COMPONENT MAINTENANCE MANUAL
AVIATION RECORDERS
Model FA5000
Initial Issue Page 705
Sep. 30/11
Assembly
23–70–40
Use or disclosure of information on this sheet is subject to
the restrictions on the cover page of this document.
DETAIL “A”
(1
−
65)
(1
−
70)
(1
−
75)
(1
−
60)
(1
−
120)
(1
−
55)
(1
−
50)
(1
−
85)
(QTY 2)
(QTY 2)
SEE DETAIL “A”
P
−
5
Connector
(1
−
110)
(1
−
115)
(QTY 2)
(1
−
135)
(1
−
100)
J2
Connector
Some parts are removed
for clarity purposes
NOTE:
(1
−
5)
(REF,)
(QTY 2)
J
−
7
J
−
6
RED
BLACK
(1
−
140)
Torque (5
−
6
in/lbs)
Torque
(5
−
6 in/lbs)
Torque
(2
−
3
in/lbs)
Torque2
−
3
in/lbs)
Figure 702. Main Processor (MP) Installation Diagram
D.
Aircraft Interface PWA (AI) Installation
(See Figure 703 or IPL Figure 1, Item 30)
AIRCRAFT INTERFACE PWA INSTALLATION PROCEDURE
NOTE:
Apply Loctite to all screw installations for the following proced-
ures:
The document reference is online, please check the correspondence between the online documentation and the printed version.