TM 1-1520-238-232-266Change 32.76.MAIN LANDING GEAR LEFT SHOCK STRUT STRUCTURAL SUPPORTREMOVAL/INSTALLATION – continued(8) Remove shear bolt (26), self-locking nut (27),and washer (28) from support (5).(9) Remove angle (29) from support (5).(a) Remove two shear bolts (30), self-lockingnuts (31), and washers (32) from angle(29).(10) Remove three shear bolts (33), self-lockingnuts (34), and washers (35) from support (5).(11) Remove support (5) from airframe (2).2.76.4. Cleaninga. Wipe removed and attaching parts and sur-faces with a clean rag.2.76.5. Inspectiona. Check mounting surface, support, and anglefor corrosion (para 1.49).WARNINGIf support is cracked, replace attach-ing bolts.b. Check support and angle for bends and/orcracks (para 2.12).c. Check mounting surface for broken orstripped threads of nutplates(TM 1-1500-204-23).GO TO NEXT PAGEM04-3744-4A3335342526302932312728
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