S 864-028-C01
(30)
Lower the thrust reverser half and attach it to the dolly (or the shipping container).
S 094-029-C01
(31)
Remove the sling and fittings unless you are going to install the same thrust reverser half again.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C01 Page 414 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
TASK 78-31-01-404-030-C01
3. Thrust Reverser Half Installation
_________________________________
A. Equipment
(1)
Block, Pulley - C71002-77
(2)
Boom, Thrust Reverser Handling - C71002-2
(3)
Dolly, Thrust Reverser - C78011-1 or 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)
Rod, Alignment C78015-1 (2 required)
(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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITHOUT ú 78-31-01
VIBRATION ISOLATOR SUSPENSION ú CONFIG 1 ú C01 Page 415 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
E. Procedure
S 844-091-C01
(1) Make sure that the thrust reverser you are to install is a
non-isolated thrust reverser.
(a) If the thrust reverser you are to install is an isolated thrust reverser, make sure that Service Bulletin 737-78-1059 is completed before you install an isolated thrust reverser on an airplane with non-isolated struts.
S 844-092-C01
(2) If you are to install a new thrust reverser on the airplane, make
sure the forward hinge link for the thrust reverser has been
transferred to the new one to be installed.
S 044-030-C01
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.
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. 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：737-300 400 500 AMM 飞机维护手册 EXHAUST(57)
