78-31-03
ALL ú ú C07 Page 409 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
D. Access
(1) Location Zones
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
502/602 Fan Cowl - Left
503/603 Fan Cowl - Right
101 Control Cabin - Left
102 Control Cabin - Right
E. Locking Actuator Buildup (Fig. 402)
S 864-036-C00
(1) If necessary, buildup a basic locking actuator into a left half (LH) locking actuator or into a right half (RH) locking actuator.
(a)
The differences between a LH locking actuator and a RH locking actuator are the leaf spring part numbers and the installed position of the fitting [190], the leaf spring, and the bellcrank assembly [125].
(b)
When you are finished with the buildup, the basic locking actuator part number will be changed to a new part number for either the left half (LH) or the right half (RH). 1) Basic locking actuator part number 315A1801-13 becomes:
315A1801-14 LH
315A1801-15 RH
2) Basic locking actuator part number 315A1801-17 becomes: 315A1801-18 LH 315A1801-19 RH
3) Basic locking actuator part number 315A1801-21 becomes: 315A1801-22 LH 315A1801-23 RH
4) Basic locking actuator part number 315A1801-25 becomes: 315A1801-26 LH 315A1801-27 RH
(c)
Install the rod [65] and the bushing [60] in the appropriate end of the bellcrank assembly [125].
(d)
Install the bolt [45A], washers [50], and collar [55].
(e)
Install the bushings [30, 40] in the clevis end of the actuator [195].
(f)
Position the flange of the bushing [40] inside the clevis, and position the flange of the bushing [30] outside the clevis.
(g)
Install the fitting [190] on the actuator [195] with the screws
[180] and washers [185].
(h)
Tighten the screws [180] to 27-33 pound inches.
NOTE: Do not install lockwire at this time.
____
(i) Temporarily install the bellcrank assembly [125] on the fitting
[190] with the bolt [105], washers [110], and bushing [120].
NOTE: Do not install the collar [115].
____
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-03
ALL ú ú C03 Page 410 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
REVERSER WIRE BUNDLE
FEEDBACK CABLE
FLEXIBLE HYDRAULIC LINES
MANUAL DRIVE
CONNECTOR REVERSER WIRE BUNDLE SYNC LOCK
UPPER FEEDBACK (LOCKING) CABLE ACTUATOR
SEE B
HYDRAULIC FLEXIBLE MANUAL A 2
LINES DRIVE
ROTATING
FLEX SHAFT
UPPER (LOCKING)
ACTUATOR
SEE B
MANUAL UNLOCK HANDLE
ROTATING FLEX SHAFT A1
1
AIRPLANES WITHOUT
THRUST REVERSER SYNC LOCKS.
2 AIRPLANES WITH THRUST REVERSER SYNC LOCKS.
Thrust Reverser Actuator Installation Figure 402 (Sheet 1)
E63777
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
78-31-03
ALL ú ú C01 Page 411 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
130
2 65A. ROD ASSEMBLY 100A, 101 125. BELLCRANK THRU
100A. ROD 2 ASSEMBLY 155
145. PLATE
101. BALL 45A. LOCKBOLT 145. PLATE 135. BUSHING
50. WASHER 150A. RIVET 130. BUSHING 101. BALL 60. BUSHING
115. COLLAR
135. BUSHING
110. WASHER 1
120. BUSHING 80. BEARING
85. NUT
140. BUSHING
90. WASHER
130. BUSHING
75. NUT 155. BELLCRANK
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(103)
