TM 1-1520-238-23
Change 6
5-79
5.14A
MAIN ROTOR BLADE FORWARD AND AFT TIP WEIGHT REMOVAL/INSTALLATION
(AVIM) continued
e. Inspect (QA).
f. Install leading edge tip assembly (para 5.13).
g. Perform main rotor blade track and balance maintenance operational check (TM 1-1520-238-T).
END OF TASK