(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
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 415 (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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
(8)
Pins, Attach, Hoist Fitting - C71003-104
(2 quantity)
(9)
Rod, Alignment C78015-1 (2 quantity)
(10)
Sling, Thrust Reverser - C78003
(11)
Wrench Set, Thrust Reverser Hinge - C78014
B. Consumable Materials
(1)
Cement, Synthetic Rubber Buna N - BMS 5-36
(AMM 70-10-01/201)
(2)
Clay, Modeling
(3)
Grease, Aircraft Ball and Roller Bearing -BMS 3-24 (AMM 70-10-01/201)
(4)
Primer - BMS 10-11, Type 1 (AMM 70-10-01/201)
C. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 29-15-00/201, Hydraulic System A, B and Standby
(3)
AMM 54-32-01/401, Forward Fairing
(4)
AMM 71-11-02/401, Fan Cowl Panels
(5)
AMM 78-31-00/201, Thrust Reverser System
(6)
AMM 78-31-05/401, Cascades
(7)
AMM 78-31-08/401, Fan Duct Cowl and Thrust Reverser Opening Actuator
(8)
AMM 78-31-09/401, Flap Seal Door Deflector
(9)
AMM 78-34-02/201, Feed Back Push-Pull Cables
D. Access
(1) Location Zones
101/102 Flight Compartment
506 No. 1 Engine
606 No. 2 Engine
E. Procedure
S 864-029-C02
WARNING: BE CAREFUL WHEN YOU REMOVE AND INSTALL THE THRUST REVERSER IN
_______ SUDDEN STRONG WINDS CONDITIONS. DO NOT USE THE HOLD-OPEN ROD TO HOLD THE COWLING IN THE OPEN POSITION IF THE WIND VELOCITY IS MORE THAN 60 KNOTS. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE EQUIPMENT.
WARNING: DO THE DEACTIVATION PROCEDURE TO PREVENT THE OPERATION OF THE
_______ THRUST REVERSER. THE ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do the deactivation procedure for the thrust reverser for ground maintenance (AMM 78-31-00/201).
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 416 (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 044-026-C02
(2) Open the circuit breakers and attach the DO-NOT-CLOSE tags for the applicable engine as follows:
(a) P6 Load Control Center
1) ENG 1 THR REV IND SYS
2) ENG 2 THR REV IND SYS
3) ENG 1 SYNC LOCK
4) ENG 2 SYNC LOCK
5) ENG 2 SYNC LOCK - ALTN
S 864-032-C02
(3) Make sure you remove the forward two hinge seal supports from the upper bifurcation of the thrust reverser.
S 434-004-C02
CAUTION: MAKE SURE THAT THE THRUST REVERSER HALVES DO NOT CLOSE AT THE
_______ SAME TIME BEFORE THE FINAL ADJUSTMENT. THIS CAN CAUSE STRUCTURAL DAMAGE TO THE THRUST REVERSER HALVES.
(4)
Adjust the compression rods (Fig. 404) to the length shown.
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