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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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 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 430
 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
S 434-091-C02
 (64)
 If you installed an inboard thrust reverser half, make sure that the deflectors of the flap seal door are installed (AMM 78-31-09/401).

 S 434-092-C02

 (65)
 Install the fan cowl panel (AMM 71-11-02/401).

 S 224-100-C02

 (66)
 IF YOU INSTALLED A DIFFERENT THRUST REVERSER HALF OR CHANGED THE ENGINE; Do a check for aerodynamic smoothness between the fan cowl and the thrust reverser sleeve (AMM 78-31-10/201).

 S 414-110-C02

 (67)
 Supply hydraulic power (AMM 29-15-00/201).

 S 414-017-C02

 (68)
 Supply hydraulic pressure from the reservoir (AMM 29-09-00/201).

 S 714-095-C02

 (69)
 Do these tests in AMM 78-31-00/501 as follows:

 (a)
Indicator lights test.

 (b)
Normal Operation Test.

 1)  Operate the thrust reverser between the retract and the extend position until all the air is bled from reverser hydraulic system as evidenced by smooth translation of the sleeves.

 (c)
Auto-Restow Test.

 


 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 431 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
THRUST REVERSER - REMOVAL/INSTALLATION
______________________________________
 1.  General
_______
 A.  This procedure removes and installs the left or right thrust reverser half on the left or right engine.
 TASK 78-31-01-004-001-C03
 2.  Thrust Reverser Half Removal
____________________________
 A.  Equipment
 (1)  
Block, Pulley - C71002-77

 (2)  
Boom, Thrust Reverser Handling - C71002-2

 (3)  
Dolly, Thrust Reverser - C78011-1,
 Optional: C78002-1


 (4)  
Hoist Assembly - Fish Pole, F80039-1
 (or equivalent)


 (5)  
Fitting, Bootstrap Hoist Attach (Inboard) -C71003-2


 (6)  
Fitting, Bootstrap Hoist Attach (Outboard) -C71003-3


 (7)  
Matting, Rubber - 2 pieces - each approximately
 4 feet (1.2 meters) square


 (8)  
Pins, Attach, Hoist Fitting - C71003-104
 (2 quantity)


 (9)  
Sling, Thrust Reverser - C78003

 (10)
 Wrench Set, Thrust Reverser Hinge - C78014

 B.  
References

 (1)  
AMM 54-32-01/401, Forward Fairing

 (2)  
AMM 71-11-02/401, Fan Cowl Panels

 (3)  
AMM 78-31-00/201, Thrust Reverser System

 C.  
Access

 (1)  
Location Zones
 101/102 Flight Compartment
 506 No. 1 Engine
 606 No. 2 Engine


 D.  
Procedure


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 COWL/REVERSERS USED ON STRUTS WITH ú  78-31-01
 VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C01 Page 401 (AIRPLANES POST-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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