ARMY TM 9-2815-259-24 AIR FORCE TO 38G1-125-2 MARINE CORPS 09249A/09246A-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