TM 1-1520-238-23
13-100
13.30.
FORWARD AVIONICS BAY VANEAXIAL FAN REMOVAL/INSTALLATION - continued
c. Install fan (3) on fuselage (23).
(1) Position fan (3) on fuselage (23).
(2) Install two screws (8) and washers (9) on fan
(3).
d. Install fan wire harness (1) on bracket (11) and
fan (3).
(1) Install clamps (16) and (18) on fan wire har-
ness (1).
(2) Install screw (8) through washer (9), clamp
(18), and fan (3).
(3) Install screw (12) through washer (13), clamp
(14), spacer (15), clamps (16) and (17), and
bracket (11).
e. Install clamp (19) on fan (3).
(1) Install screw (8) and washer (9).
f. Attach fan electrical wires (20) to splices (21)
on wire harness (22) (W118 left or W119 right)
(TM 55-1500-323-24).
g. Apply sealing compound to four screws (8).
Use sealing compound (item 178, App F).
h. Install left or right forward avionics bay va-
neaxial fan air duct (para 13.31).
i. If removed, install TB 305 track assembly
(para 9.54).
j. Inspect (QA).
k. Perform ECS maintenance operational check
(TM 1-1520-238-T).
l. Install access panel L60 or R60 (para 2.2).
END OF TASK
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M04-663-9
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M04-663-1 1
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