5) Apply corrosion inhibiting compound to all exposed wheel well structure. Special
effort should be made to apply corrosion inhibitor along doubler edges, along faying
surfaces and on fastener heads. The use of spray equipment with nozzle directed
into faying surface is recommended.
6) Apply water displacing corrosion inhibiting compound to the frames at BS 685 and
706, WL 193 to 208.
7) Regrease all grease fittings in the treatment area.
8) In cases where the wheel well is cleaned with steam or high pressure water and
detergent, reapplication of corrosion inhibiting compound is recommended.
SUBTASK 53-11-37-610-031
(5) Frequency of Application
(a) Periodic inspection is required to areas identified as susceptible to corrosion and should
be consistent to the schedules specified in the Maintenance Planning Document.
Operators must be aware of reported problems and areas of occurrences.
(b) Periodic application of corrosion inhibiting compound, G00009 is necessary to areas
identified and should be consistent to the schedule specified in the Maintenance Planning
Document.
END OF TASK
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-11-37
Page 222
D633A101-ILF Oct 15/2014
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
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