(2)
Access Panels
317AL APU Access Door - Left
318AR APU Access Door - Right
G.
Procedure
S 012-380
(1)
Open the left APU access door, 317AL, and right APU access door, 318AR:
(a)
While you hold the two APU access doors in the closed position, open the six latches on the right access door.
NOTE: The left access door will open fully and the right
____ access door will drop approximately one inch (2.5 cm) from the fuselage frame when the last latch is opened.
NOTE: A lanyard is attached to the aft end of the right access
____ door to hold the access door to the APU compartment bulkhead.
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747-400 MAINTENANCE MANUAL
CAUTION:_______ BE CAREFUL NOT TO MOVE THE TWO APU ACCESS DOORS TO THE
OUTBOARD SIDE FROM THE FULL OPEN POSITION. THE FULL OPEN
POSITION IS WHERE THE APU ACCESS DOOR IS DOWN AND THE TWO
HOLD-OPEN RODS ARE CONNECTED TO THE TWO BRACKETS ON THE
APU COMPARTMENT BULKHEAD. DAMAGE TO THE ELEVATOR CONTROL
SURFACES CAN OCCUR.
(b)
Open the left access door to the fully open position and remove the two hold-open rods from the two clips.
(c)
Remove the two quick-release pins from the two brackets on the left APU compartment bulkhead.
(d)
Connect the two hold-open rods from the left access door to the two brackets and install the two quick-release pins.
(e)
Push the right access door up and remove the lanyard from the pin on the aft APU compartment bulkhead.
(f)
Open the right access door to the fully open position and remove the two hold-open rods from the two clips.
(g)
Remove the two quick-release pins from the two brackets on the right APU compartment bulkhead.
(h)
Connect the two hold-open rods from the right access door to the two brackets and install the two quick-release pins.
S 862-117
(2)
Make sure the APU control switch on the P5 overhead panel is OFF and attach a DO-NOT-OPERATE tag.
S 862-118
(3)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6 Main Power Distribution Panel 1) 6H18, APU DC FUEL PUMP 2) 6K18, APU ALTN CONT
(b)
P83 Aft APU Equipment Control and Circuit Breaker Panel 1) APU PRIME CONT
(c)
P180 DC Power Distribution Panel 1) 180H4, FUEL BOOST PUMP CONT AFT 2 & FWD 3
(d)
P414 Power Distribution Center - Left Panel 1) 414R18, FUEL BOOST PUMP MAIN AFT 2
S 022-381
WARNING: DO NOT TOUCH THE IGNITION COMPONENTS UNTIL YOU DO THESE STEPS.
_______ THESE STEPS WILL RELEASE THE HIGH VOLTAGE FROM THE IGNITION EXCITER. IF YOU DO NOT OBEY THIS PROCEDURE, INJURY TO PERSONS CAN OCCUR.
(4)
Do these steps to release the high voltage from the ignition exciter:
(a)
Make sure six minutes have gone by since the last APU start.
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747-400 MAINTENANCE MANUAL
(b) Disconnect the electrical connector D95006 (P6) (7) from the ignition exciter (6).
CAUTION: DO NOT LET THE BRAIDS OR FERRULES OF THE TWO IGNITION
_______ CABLES MOVE WHEN YOU LOOSEN THE TWO COUPLING NUTS. DAMAGE TO THE TWO IGNITION CABLES CAN OCCUR.
(c) Loosen the two coupling nuts on the two ignition cables (5) until you can disconnect the ignition cables.
S 482-373
(5)
Install the oil flush cart:
(a) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 机载辅助动力 1(35)
