Boeing 737-600 - Task 53-51-21-400-801 - Aft Wing-To-Body Fairing Panel Installation

12) Remove the fasteners for access panel [59]:
Number Name/Location
194GL Aft Wing To Body Fairing Panel
13) Remove the fasteners for access panel [63]:
Number Name/Location
194GR Aft Wing To Body Fairing Panel
14) Remove the fasteners for access panel [60]:
Number Name/Location
194HL Aft Wing To Body Fairing Panel
15) Remove the fasteners for access panel [61]:
Number Name/Location
194HR Aft Wing To Body Fairing Panel
(b) Remove the fairing panel from the airplane.
END OF TASK
TASK 53-51-21-400-801
7. Aft Wing-To-Body Fairing Panel Installation
(Figure 403)
A. General
(1) This task includes the steps to install access panels:
B. References
Reference Title
27-51-00-820-801 Trailing Edge Flap Control System Adjustment and Test
(P/B 501)
28-25-07-420-801 APU Fuel Feed Line Shroud Drain Mast Installation (P/B 401)
34-32-11-400-801 Marker Beacon Antenna Installation (P/B 401)
34-32-11-400-802 Marker Beacon Antenna with Gasket - Installation (P/B 401)
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
C00259 Coating - Chemical And Solvent Resistant
Finish, Corrosion Inhibiting Primer
BMS10-11 Type I
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-51-21
Page 423
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL