TM 1-1520-238-23
4-15
4.2.
ENGINE INSPECTION continued
(4) Reinstall engine mounts (para 4.31).
(5) Reinstall support pin in aft lower engine mount (para 4.50 No. 1 engine or 4.54 No. 2 engine).
(6) Reinstall support pin in aft inboard engine mount (para 4.51 No. 1 engine or 4.55 No. 2 engine).
(7) Apply torque stripe per step p(2)(a).
(8) Monitor support pin and aft engine mount bushings for 10 flight hours to ensure bushing rotation has been
corrected. If bushings continue to rotate, replace bushings.
END OF TASK