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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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