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时间:2011-04-11 09:23来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (5)  
Do this task: "Safety Lock Removal and Leading Edge Flap
 Activation" (Ref 27-81-00/201).


 (6)
Do this task: "Leading Edge Flap Retraction: (Ref 27-81-00/201).


 S 862-080
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 33-42-02
 ALL  ú ú 08 Page 214 ú Feb 18/02
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A
747-400 MAINTENANCE MANUAL
 S 862-081
 (7)  
Remove the DO-NOT-OPERATE tag for the flap control lever.

 S 862-050

 (8)  
Remove electrical power if it is not necessary (Ref 24-22-00/201).


 TASK 33-42-02-962-051
 4.  Transformer Replacement (Fig. 205)_______________________
 A. Special Tools and Equipment
 (1)  Lock, Leading Edge Flap Drive Unit (Ref 27-81-00/201)
 B. Parts ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 203 | 1 | Mounting screw | 33-42-02 | 01 | 15 | | | 2 | Transformer | | | 10 | 2......…........…...................................…............….....….......1
 C. References
 (1)  
20-11-14/701, Metal Surfaces, Cleaning and Preperation for Bonding

 (2)  
24-22-00/201, Manual Control, Electrical Power Generation System

 (3)  
27-81-00/201, Leading Edge Flap System

 (4)  
SSM 33-42-10


 D. Access
 (1)  Location Zone
 511 Leading Edge to Front Spar, Left
 611 Leading Edge to Front Spar, Right

 E. Procedure
 S 862-127
 (1)  Prepare to replace the transformer
 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 AND DAMAGE TO EQUIPMENT.
 (a)  Do this task: "Leading Edge Flap Extension" (Ref 27-81-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 33-42-02
 ALL  ú ú 05 Page 215 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

LEADING EDGE CAVITY ACCESS DOORS
SEE A
INSTALLED) DOOR (WHEN CAVITY ACCESS LEADING EDGE  TRANSFORMERS 2. LANDING LIGHT  WING RIB TRANSFORMER AND SURFACE BETWEEN CRITICAL FAYING 
15V AC IN 4. CONNECTOR 3. OUTPUT WIRES 
SEE  B  (EXAMPLE) 5. GROUND STUDS 
FLAP (REF) KRUEGER  LIGHT LANDING OUTBOARD  (4 LOCATIONS) SCREWS 1. MOUNTING 
TRANSFORMER INSTALLATION (ON LEADING EDGE BETWEEN LANDING LIGHTS) 
A  B 
Figure 205 Landing Light Transformer Replacement 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 33-42-02
 ALL  ú ú 06 Page 216 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 WARNING:
_______
 (b)

(c)

(d)

(e)

(f)

(g)


A
747-400
MAINTENANCE MANUAL

YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO INSTALL
 THE LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU
 DO NOT INSTALL THE SAFETY LOCKS CORRECTLY. THIS CAN CAUSE
 INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.

Do this task: "Extended Leading Edge Flap Deactivation and
 Safety Lock Installation" (Ref 27-81-00/201).
Install a DO-NOT-OPERATE tag on the flap control lever.
Get access to the rear of the landing light through the access
 door.
 
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本文链接地址:747-400 AMM 飞机维护手册 灯 LIGHTS(90)