COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
Model FA5000
Initital Issue Page 17
Sep. 30/11
Description and Operation
23–70
−
40
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
B.
Physical Characteristics
For specific physical characteristic, refer to Section 800, Fits and Clearances.
C.
Electrical Characteristics
For specific electrical characteristics, refer to Section 800, Fits and Clearances.
D.
Environmental Characteristics
For specific environmental characteristics, refer to Section 800, Fits and Clearances.
E.
Crash and Fire Protection
For specific crash and fire protection specifications, refer to Section 800, Fits and
Clearances.
F.
CSMU Torque Requirement
For specific CSMU torque requirements, refer to Section 800, Fits and Clearances.
6.
INSTALLATION
The information provided in this section is for general knowledge use only. For authorized
detailed installation instructions, refer to the Model FA5000CVDR Installation and Opera-
tion Instruction Manual, p/n: 165E5327-01.
The Model FA5000 is an environmentally hardened unit housed in an trayless mounted
short box painted international orange. The FA5000 does not require external shock
mounting for installation into the aircraft. However, the Model FA5000CVDR has a mount-
ing chassis system and does not require an additional mounting tray for aircraft installa-
tion.
Table 6.
P/N: 5001
−
61XX
−
11 Pin Outs and Signal Descriptions
AI
J1
PIN
AIRCRAFT INTERFACE
SIGNAL NAME
I/O
FUNCTION
1
ATE ETHERNET TX ()
OUT
10/100BaseT/TX Ethernet TX+ and TX differen
tial pair, IEEE803.32002. Used for integrated auto
test with results display.
2
ATE ETHERNET TX (+)
OUT
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