TM 55-1520-240-23-6
7-114
DISASSEMBLE AND INSPECT FLIGHT CONTROL RESERVOIR/COOLER
(AVIM)
(Continued)
7-114
NOTE
General inspection criteria (Task
7-1.1) for obvious damage applies
unless otherwise stated.
Inspection steps cover parts that are
subject to wear.
1.
Remove tube (1) between reservoir (2) and
manifold (3).
1.1.
Check tube (1) for dents and scratches. Dents
shall not be deeper than 0.050 inch. Scratches
shall not be deeper than 0.004 inch.
2.
Remove lockwire, three screws (4), and washers
(5). Remove manifold (3) with supply tube (6)
from reservoir (2).
3.
Remove nut (7) and elbow (8) from manifold (3).
4.
Remove cotter pin (9), pin (10) and supply tube
(6) from manifold (3).
5.
Remove two packings (11) from tube (8).
5.1.
Measure outside diameter of ends (11.1) of tube
(6). Diameter shall not be less than 1.13 inches.
Ends shall not be out of round more than 0.003
inch.
5.2.
Check tube (6) for dents and scratches. Dents
shall not be deeper than 0.180 inch. Scratches
shall not be deeper than 0.010 inch.
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