TM 55-1520-240-23-6
7-330
BLEED UTILITY HYDRAULIC WHEEL BRAKE SYSTEM
(Continued)
7-330
Filter assembly kit
ADHT6814-M9716M must be
installed in test stand pressure
lines. Otherwise, system can be
contaminated.
NOTE
To operate hydraulic test stand, refer
to applicable manual.
PILOT’S RIGHT AND LEFT WHEEL BRAKE SYSTEM
1.
Working in cockpit, tag and disconnect hose
(1) from PRESS port (2) of pilot’s right brake
cylinder (3).
2.
Install cap (4) in port (2) of cylinder (3).
3.
Tag and disconnect hose (5) from RTN port (6)
of cylinder (3).
4.
Install plug (7) in hose (5).
5.
Connect hose (1) to port (6) of cylinder (3).
6.
Remove bleed plug (8) from port (9) of cylinder
(3).
7.
Connect hose (10) to port (9) of cylinder (3).
Position loose end of hose in container.
8.
Install plug (11) in hose (10).
9.
Working at right forward landing gear, connect
bleed hoses (12) to bleed fittings (13) of two
wheel brake cylinders (14 and 15). Position
hoses in container.
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