BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE F
ELECTRICAL CONNECTOR
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
F12237
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 406
(AIRPLANES PRE-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
BOLT
COUNTERSUNK
WASHER
ANTI-
ROTATION
WASHER
FORWARD HINGE FITTING
ANTI-ROTATION WASHER
HINGE CROSS ROD
PLAIN (2 LOCATIONS)
WASHER
A LOCKING
A-A
DEVICE
JAMNUT
REVERSER
STRUCTURE
A FWD
FORWARD HINGE FITTING
0.005-0.025 INCH CLEARANCE (0.13-0.64 mm)
C
PLAIN WASHER(S) ANTI-ROTATION WASHER
CENTER HINGE FITTING
ANTI-
HINGE COUNTERSUNK ROTATION
CROSS ROD WASHER WASHER
(2 LOCATIONS) B BOLT
LOCKING
DEVICE B-B
JAMNUT
REVERSER STRUCTURE
B FWD
CENTER HINGE FITTING
D
Thrust Reverser Installation Figure 402 (Sheet 3)
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 407
(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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 034-019-C02
CAUTION: DO NOT EXTEND THE FEEDBACK PUSH-PULL CABLES OF THE THRUST
_______ REVERSER WHILE THEY ARE DISCONNECTED FROM THE ACTUATOR. THIS CAN CAUSE THE RACK AND PINION IN THE CONTROL BOX OF THE STRUT DRUM TO BE OUT OF ADJUSTMENT.
(20) Disconnect the feedback cable from the upper locking actuator (View B, Fig. 402).
(a)
Loosen the jamnut and release the cable from the support
bracket.
(b)
Disconnect the cable end of the feedback cable from the
bellcrank of the locking actuator.
(c)
Secure the loose end of the cable away from the reverser.
3 O'CLOCK
9 O'CLOCK
SLIDER
C-C
AFT HALF
Figure 402 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2 WITH HINGE CROSS RODS ú C03 Page 408 (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 ////////////////////////
ELECTRICAL CONNECTOR
SUPPORT BEAM FAN COWL
SYNC LOCK WIRE BUNDLE
WIRE BUNDLE THRUST REVERSER
LINE HYDRAULIC FLEXIBLE CABLE FEEDBACK
F
Thrust Reverser Installation
Figure 402 (Sheet 5)
F12873
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
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