TM 1-1520-238-23
Change 5
5-75
5.13.
MAIN ROTOR BLADE LEADING EDGE TIP REPLACEMENT continued
(6) Coat 21 screws (3) and 2 screws (4) with
antiseize
compound.
Use
antiseize
compound (item 26, App F).
(7) Install 21 screws (3) and 2 screws (4), wet, on
edge tip (1) lower surface. Use hi-torque
screwdriver.
(8) Torque screws (3) and screws (4) to 45 INCH-
POUNDS. Use hi-torque screwdriver and
torque wrench.
(9) Fill and flair any gaps 0.015 INCH or larger.
Use adhesive (item 1, App F).
(10) Allow adhesive to cure at room temperature
for 24 HOURS minimum.
b. Inspect (QA).
c. Perform main rotor blade track and balance
maintenance
operational
check
(TM 1-1520-238-T).
END OF TASK
M04-207-6A
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