TM 1-1520-238-23
8-89
8.34.
PILOT STANDBY ATTITUDE INDICATOR REMOVAL/INSTALLATION – continued
c. Remove standby attitude indicator (1) from
instrument panel (2).
(1) Remove three screws (3).
(2) Pull indicator (1) from panel (2).
(3) Detach connector P383 (4) from receptacle
(M302)J1 (5).
8.34.4. Cleaning
a. Wipe mounting area and indicator with a clean
rag.
8.34.5. Inspection
a. Check indicator and panel mounting area for
cracks, nicks, and dents (para 8.29).
b. Check panel screw holes for stripped or dam-
aged threads (para 8.29).
8.34.6. Installation
a. Install indicator (1) in panel (2).
(1) Attach connector P383 (4) to receptacle
(M302)J1 (5).
(2) Aline indicator (1) with screw holes in panel
(2).
(3) Install three screws (3).
b. Inspect (QA).
c. Perform flight instruments maintenance op-
erational check (TM 1-1520-238-T).
END OF TASK
M04-201-3
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M04-201-4
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M04-201-5
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M04-201-6
