S 417-024
(2)
Close the APU access doors.
(a)
Do a visual check of the EGT bus bars: 1) Make sure the bus bars are not damaged. 2) Make sure no metal parts touch the bus bars. 3) Make sure the bus bars do not touch each other.
(b)
Disengage the support rods for the APU access doors.
(c)
Put the support rods in the clips on the inner side of the APU access doors.
(d)
Make sure the insulation covers attach correctly to the APU compartment firewall.
(e)
Close the APU access doors.
(f)
Close the latches on the APU access doors.
S 867-025
(3)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P83 Panel, E8 Aft Equipment Center
1) APU PRIMARY CONT
(b)
P6 Main Power Supply Panel
1) 6K18 APU ALTN CONT
S 867-026
(4) Remove the DO-NOT-OPERATE tag from the APU control switch on the P5 panel.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-16-00
ALL ú ú 03 Page 705 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
COMBUSTION CHAMBER DRAIN VALVE - REMOVAL/INSTALLATION
_____________________________________________________
1. General_______
A. This procedure contains the tasks to remove and install the drain valve for the combustion chamber.
B. The drain valve for the combustion chamber is on the combustion chamber in the six o'clock position. It is connected to the drain system interface through a drain tube.
C. You can get access to the drain valve through the APU access doors.
TASK 49-16-01-004-001
2. Combustion Chamber Drain Valve Removal (Fig. 401)______________________________________
A. References
(1)
IPC 49-16-01 Fig. 1
B.
Access
(1)
Location Zone 317 APU Compartment-Six O'Clock Position On Gas Generator Case, LH
318 APU Compartment-Six O'Clock Position On Gas Generator Case, RH
(2)
Access Panel
317AL APU Access Door
318AR APU Access Door
C.
Procedure
S 864-002
(1)
Make sure the APU control switch on the P5 panel is OFF and attach a DO-NOT-OPERATE tag.
S 864-003
(2)
Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6 Main Power Supply Panel
1) 6K18 APU ALTN CONT
(b)
P83 Panel, E8 Aft Equipment Center
1) APU PRIMARY CONT
S 014-004
(3)
Open the APU access doors:
(a)
Open the latches on the APU access doors.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-16-01
ALL ú ú 01 Page 401 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SEE A
GAS GENERATOR
CASE8. GASKET
1.
SEAL COVER
2.
GASKET
3.
RETAINER RING
4.
DRAIN VALVE DRAIN VALVE
5.
SPRING ASSEMBLY
6.
DRAIN VALVE ADAPTER
7.
DRAIN LINE
A
Combustion Chamber Drain Valve Installation Figure 401
F58216
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-16-01
ALL ú ú 02 Page 402 ú Feb 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(b)
Open the APU access doors.
(c)
Engage the support rods for the APU access doors.
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 機(jī)載輔助動力 1(136)
