET LO

MIC LOICS KEY

MIC HI

HEADSET HI

H/S 18

4

38

2137

320

22

3923

40

6

5

24

4125

42

8

7

26

4327

44

10

9

28

4529

46

12

11


MIC 14 HIMIC 14 LO

ICS KEY 14XMIT KEY 14











14

3013

W/O

W/B

W

W/G



15 W/G

3316

32 W/O

W

W/B

SPARE KEY 11 47

HS13 TX21 KEY 34

3



D50M 5

8

4

G13162 A


GA182 10 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

8





PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

SPARE KEY 12 17 4

SPARE KEY 13 49 4

SPARE KEY 14 50 4

SPARE KEY 15 48 4

15

15

34

56

2

7

10

11

1314

19

8

P7 D15F 10

RESERVEDRESERVED

COM2DIR

COM1DIR

GND

DIMMER 2

DIMMER 1

GND

GNDGND

+28V IN 2+28V IN 2

+28V IN 1+28V IN 1 +28V AVIONICS POWER 1

AUDIOROUTER 1

5A

+28V AVIONICS POWER 2

AUDIOROUTER 2

5A

TO DIMMER BUS 2

TO DIMMER BUS 1

CONNECT THESE TWO GROUND WIRES TO SEPARATE SCREWS

20 AWG

20 AWG

20 AWG

20 AWG

G13162 A

P139-HD AUDIO SYSTEMROUTER J7 CONNECTIONS

GA182 11of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

J7

1111

11

11

11

11

TO PILOT CONTROL PANELSEE SHEET 13

TO COPILOT CONTROL PANELSEE SHEET 13

13

8

8




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

W/G

W/O

W

W/B

DATA LO2 DATA HI

GND+28V4

3

1

CONTROL

To Gnet connections on G13160 J2, J4 and J6(typical for each Gnet bus)

6

87

5

9

PANEL

2

45

3

7

98

6

1 DATA LO

+28VGNDDATA HI

PANELCONTROL

2

45

3

7

98

6

1

ADDR 1

ADDR 3ADDR LO

ADDR 2

DATA LOW

+28VGND

ADDR 0

DATA HI

PANELCONTROL

Additional control panels or other Gnet interface devices as required, up to 15 total per Gnet bus.

AEJN

BFKP

DHMS

CGLR

W T

Y Z

G

RY

L

CH

SZ

M

D

F

PW

K

BE

NT

J

A

W/O

W

W/B

W/G

W/B

W

W/G

W/O

To additional control panel or additional terminal blocks if

required

To additional Control panel if required

W/O

W/B

W

W/G

W/G

W

W/B

W/O

W/G

W/O

W/B

W

W/O

W/B

W

W/G

"5" = 6-8-9"6" = 5-8-9"7" = 8-9"8" = 5-6-7-9

"9" = 6-7-9"A" = 5-7-9"B" = 7-9"C" = 5-6-9

For every control panel or other peripheral device connected to a particular Gnet bus, a unique device address from "1" to "9" or "A" to "F" must be wired into the connector. The address for each device on each Gnet bus is defined in the system configuration software for the specific installation.

Using 24 AWG wire 1.5" long for each jumper, connect the following pins together for Gnet addressing for each connector, as specified in the system configuration requirements. Make no connections to unlisted pins.

The first control panel on any given Gnet bus should be set as address "F" with no jumpers. Additional panels on the same bus should be given addresses in descending order: "E", "D", "C" etc.

ADDRESSSET TO 'F'

(SEE BELOW)

ADDRESSJUMPERS

(SEE BELOW)

ADDRESSJUMPERS

(SEE BELOW)

"1" = 6-7-8-9"2" = 5-7-8-9"3" = 7-8-9"4" = 5-6-8-9

"D" = 6-9"E" = 5-9"F" = NONE

GNET ADDRESS JUMPERS:

3

3

3

D9F 7

D9F 7

D9F 7

9

9

GNET DATA HIGNET DATA LO

GNET +28VGNET GND

G13162 A

P139-HD AUDIO SYSTEMGNET INTERCONNECTS

GA182 12 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

ADDR 0

ADDR 2

ADDR LOADDR 3

ADDR 1

ADDR 0

ADDR 2

ADDR LOADDR 3

ADDR 1


+28V AVIONICS POWER

AUDIOPANEL

5A

AIRFRAME GROUND

TO GNET CONNECTIONS ON J3 AND J4 (TYPICAL FOR EACH GNET CHANNEL)

BF

KP

WGNET DATA HI

GNET DATA LOW

W/B

If the audio system has more than 6 control panels an external power source for the additional panels must be provided. Up to 12 additional control panels may be powered from each external 5A breaker.

GNET EXTERNAL POWER:

A

E

J

N

T

B

F

K

P

W

C

G

L

R

Y

D

H

M

S

Z

Terminal blockinternal

connections9




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL

15

If six or less control panels are to be installed then each panel should be connected to a separate Gnet bus and terminal blocks are not required.

The pilot's primary control panel should be the first device on Gnet bus 1. The copilot's primary control panel should be the first device on Gnet bus 3. The control panel associated with HEADSET13 should be the first device on Gnet bus 5.

Additional control panels should be evenly distributed among available Gnet busses.

CONTROL PANEL BUS ASSIGNMENT:

9

15

TERMINAL BLOCK

PRELIMINARY4/10/15 00

10

J3 D9M10

COM1DIR

G13162 A

P139-HD AUDIO SYSTEMG13115 CONTROL HEAD WIRING

GA182 13 of 13

GA 3/27/14

SJC 3/27/14

CLB 3/27/14

J7


35

36

P2 D50M 5J2

3GND

6 COM ISO

P3

7 GND

8

TX PTT9

ICS PTT

ICS KEY 1

XMIT KEY 1

P7 D15FS

TO OTHER PTT SWITCHES

Pilot Control HeadG13160 Digital Audio System

REFER TO PAGE 6 OR PAGE 10

G13115 or G13116

12

The G13115 and G13116 control heads thave two electromechanical toggle switches on the front panel; an EMERG/NORMAL locking toggle switch, and a 3-position momentary switch for ICS/OFF/TX PTT. When each switch is "on" the appropriate pin on the J3 connector is connected to GND, pin 7.

The above wiring diagram illustrates the use of the EMER/NORMAL switch on the pilot's G13115/G13116 primary control panel to control the Emergency Mode operation for the pilot headset. The operation of the Digital Audio System in Emergency Mode is detailed in NOTE 8 on G13162 sheet 1.

The pilot's primary control head MUST be wired to COM1DIR as shown if this is the primary audio system installed. ONLY if the audio system is installed as a secondary may the connection be omitted and the COM1DIR pin on the G13160 be connected to ground.

In most installations, the copilot's primary control panel will be wired to COM2DIR, connecting to the appropriate pins as shown in the above table. Exceptions are if the audio system is not the primary audio system or if the HEADSET 2 port is not at a location used by flight crew. In these situations the COM2DIR pin on the G13160 should be directly connected to ground.

NOTE: When the Copilot goes into Emergency Mode, Headset Port 13 and Radio Ports 21 and 30 will also go into emergency mode as detailed in NOTE 8 on G13162 sheet 1.

The EMERG/NORMAL switch is only connected for the pilot and copilot control head. For other control panel locations, a G13115NS or G13116NS panel with the EMERG/NORMAL switch not instaled may be used.

The ICS PTT and TX PTT pins on the copilot control panel should be connected in parallel with the appropriate PTT switches on the copilot cyclic and/or foot switches.

In all other crew positions the ICS PTT and TX PTT pins on the associated control head may be connected in parallel with the appropriate PTT switches for that headset.

Copilot Pin AssignmentNAME G13115/6 G13160

COM2DIR J3 pin 6 J7 pin 11

GND J3 Pin 7 J7 pin 5

ICS KEY2 J3 pin 8 J4 pin 35

XMIT KEY 2 J3 Pin 9 J4 pin 36




PRO NO.

CHECKED

APPROVAL

DRAWN

SHT. DWG NO.

DATE

DATE

DATE TITLE

REV.

DESCRIPTION

REVISION

REV DATE APPROVAL