COMPONENT MAINTENANCE MANUAL
AVIATION PRODUCTS
Model FA5000
Rev. 02 Page 27
July 21/17
Description and Operation
23–70−30
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
ERASE A
ERASE C
PUSH TO TEST
2
PILOT AUDIO
CO‐PILOT AUDIO
SPARE AUDIO
(TO 3RD CREW MEMBER
OR PA SYSTEM)
CHASSIS
GROUND
TEST INDICATOR
RECORD ON
AIRCRAFT WIRING INTERLOCKS
(LANDING GEAR MUST BE DOWN
AND BRAKE LOCKED TO ALLOW
MEMORY TO BE ERASED)
CHANNEL 1
CAM
CHANNEL 2
CHANNEL 3
AIRCRAFT
INTERFACE
PWA
MONITOR
AUDIO TO
HEADSET
JACK
2
2
2
2
2
2
MAIN
PROCESSOR
PWA
CSMU
(Crash Survivable Memory Unit)
ASSEMBLY
(CRASH PROTECTED SOLID STATE MEMORY)
TO AIRCRAFT
FAULT MONITORING
SYSTEM
GSE OUTPUT
COCKPIT
AREA
MICROPHONE
(CAM)
STOP RECORDING/
MODEL FA5000 GACVR
GACVR FAULT
TO GROUND STATION
TEST EQUIPMENT
GMT_IN_B (429)
GMT_IN_A (429)
GEAR
BRAKE
AUDIO OUT
+18 VDC
115 VAC
400 Hz
**OMS OUTPUT A 429
**OMS OUTPUT B 429
**DATA LINK FAULT
**DATA LINK & OMS GACVR
**DATA LINK IN B 429
**DATALINK IN
A 429
***RIPS FAULT INPUT
***RIPS MAINTENANCE INPUT
***RIPS ACTIVE INPUT
**DATA LINK VALID
***EXTERNAL RIPS INTERFACE
TO GACVR
*CAN BE CUSTOMER SUPPLIED
*
(Except P/N
5000-5001-50)
28 VDC
RIPS
(Internal)
Figure 15.
Model FA5000 GACVR (P/N: 500X‐500X‐50)
Functional System Block Diagram
The document reference is online, please check the correspondence between the online documentation and the printed version.
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