(d)
Put a DO-NOT-OPERATE tag on the flap control lever.
S 424-025
(2) Do these steps to install the power supply:
(a)
Put the power supply in its position on the mounting bracket.
(b)
Install the mounting bolts.
(c)
Connect the electrical connectors.
S 714-026
(3) Do these steps to do a test of the power supply:
(a) Make sure this circuit breaker is closed:
1) P6 Main Power Distribution Panel a) 6L32 ANTI COLL LTS WHITE
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-44-06
ALL ú ú 01 Page 404 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
WARNING: DO NOT LET THE STROBE LIGHT FLASH DIRECTLY IN YOUR EYES.
_______ THE INTENSITY OF THE STROBE LIGHT CAN CAUSE DAMAGE TO YOUR EYES.
(b)
Put the STROBE switch on the P5 panel to ON.
(c)
Make sure the strobe lights are on.
(d)
Put the STROBE switch on the P5 panel to OFF.
(e)
Make sure the strobe lights are off.
D. Put the airplane back to its usual condition
S 864-027
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT DO THE STEPS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(1) Do this task: "Safety Lock Removal and Leading Edge Flap
Activation" (Ref 27-81-00/201).
S 864-028
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(2)
Do this task: "Leading Edge Flap Retraction"
(Ref 27-81-00/201).
(3)
Remove the DO-NOT-OPERATE tag from the flap control lever.
S 864-029
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-44-06
ALL ú ú 01 Page 405 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
S 864-018
(4) Remove electrical power if it is not necessary (Ref 24-22-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
33-44-06
ALL ú ú 01 Page 406 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
TAIL CONE WHITE ANTI-COLLISION LIGHT - MAINTENANCE PRACTICES
____________________________________________________________
1. General_______
A. This procedure contains a task for the replacement of the lamps.
TASK 33-44-07-962-001
2. Lamp Replacement (Tail Cone White Anti-Collision Light) (Fig. 201)_______________________________________________________
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 燈 LIGHTS(116)
