ARMY TM 9-2815-260-24
AIR FORCE TO 38G1-126-2
MARINE CORPS TM 09244A/09245A-24
FIGURE 4-53 FLYWHEEL FLATNESS
Table 4-6. Flywheel Face Flatness Specifications
0.009 in. (0.23 mm)
Maximum variation per 1.0 in. (25 mm) of
0.0005 in. (0.013 mm)
Flywheel is heavy. Provide adequate lifting device to support weight.
Failure to comply could result in serious personal injury.
Remove bolts (Figure 4-54).
FIGURE 4-54. FLYWHEEL REMOVAL
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