TCH.1C-27J-2-29JG
PROCEDURE:
CAUTION
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Make sure that No. 1 (No. 2) Hydraulic
System is filled andbled before you start
this functional test.This will prevent
damage to the equipment and loss of
mission effectiveness.
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2-30.1
Carry out the functional test of LH (RH) MLG low
pressure switch in according to the following
procedure:
A.Connect external electrical supply to the aircraft.
B.Open the circuit breaker HYD ACMP1 2DE (HYD
ACMP2 1DE) located on Rear Lower
CircuitBreakers Panel (455VE) in positions R 8 (R
11).
C.Place the ACMP1 (ACMP2) switch located on
Hydraulic/Smoke Detection Control Panel
(204VE)in ON position.
D.Verify that the ACMP1 (ACMP2) FAULT light
located on Hydraulic/Smoke Detection Control
Panel(204VE) illuminates.
E.Operate the ACMP1 (ACMP2) by engaging the
circuit breaker HYD ACMP1 2DE (HYD
ACMP21DE) located on Rear Lower Circuit
Breakers Panel (455VE).
F.Verify that the ACMP1 (ACMP2) FAULT light
located on Hydraulic/Smoke Detection Control
Panel(204VE) extinguishes.
G.Disconnect the external electrical supply from the
aircraft.
29-10-50
2-205