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REPAIR  CONNECTING LINK  (DRAG STRUT)  AND  ENGINE  MOUNT  FITTINGS (AVIM) (Continued) - TM-55-1520-240-23-3_463
REPAIR  CONNECTING  LINK  (DRAG  STRUT)  AND  ENGINE  MOUNT  FITTINGS (AVIM) (Continued) - TM-55-1520-240-23-3_465

TM-55-1520-240-23-3 CH-47D Heilcopter Manual
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TM  55-1520-240-23-3 4-42 REPAIR  CONNECTING  LINK  (DRAG  STRUT)  AND  ENGINE  MOUNT  FITTINGS (AVIM) (Continued) 4-42 e. Drill  0.0927 to 0.0937  inch  round  hole  into new  bushing  (27)  to  within  approximately 0.010  inch of  inside  edge  of  bushing. NOTE Do  not allow lockpin  (29) to  protrude into  slot  of bushing  (27) after peening. f. Insert  new  lockpin  (29) and  peen  lug  (35) over  lockpin  at  90º  to  original  peen. 4-226







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