TM 1-1520-238-23
2-280
2.80.
LEFT FUSELAGE FOOTSTEP REMOVAL/INSTALLATION – continued
2.80.3. Removal
a. Remove left fuselage footstep (1) from two
footstep sockets (2).
(1) Hold two screws (3). Remove self-locking
nuts (4) and washers (5).
(2) Remove two screws (3) and washers (6) from
sockets (2) and footstep (1).
(3) Remove footstep (1) from two sockets (2).
2.80.4. Cleaning
a. Wipe removed and attaching parts and sur-
faces with a clean rag.
2.80.5. Inspection
a. Check footstep for wear, deformation, cracks,
corrosion, anti-skid coating, and bolt holes
elongation (para 2.11).
2.80.6. Installation
a. Install footstep (1) in sockets (2).
(1) Install footstep (1) in two sockets (2).
(2) Install two screws (3) through washers (6),
sockets (2), and footstep (1).
(3) Hold two screws (3). Install washers (5) and
nuts (4).
b. Inspect (QA).
END OF TASK
M04-1480-2
4
5
2
6
3
1
M04-1480-3
2
6
3
4
5
1
