S 424-020
(4)
Install the electrical connector on the DC motor (DV906 right, DV91C left).
S 434-018
(5)
Install the safety screen.
E. Outflow valve manual operation test
S 864-010
(1)
Apply electrical power (Ref 24-22-00/201).
S 864-011
(2)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6 Main Power Distribution Panel
1) 6J28 CABIN PRESS AUTO A
2) 6J31 CABIN PRESS CONT R
3) 6J30 CABIN PRESS CONT L ICU
4) 6J31 CABIN PRESS CONT R ICU
5) 6L6 CABIN PRESS MAN L
6) 6L7 CABIN PRESS MAN R
(b)
P414 Main Power Distribution Panel
1) 414M8 CABIN PRESS ICU LEFT
2) 414B8 CABIN PRESS ICU RIGHT
(c)
P83 Aft Equipment Center
1) OUTFLOW VALVE-R
2) OUTFLOW VALVE-L
S 714-019
(3) Do a manual operation test:
(a)
Push the applicable (MAN L or MAN R) switch-light, on the P5 panel, to the ON position.
(b)
Move the OPEN/CLOSE switch, on the P5 panel, to the CLOSE position.
(c)
Make sure the outflow valve position indicator moves to the closed position.
(d)
Move the OPEN/CLOSE switch, on the P5 panel, to the OPEN position.
(e)
Make sure the outflow valve position indicator moves to the fully open position.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-31-08
ALL ú ú 01 Page 404 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(f) Push the applicable (MAN L or MAN R) switch-light, on the P5 panel, to the off position.
S 864-016
(4) Remove electrical power (Ref 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
21-31-08
ALL ú ú 03 Page 405 ú Jun 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
OUTFLOW VALVE FLAPPER DOORS - REMOVAL/INSTALLATION
__________________________________________________
1. General_______
A. There are two tasks in this procecure. The first task is the removal of the Outflow Valve Flapper Door, the second task is the installation of the Outflow Valve Flapper Door.
B. Access to both outflow valves is through the access door in the aft bulkhead of the bulk cargo compartment. Since both valves are identical, the flapper doors on only one (the left valve) will be covered.
TASK 21-31-09-004-001
2. Outflow Valve Flapper Doors Removal (Fig. 401)___________________________________
A. References
(1)
IPC 21-31-01 Fig. 2
(2)
WDM 21-31-13, 21-31-21, 21-31-22
(3)
SSM 21-31-02, 21-31-04
B. Access
(1) Location Zone
151 Area Aft of Bulk Cargo Compartment, LH
152 Area Aft of Bulk Cargo Compartment, RH
C. Procedure
S 864-003
(1) Open these circuit breakers and attach DO-NOT-CLOSE tags:
(a)
P6 Main Power Distribution Panel
1) 6J28 CABIN PRESS AUTO A
2) 6J29 CABIN PRESS AUTO B
3) 6J30 CABIN PRESS CONT L ICU
4) 6J31 CABIN PRESS CONT R ICU
5) 6L6 CABIN PRESS MAN L
6) 6L7 CABIN PRESS MAN R
(b)
P414 Main Power Distribution Panel
1) 414M8 CABIN PRESS ICU LEFT
2) 414B8 CABIN PRESS ICU RIGHT
(c)
P83 in the aft equipment center
1) OUTFLOW VALVE-R
2) OUTFLOW VALVE-L
S 014-004
(2)
Remove the access panel on the aft bulkhead of the bulk cargo compartment to get access to the outflow valves (1).
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 空調 AIR CONDITIONING 1(126)
