BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 224-097-C03
(52)
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 414-106-C03
(53)
Supply hydraulic power (AMM 29-15-00/201).
S 414-107-C03
(54)
Supply hydraulic pressure from the reservoir (AMM 29-09-00/201).
S 714-100-C03
(55)
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.
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COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C03 Page 430 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
THRUST REVERSER - CLEANING/PAINTING
___________________________________
TASK 78-31-01-807-017-C00
1. Thrust Reverser Witness Mark Installation_________________________________________
A. Equipment
(1)
B780092/21 - Thrust Reverser Maintenance Lock Equipment
B.
Consumable Materials
(1)
C00033 BMS 10-60 Type II
C.
References
(1)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
D.
Access
(1)
Location Zones
101/102 Flight Compartment
506 No. 1 Engine
606 No. 2 Engine
E.
Apply The Witness Mark
S 867-017-C00
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL
_______ SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1)
Supply the hydraulic power (AMM 29-15-00/201).
S 867-026-C00
(2)
Slowly move the engine No. 1(2) reverse thrust lever up and aft to the extended position.
(a) Make sure that the reverser sleeves on engine No. 1(2) move to the fully extended position.
S 867-000-C00
(3) Move the engine No. 1(2) reverse thrust lever forward and down to the retracted position.
(a) Make sure that the reverser sleeves on engine No. 1(2) move to the fully retracted position.
S 047-020-C00
WARNING:_______MAKE SURE THAT YOU DEACTIVATE THE DEPLOY CONTROL CIRCUIT. THIS PROCEDURE REQUIRES HYDRAULIC PRESSURE TO BE APPLIED. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(4) Disconnect the electrical connectors D3052 (ENG 1) or D3056 (ENG 2) from the control valve module of the thrust reverser (Fig. 701).
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78-31-01
ALL ú ú C01 Page 701 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
GROUND SUPPORT EQUIPMENT WIRE BUNDLE
AIRPLANE WIRE BUNDLE
REVERSER CONTROL VALVE MODULE
A
Ground Support Equipment Wire Bundle Installation
Figure 701
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