SUBTASK 53-12-12-010-005
(6) If necessary, remove the hydraulic fuses and other equipment for access to the aft links in the
MLG wheel well.
E. Forward Link Removal
SUBTASK 53-12-12-020-001
(1) From the passenger compartment, remove the bolt [2], bolt [3], washers [4], bushing [5],
bushing [6], washers [7] and nuts [8] that attach the link [1] to the fitting [14] and fitting [15].
(a) Remove the link [1].
F. Aft Link Removal
SUBTASK 53-12-12-020-002
(1) From the MLG wheel well, remove the bolt [2], bolt [3], washers [4], bushing [5], bushing [6],
washers [7] and nuts [8] that attach the link [1] to the fitting [13] and stringer [17].
(a) Remove the link [1].
1) If necessary, do the next step.
SUBTASK 53-12-12-020-003
(2) If necessary, remove the bolts [9], bolts [10], bolts [11] and collars [12] that attach the
fitting [13] to the spar frame [16], fitting [14] and fitting [15] (SRM 51-40-02-0G-0).
NOTE: Make a record of the fastener positions for installation.
(a) Remove the fitting [13].
(b) Remove the link [1].
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-12-12
Page 402
D633A101-ILF Oct 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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