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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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747-400
MAINTENANCE MANUAL


ELECTRICAL
CONNECTOR


BRACKET
A-A B-B Flap Power Package Installation Figure 401 (Sheet 4)
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MAINTENANCE MANUAL

 S 034-013

 CAUTION:_______ MAKE SURE THAT THE FLAPS ARE FULLY RETRACTED BEFORE YOU
 DISCONNECT THE RVDT.  YOU CANNOT EASILY SET UP THE RVDT FOR
 INSTALLATION IN THE TRANSMISSION IF IT IS REMOVED WITH FLAPS

 EXTENDED.
 (6)  
Disconnect the electrical connector from the applicable RVDT (11) (AMM 27-58-01/401):

 (a)  
DM7889, Inboard Power Pack Transmitter

 (b)  
DM7892, Outboard Power Pack Transmitter


 S 034-014
 (7)  
Disconnect the electrical connector from the applicable limit switch pack (12) (AMM 27-51-18/401):

 (a)  
DS2102, Inboard Limit Switch Pack

 (b)  
DS2103, Outboard Limit Switch Pack


 S 034-015
 (8)  
Disconnect the hydraulic lines from the flap control module (7):

 (a)  
Disconnect the two hydraulic lines (10) from the power package (1).

 (b)  
Install plugs in the hydraulic lines (10) andcaps to prevent contamination in the open ports.


 S 494-031
 (9)  
Install the support equipment to the flap power package:

 (a)  
Attach the fishpole hoist to the lift point on the wheel well bulkhead (Fig. 401).

 (b)  
Attach the hoisting adapter to the lift lugs on the power package (1)


 S 024-032
 (10)
 Remove the flap power package:

 (a)  
Remove the three bolts (21).


 NOTE:____ Manually hold the flap power package (1) in its position
 while you remove the bolts.  The power package will move
 away from the bulkhead when you remove the bolts
 (Fig. 401).
 (b)  Lower the flap power package (1) from the airplane.
 (c)  Remove the fishpole hoist and hoisting adapter.
 (d)  Remove the bushings (18 and 23) from the mounting lugs and
 attach a tag to them.
 (e)  Remove the adapters (14) from the flap control module.  Install
 a cap in the open ports.

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747-400 MAINTENANCE MANUAL
 TASK 27-51-09-404-016
 3.  Flap Power Package Installation_______________________________
 A. Special Tools and Equipment
 (1)  
PF51003-1 or PF51-009-1, Fishpole Hoist, available commercially, or equivalent.

 (2)  
OHME65B81110-1, Inboard TE Flap Power Unit Hoisting Adapter

 (3)  
OHME65B81111-3, Outboard TE Flap Power Unit Hoisting Adapter

 B.
Consumable Materials

 (1)  
D00054, Lubricant - Assembly, Skydrol, MCS 352

 (2)  
G00062, Fluid - Hydraulic, Fire Resistant, BMS 3-11


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747-400
MAINTENANCE MANUAL

 C. Parts ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 1 | Power Pack (INBD) | 27-51-09 | 01 | 48 | | | 1 | Power Pack (OUTBD) | | 03 | 82 | | | 3 | Bolt (INBD) | 27-51-08 | 01 | 5 | | | 3 | Bolt (OUTBD) | | | 5 | | | 4 | Washer (INBD) | | | 15 | | | 4 | Washer (OUTBD) | | | 15 | | | 5 | Nut (INBD) | | | 20 | | | 5 | Nut (OUTBD) | | | 20 | | | 14 | Adapter (INBD) | 27-51-09 | 01 | 135 | | | 14 | Adapter (OUTBD) | | 03 | 152 | | | 15 | Packing (INBD) | | 01 | 145 | | | 15 | Packing (OUTBD) | | 03 | 173 | | | 16 | Ring (INBD) | | 01 | 162 | | | 16 | Ring (OUTBD) | | 03 | 183 | | | 17 | Packing (INBD) | | 01 | 155 | | | 17 | Packing (OUTBD) | | 03 | 163 | | | 18 | Bushing (INBD-CNTR) | | 01 | 44 | | | 18 | Bushing (OUTBD-CNTR) | | 03 | 67 | | | 18 | Bushing (INBD-SIDE) | | 01 | 450 | | | 18 | Bushing (OUTBD-SIDE-UPPER) | | 03 | 532 | | | 18 | Bushing (OUTBD-SIDE-LOWER) | | | 592 | | | 19 | Washer (INBD) | | 01 | 38 | | | 19 | Washer (OUTBD) | | 03 | 57 | | | 20 | Nut (INBD) | | 01 | 42 | | | 20 | Nut (OUTBD) | | 03 | 62 | | | 21 | Bolt (INBD) | | 01 | 34 | | | 21 | Bolt (OUTBD-UPPER) | | 03 | 37 | | | 21 | Bolt (OUTBD-LOWER) | | | 42 | | | 21 | Bolt (OUTBD-MID) | | | 47 | | | 22 | Washer (INBD) | | 01 | 36 | | | 22 | Washer (OUTBD) | | 03 | 52 | | | 23 | Bushing (INBD-CNTR) | | 01 | 46 | | | 23 | Bushing (OUTBD-CNTR ) | | 03 | 72 | | | 23 | Bushing (INBD-SIDE) | | 01 | 420 | | | 23 | Bushing (OUTBD-SIDE) | | 03 | 577 | 2......…........…...................................…...........….....…........1
 
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