TM 1-1520-238-23
2-617
2.171.
PILOT/CPG ARMORED CREW SEAT FRAME ASSEMBLY ATTENUATOR
REMOVAL/INSTALLATION continued
2.171.3. Removal
a. Enter pilot and/or CPG station (para 1.56). Ob-
serve all safety precautions.
b. Remove attenuator (1) from frame assembly
(2).
(1) Remove shear bolt (3), self-locking nut (4),
and washer (5) from rod end clevis (6).
(2) Remove shear bolt (7), two washers (8), and
self-locking nut (9) from yoke assembly (10).
(3) Remove attenuator (1) from frame assembly
(2).
2.171.4. Cleaning
a. Wipe attenuator attachment area with clean
rag.
2.171.5. Inspection
a. Check attenuator attachment area for corro-
sion (para 1.49).
b. Check attenuator attachment area for cracks.
None allowed.
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