TCH.1C-27J-2-29JG
2-8.2
FLUSHING NO. 2 SYSTEM (refer to figure
)
(Cont'd)
NOTE
If a not modified cartridge has been used : If
the clogging indicator of the return filter
comes out during the flushing procedure,
stop the operation. Visually check return
filter cartridge. In case of heavy
contamination replace the filter element, and
restart the procedure afterwards.
8.Regulate the test stand (AGE NO. 00262) at flow rate
of 13 gpm (50 l/min), the pressure line at 3000 psi
(211 kg/cm²).
9.Start and operate the test stand according to the
applicable procedures.
10.Cycle rudder, ailerons and elevator through their full
deflection by moving rudder pedals and control wheel
for 15 minutes. Actuate wheel brakes (normal) for 15
minutes. Use caution to prevent damage to
components.
11.Actuate ramp and cargo door, attitude variation
system and flaps through 10 complete cycles.
12.Jack the Aircraft (AGE NO. 00014 and AGE NO.
00015) and actuate the Landing Gear through 10
complete cycles.
13.With hydraulic test stand (AGE NO. 00262) regulated
as per above step 6, drain reservoir by opening the
reservoir drain cock (8). After emptying reservoir, refill
it again.
14.Take an hydraulic fluid sample from the system in
accordance with (refer to para ) .
(Cont'd)
29-10-00
2-54