EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-21-01
ALL ú ú C02 Page 406 ú Nov 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
FORWARD ENGINE MOUNT THRUST LINK ASSEMBLY - REMOVAL/INSTALLATION
________________________________________________________________
1. General_______
A. This procedure has two tasks, to remove and install the thrust link
assembly.
B. The thrust link assembly of the forward engine mount extends from these
locations:
(1)
The fittings on the right and left sides of the fan frame.
(2)
To the same thrust fitting installed on the bottom of the strut.
TASK 71-21-02-004-001-C00
2. Thrust Link Assembly Removal____________________________
A. References
(1)
AMM 71-11-02/201, Fan Cowl Panels
(2)
AMM 78-31-00/201, Thrust Reverser System
B.
Access
(1)
Location Zones
5 Left Nacelle
6 Right Nacelle
(2)
Access Panels
5737L/5746R Engine No. 1 - Fan Cowl Panels
5738L/5739R Engine No. 1 - Thrust Reverser Halves
5837L/5846R Engine No. 2 - Fan Cowl Panels
5838L/5839R Engine No. 2 - Thrust Reverser Halves
C.
Procedure (Fig. 401)
S 014-010-C00
(1) Open the fan cowl panels (AMM 71-11-02/201).
S 014-011-C00
WARNING: OBEY THE INSTRUCTIONS IN THIS PROCEDURE WHEN YOU OPEN THE
_______ THRUST REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO THE EQUIPMENT CAN OCCUR.
(2)
Open the thrust reversers (AMM 78-31-00/201).
S 024-002-C00
(3)
Remove the two thrust links from the thrust link assembly.
(a)
Remove the bolt, nut, and washers that attach each thrust link to the evener bar.
(b)
Remove the bolt, nut, and washers that attach each thrust link to the fan frame fitting.
S 024-003-C00
(4) Remove the thrust link assembly from the strut.
(a) Remove the five bolts and washers that attach the thrust fitting to the strut.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-21-02
ALL ú ú C01 Page 401 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A STRUT WEDGE SURFACE BOLT, NUT, (4 LOCATIONS) AND WASHER
(5 LOCATIONS) BARREL NUT
WASHER (5 LOCATIONS) VERTICAL DEFLECTORBOLT
(5 LOCATIONS)
WASHER
(2 LOCATIONS)
BOLT BOLT, NUT, SUPPORT BRACKET
BOLT (2 LOCATIONS) AND WASHER (2 LOCATIONS) (2 LOCATIONS)
(ASSEMBLED)
A
FAIL-SAFE FITTING BOLT
BOLT FITTING THRUST
1 (2 LOCATIONS)
1
WASHER WASHER (2 LOCATIONS)
COLLAR THRUST LINK (2 LOCATIONS)
WASHER
(2 LOCATIONS)
WASHER
NUT (2 LOCATIONS) WASHER (2 LOCATIONS)
NUT EVENER BAR NUT (2 LOCATIONS)
(DISASSEMBLED)
A
1
IT IS USUAL TO HAVE SOME AXIAL MOVEMENT OF
THE BOLTS CONNECTING THE EVENER BAR TO THE
THRUST LINK AND THE EVENER BAR TO THE THRUST
FITTING
Forward Engine Mount Thrust Link Assembly Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 動(dòng)力裝置 POWER PLANT 2(152)
