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Page Title: SELF–RETAINING BOLT FIT CHECK – continued
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SECTION  I.    FLIGHT CONTROLS MAINTENANCE – GENERAL
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TM-1-1520-238-23-7-1 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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FLIGHT CONTROL SYSTEM PUSH-PULL ROD ADJUSTABLE ROD END BEARING ASSEMBLY REPLACEMENT/ADJUSTMENT

TM 1-1520-238-23 11-16 Change 2 11.1. SELF–RETAINING BOLT FIT CHECK – continued c.   Check for proper retention. (1)   If bolt (1) can be pulled out of assembly with- out any restraining force, bolt (1) and assem- bly should be checked for proper size. d.   Check gap under head of bolt (1). (1)   Pull on bolt (1) until retaining ring (2) inside edge is flush with surface (3). (2)   Measure  gap  between  head  of  bolt  (1)  and surface (4). Use thickness gage. (3)   If gap A is 0.032 INCH or more, add AN960 washer under head of bolt (1). (4)   Maximum thickness of washer combination to be added is 0.128 INCH (two washers 0.063 INCH  thick)  or  a  combination  of  one  thick washer and a 0.032 INCH thick washer for a lesser gap). e.   Check that retaining ring (2) clears surface (3) completely. (1)   Remove one washer and replace with thinner washer if retaining ring (2) does not clear sur- face (3). END OF TASK M04-2386-3 1 M04-2386-4 1 4 2 3 A IF 0.032 OR GREATER ADD WASHER

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