(Continued)
Reference Description Specification
C00259 Coating - Chemical And Solvent Resistant
Finish, Corrosion Inhibiting Primer
BMS10-11 Type I
C00308 Compound - Corrosion Preventive, Petrolatum
Hot Application
MIL-C-11796
C00528 Compound - Corrosion Preventive, Petroleum
Hot Application (Soft Film)
MIL-C-11796 Class III
G00009 Compound - Organic Corrosion Inhibiting BMS3-23
D. Location Zones
Zone Area
191 Lower Wing-To-Body Fairing - Forward of Wing Box
E. Access Panels
Number Name/Location
191AL Forward Wing To Body Fairing Panel - Upper
191AR Forward Wing To Body Fairing Panel - Upper
191BL Forward Wing To Body Fairing Panel, Ram Air Inlet
191BR Forward Wing To Body Fairing Panel, Ram Air Inlet
191CL Forward Wing To Body Fairing Panel - Middle
191CR Forward Wing To Body Fairing Panel - Middle
191D Forward Wing To Body Fairing Panel - Lower
191E Low Pressure ECS Panel - Forward
191FL Forward Wing To Body Fairing Panel - Mid Fairing, Above Ram Air Inlet
191FR Forward Wing To Body Fairing Panel - Mid Fairing, Above Ram Air Inlet
191GL Ram Air Actuator Panel - Forward
191GR Ram Air Actuator Panel - Forward
191HL Ram Air Inlet Lip Panel - Forward
191HR Ram Air Inlet Lip Panel - Forward
F. Prepare for Forward Wing-To-Body Fairing Panel Installation Procedure
SUBTASK 53-51-21-210-006
(1) Make sure that the mating surfaces between the panel and the structure are free from
contamination.
NOTE: Teflon is applied in the mating surface. The teflon is not contamination. It is not
necessary to remove the teflon.
SUBTASK 53-51-21-160-003
(2) Make sure that the teflon mating surface is in good condition.
(a) If necessary, repair the teflon substrip. Refer to this task: Bonded Teflon Rub Pad Repair,
TASK 51-51-00-340-805.
SUBTASK 53-51-21-210-005
(3) Make sure that the designated electrical bonds for the panel are identified.
(a) Refer to this task: Wing-To-Body Fairing Panel Designated Electrical Bond Visual
Inspection, TASK 53-51-21-211-801.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-51-21
Page 404
D633A101-ILF Oct 15/2015
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL
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