(b)
Remove the aft half of the slider with the eccentric pins attached.
S 954-015-C03
(16) Apply masking tape along the seal segments on the primary sleeve assembly.
S 414-016-C03
CAUTION: MAKE SURE THERE IS PROPER CLEARANCE BETWEEN THE THRUST REVERSER
_______ AND THE SEAL SEGMENTS OF THE PRIMARY SLEEVE ASSEMBLY WHEN YOU CLOSE THE THRUST REVERSER HALF. DAMAGE TO EQUIPMENT CAN OCCUR.
(17)
Close but do not latch the thrust reverser half (AMM 78-31-00/201).
S 034-017-C03
(18)
Disconnect the opening actuator of the thrust reverser from the upper attach fitting on the reverser (View B, Fig. 402).
S 434-018-C03
(19)
Secure the upper end of the opening actuator to the engine with string to make sure it is clear of the thrust reverser.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3 WITH CROSS BEAMS ú C01 Page 404 (AIRPLANES POST-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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
SEE A
COMPRESSION PADS AFT UPPER
SEE D SEE C
SEE E
(INBOARD HALF ONLY) DOOR DEFLECTORS FLAP SEAL
UPPER BIFURCATION
FORWARD UPPER COMPRESSION PAD
SEE B
LOWER BIFURCATION
LOWER COMPRESSION PADS (LEFT HALF ONLY)
A
Thrust Reverser Installation
Figure 402 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3
WITH CROSS BEAMS ú C02 Page 405
(AIRPLANES POST-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E69161
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ELECTRICAL CONNECTOR SEE F
WIRE BUNDLE THRUST REVERSER
BEAM SUPPORT FAN COWL SUPPORT BRACKET FEEDBACK CABLE FLEXIBLE LINES HYDRAULIC SYNC LOCK WIRE BUNDLE JAMNUT CABLE FEEDBACK
ACTUATOR UPPER (LOCKING)
MANUAL HANDLE UNLOCK
UPPER ATTACH FITTING OPENING ACTUATOR
B
Figure 402 (Sheet 2) Thrust Reverser Installation
F12876
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 3
WITH CROSS BEAMS ú C02 Page 406
(AIRPLANES POST-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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ////////////////////////
STRUT
AA AA
THRUST NAC STA 206.5 THRUST
REVERSER
REVERSER C
STRUT
BB BB
NAC STA 224.0
THRUST THRUST REVERSER REVERSER
D
SELF-LOCKING BOLTPLAIN
NUT THRUST
WASHER
COUNTERSUNK REVERSER
0.032 WASHER
GAP
0.005
0.16
0.16
MINIMUM
MINIMUM
0.12
STRUT0.12
MINIMUM
MINIMUM PLAIN 0.032
STRUT GAP
WASHER 0.005
COUNTERSUNK
WASHER
BOLT THRUST SELF-LOCKING REVERSER NUT
FWDFWD
B-BA-A
Thrust Reverser Installation Figure 402 (Sheet 3)
E69442
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
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(77)