(3)
AMM 78-31-03/501, Thrust Reverser Hydraulic Actuators
(4) AMM 78-31-04/401, Rotary Flex Shafts ú (5) SRM 54-30-02/101, Fan Duct Cowl and Thrust Reverser Structure ú Allowable Damage
C. Access
(1)
Location Zones
506 Engine No. 1 - Thrust Reversers
606 Engine No. 2 - Thrust Reversers
(2)
Access Panels 5783L/5739L Fan Duct Cowl and Thrust Reverser - Engine No. 1 5738R/5739R Fan Duct Cowl and Thrust Reverser - Engine No. 2 5713L/5714L Upper Actuator Access Door - Engine No. 1 5813R/5814R Upper Actuator Access Door - Engine No. 2 5715L/5716L Middle Actuator Access Door - Engine No. 1 5815R/5816R Middle Actuator Access Door - Engine No. 2 5717L/5718L Lower Actuator Access Door - Engine No. 1 5817R/5818R Lower Actuator Access Door - Engine No. 2
D.
Procedure
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-00
ALL ú ú C01.1 Page 601 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
(8 LOCATIONS) "C" DUCT DRAINS
AFT UPPER COMPRESSION PADS
SEE H B COMPRESSION PAD FORWARD UPPER SEE
(INBOARD HALF ONLY) DOOR DEFLECTORS FLAP SEAL
SEE J
ISEE PADS (LEFT HALF ONLY) LOWER COMPRESSION Figure 601 (Sheet 1) Thrust Reverser System - Inspection/Check A FWD
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-00
ALL ú ú C01 Page 602 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE B
SEE F REVERSER WIRE BUNDLE
SEE G FEEDBACK CABLE
SEE C
FLEXIBLE HYDRAULIC LINES
MANUAL DRIVE SEE E
CONNECTOR REVERSER WIRE BUNDLE SYNC LOCK
UPPER FEEDBACK (LOCKING) CABLE ACTUATOR
SEE D
SEE C
FLEXIBLE
B2
HYDRAULIC
MANUAL
LINES
DRIVE ROTATING FLEX SHAFT
UPPER (LOCKING) ACTUATOR SEE E SEE D
MANUAL UNLOCK HANDLE
ROTATING FLEX SHAFT B1
1
AIRPLANES WITHOUT
THRUST REVERSER SYNC LOCKS.
2
AIRPLANES WITH THRUST
REVERSER SYNC LOCKS.
Thrust Reverser System - Inspection/Check
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-00
ALL ú ú C01 Page 603 ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
HYDRAULIC FLEXIBLE
CONNECTIONS HYDRAULIC
LINES
FAN COWL
SUPPORT BEAM
C
ACTUATOR (LOCKING) UPPER COUPLING NUT SHAFT TUBE ROATING FLEX
CONNECTIIONS HYDRAULIC PLUG
D
Figure 601 (Sheet 3) Thrust Reverser System - Inspection/Check
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-00
ALL ú ú C02 Page 604 ú Jul 15/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ACTUATOR SEE F
EXAMPLE EACH ACTUATOR ROD END
ACTUATOR
E
A
A
THRUST REVERSER
ACTUATOR PUSH-OFF SPRING
CASCADE AFT
SUPPORT RING
F GLAND NUT ROD STOP
THRUST REVERSER
ACTUATOR ROD END
0.007-0.033 INCH (0.18-0.84 mm) 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(45)
