S 004-104
(2)
Remove a switch from a latch fitting.
(a)
Remove the lockwire from the locknut.
(b)
Remove the locknut, the key washer and the lockwasher from the switch.
(c)
Remove the switch from the latch fitting.
(d)
Disconnect the switch wiring from the airplane wiring at the appropriate connector.
NOTE: The connectors are under access panels inside the
____
door opening.
TASK 52-71-01-004-111
10. Crew Compartment Overhead Hatch Warning Switch Removal (Fig. 407)
______________________________________________________
A. Access
(1)
Access Panel
839L Control Cabin Overhead Hatch
(2)
Location Zone
221 Control Cabin, LH
B.
Procedure
S 864-113
(1)
Open these circuit breakers for the applicable EICAS system and attach the DO-NOT-CLOSE tags:
(a)
P7 Overhead Circuit Breaker Panel
1) 7F8 UPR EICAS
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-71-01
ALL ú ú 10 Page 420 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
A-A Crew Compartment Overhead Hatch Warning Switch Installation Figure 407
C78954
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-71-01
ALL ú ú 06 Page 421 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
2) 3) 4) 5) 7F9 7F10 7F14 7F15 EIU LEIU CLWR EICASEIU R
(2) S 014-114Remove the interior lining to get access to the switch.
(3) S 034-115Disconnect the electrical wire from the switch.
(4) S 024-116Remove the safety wire and loosen the locknuts to remove the switch.
TASK 52-71-01-404-029
11. Main Electronic Equipment Door Warning Switch Installation (Fig. 401)
__________________________________________________________
A. References
(1)
AMM 24-22-00/201, Manual Control
(2)
IPC 52-75-01 Fig. 1
(3)
SSM 52-71-01
(4)
WDM 52-71-14
B.
Access
(1)
Location Zone 118 Electrical and Electronics Compartment, RH
(2)
Access Panel
117A Door - Electronics Compartment Access
C.
Procedure
S 424-010
(1)
Install warning switch for the main electronic equipment door (Fig. 401).
(a)
Remove the roller guide assembly and locknut from the new switch.
(b)
Align the switch with the keyway and insert it into the cutout.
(c)
Close and lock the door.
(d)
Put the switch in the mounting bracket with the plunger against the actuator.
(e)
Connect the wiring to switch.
(f)
Adjust the position of the switch in the mounting bracket until the switch operates.
NOTE: Keep the locknuts finger-tight against the bracket.
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-71-01
ALL ú ú 10 Page 422 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(g) Turn the 2 locknuts two more full turns to allow the switch plunger to be further depressed in the switch.
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 飛機維護手冊 艙門 DOORS 4(86)
