10) Remove the fasteners for access panel [13]:
Number Name/Location
191FR Forward Wing To Body Fairing Panel - Mid Fairing, Above Ram Air
Inlet
11) Remove the fasteners for access panel [8]:
Number Name/Location
191GL Ram Air Actuator Panel - Forward
12) Remove the fasteners for access panel [14]:
Number Name/Location
191GR Ram Air Actuator Panel - Forward
13) Remove the fasteners for access panel [10]:
Number Name/Location
191HL Ram Air Inlet Lip Panel - Forward
14) Remove the fasteners for access panel [11]:
Number Name/Location
191HR Ram Air Inlet Lip Panel - Forward
(b) Remove the fairing panel from the airplane.
END OF TASK
TASK 53-51-21-400-803
3. Forward Wing-To-Body Fairing Panel Installation
(Figure 401)
A. General
(1) This task includes the steps to install access panels:
B. References
Reference Title
21-51 PACK FLOW CONTROL AND PACK COOLING SYSTEM
33-44 ANTI-COLLISION LIGHTS
51-00-59 STANDARD PREVENTIVE MAINTENANCE PROCEDURES
51-51-00-340-805 Bonded Teflon Rub Pad Repair (P/B 801)
53-51-21-211-801 Wing-To-Body Fairing Panel Designated Electrical Bond Visual
Inspection (P/B 601)
53-51-21-760-801 Wing-To-Body Fairing Panel Maximum Electrical Resistance
Check (P/B 601)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental -
Chromate Type
BMS5-95
A02315 Sealant - Low Density, Synthetic Rubber. 2
Part
BMS5-142 Type II
C00175 Primer - Urethane Compatible, Corrosion
Resistant
BMS10-79 Type III
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-51-21
Page 403
D633A101-ILF Oct 15/2018
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
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