TM 1-1520-238-23
11-828
11.188.
LONGITUDINAL MAGNETIC BRAKE SPRING MECHANISM REMOVAL/INSTALLATION – continued
g. Remove -5 rig pin (25) from rig pin hole (26).
h. Inspect (QA).
i. Perform flight control system maintenance
operational check (TM 1-1520-238-T).
j. Install door (1).
(1) Aline holes in door (1) with holes in floor (2).
(2) Install 28 screws (3) and washers (4) on door
(1).
k. Install pilot seat (para 2.161).
END OF TASK
25
26
M04-4420-11
M04-4420-12
2
1
3
4
