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时间:2011-04-09 10:08来源:蓝天飞行翻译 作者:航空
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 COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
 VIBRATION ISOLATOR SUSPENSION AND  ú  CONFIG  2
 WITH HINGE CROSS RODS  ú  C01  Page 409
 (AIRPLANES PRE-BOEING-SB 737-54-1036)  ú  Jul 12/00 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

HINGE SLIDER HALVES
A-A
Hinge Slider/Track Wear Limits

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. COWL/REVERSERS USED ON STRUTS WITH ú
 78-31-01 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2 WITH HINGE CROSS RODS ú C01 Page 410 (AIRPLANES PRE-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G67759
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-113-C02
 (21) Disconnect the electrical connector D1008 (D1016) from the sync lock (View B, Fig. 402).
 (a)  
Remove the lacing tape that ties the sync lock wiring harness to the thrust reverser wiring harness.

 (b)  
Remove the sync lock wiring harness (W1412) from the clamps that are attached to the thrust reverser. 1) Make sure the clamps are installed around the thrust

 reverser wiring harness after you remove the sync lock wire harness (W1412) from the clamps.

 (c)
Secure the wiring harness away from the thrust reverser so it will not be damaged when the thrust reverser is removed.

 (d)  
Install the protective caps on the plug and receptacle.


 S 034-020-C02
 (22) Disconnect the electrical connector (View B and F, Fig. 402) from the bracket on the fan cowl support beam.
 (a)  Install the protective caps on the plug and receptacle.
 S 034-018-C02
 CAUTION:_______MAKE SURE YOU CLEAN ALL THE HYDRAULIC FLUID LEAKAGES. THIS CAN CAUSE DAMAGE TO THE EQUIPMENT.
 (23) Disconnect the hydraulic lines (View B and F, Fig. 402) from the fan cowl support beam.
 (a)  Put the protective caps on the open fittings and lines.
 S 494-022-C02
 (24) If the bootstap handling equipment for the thrust reverser is to be used, install the equipment as follows (Fig. 403):
 (a)  
Attach the inboard and outboard bootstrap hoist attach fittings to the fittings on the strut forward bulkhead (View A, Fig. 403).

 (b)  
Attach the boom support to the hoist attach fittings
 (View A, Fig. 403).


 (c)  
Attach the base to the boom support.

 (d)  
Put the boom into the base.

 (e)  
Install the upper attach fittings of the sling, C78003, to the bushed clevis fittings on the upper bifurcation of the thrust reverser (View B, Fig. 403).


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú  78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2 WITH HINGE CROSS RODS ú C03 Page 411 (AIRPLANES PRE-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
BOOM
SEE A PULLEY BLOCK
FISHPOLE HOIST
SEE B
THRUST REVERSER SLING
SEE C
BOOM
BASE
BOOM 
ATTACH PIN SET  SUPPORT 
(2 LOCATIONS) 
BOOTSTRAP HOIST 
ATTACH FITTING 
(2 LOCATIONS) 
STRUT FITTING 
(2 LOCATIONS)

A

Thrust Reverser Handling Equipment
Figure 403 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
 VIBRATION ISOLATOR SUSPENSION AND  ú  CONFIG  2
 WITH HINGE CROSS RODS  ú  C02  Page 412
 
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