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ARMY TM 9-2815-259-24 AIR FORCE TO 38G1-125-2 MARINE CORPS 09249A/09246A-24 4-76 (18)  Remove fuel supply pump push rod.  Label end for reassembly in same orientation.  Refer to Figure 4-50. FIGURE 4-50.  FUEL TRANSFER PUMP PUSH ROD LOCATION (19)  Cover all openings to prevent entry of foreign material. b.     Inspection. (1)     Measure and record valve recess (Figure 4-51) for all valves using a depth micrometer or magnetic base dial indicator.  Measurements must be made a maximum of 0.12 in. (3.0 mm) from edge of valve head. FIGURE 4-51.  VALVE RECESS MEASUREMENT


 


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