(d)
Attach a dynamometer to the inboard or outboard attach point on one arm, as it is necessary, as follows:
NOTE: On the aft bootstrap location, only one lever hoist
____ and one dynamometer are necessary. You must install the lever hoist and dynamometer on opposite arms.
1) Use the outboard hole for the outboard location. Use the inboard hole for the inboard location.
(e) Attach a lever hoist to the inboard or outboard attach point on the opposite arm. 1) Make sure you can see the dynamometer when you operate the
lever hoist.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
STRUT
SEEC D
SEEA B
FWD 1 RIGHT SIDE SKIRT FAIRING (REF)1. BOLT (AFT BOOTSTRAP ATTACH POINTS)
A
RIGHT ARM
BOLT WASHER (3 LOCATIONS)
SHACKLES OUTBOARD ATTACH POINT INBOARD ATTACH POINT
FWD DYNAMOMETER
SHACKLE
RIGHT SIDE (VIEW SHOWS AN OUTBOARD INSTALLATION)
1
REMOVE THE FASTENERS TO GET B ACCESS TO THE ATTACH POINTS. Aft Bootstrap Installation Figure 412 (Sheet 1)
C78266
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
LEFT SIDE
(VIEW SHOWS AN INBOARD INSTALLATION)
D
Aft Bootstrap Installation
Figure 412 (Sheet 2)
C78272
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A 737-300/400/500MAINTENANCE MANUAL
P/N 65C36577-3 (BACF3F015L010NN)
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CFM56 ENGINES
/ / ////////////////////////
MATERIAL: 2024-T3 OR T4 PER QQ-A-250/4 2024-T3 OR T4 CLAD PER QQ-A-250/5 7075-T6 PER QQ-A-250/12 7075-T6 CLAD PER QQ-A-250/13
P/N 65C36577-3
NOTE:____ AIRPLANES WITH SB 54-1032
Bootstrap Shim
Figure 412 (sheet 3)
H49802
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Power Plant Removal - Bootstrap Method
______________________________________ Install the Bootstrap Equipment
S 494-037-C00
CAUTION: BE CAREFUL WHEN YOU MOVE THE TRANSPORTATION BASE AND CRADLE
_______ ASSEMBLY BELOW THE POWER PLANT. DAMAGE TO EQUIPMENT CAN OCCUR IF THE TRANSPORTATION BASE AND CRADLE ASSEMBLY HIT THE ENGINE.
(5) Put the transportation base and cradle below the power plant.
NOTE: It can be necessary to raise the airplane to get
____ sufficient clearance between the transportation base and the thrust reverser. To get this clearance, extend the main and nose landing gear shock struts with dry air or nitrogen. (AMM 08-11-00/201).
When the bootstrap equipment is installed on the airplane, you must use all four persons to remove the engine.
(a) Put the cradle assembly/transportation base in front of the engine and move it rearward until the centerline of the forward cradle attach point is aligned horizontally with the centerline of the engine.
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