Quantcast FIGURE 4-53  FLYWHEEL FLATNESS

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ARMY TM 9-2815-260-24 AIR FORCE TO 38G1-126-2 MARINE CORPS TM 09244A/09245A-24 4-82 FIGURE 4-53  FLYWHEEL FLATNESS Table 4-6.  Flywheel Face Flatness Specifications Item Specification Maximum variation 0.009 in. (0.23 mm) Maximum variation per 1.0 in. (25 mm) of travel 0.0005 in. (0.013 mm) b.    Removal. __________ WARNING Flywheel is heavy.  Provide adequate lifting device to support weight.   Failure to comply could result in serious personal injury. (1) Remove bolts (Figure 4-54). FIGURE 4-54.  FLYWHEEL REMOVAL


 


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