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Boeing 737-600 - Subtask 53-51-21-390-001; Subtask 53-51-21-390-002; Subtask 53-51-21-390-003; Subtask 53-51-21-400-001

Boeing 737-600
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SUBTASK 53-51-21-390-001
CAUTION
DO NOT APPLY CORROSION-PREVENTATIVE COMPOUND TO THE BOND-
BOLTS AND THEIR HOLES. THE COMPOUND PREVENTS CORRECT
INSTALLATION OF THE BONDING BOLT. IF YOU DO NOT INSTALL THE
BONDING BOLT CORRECTLY, DAMAGE TO THE AIRPLANE CAN OCCUR.
(4) Apply the corrosion preventive compound, C00308, to the flanges on the fairing which touches
the structure.
SUBTASK 53-51-21-390-002
CAUTION
DO NOT APPLY SEALANT BETWEEN THE FAIRING PANELS THAT DO NOT
TOUCH THE FUSELAGE SKIN. IF YOU APPLY SEALANT INCORRECTLY, IT
CAN CAUSE STRUCTURAL DAMAGE TO THE FAIRING PANELS.
(5) Apply sealant, A00247 to the flanges on the fairing which touches the body skin.
SUBTASK 53-51-21-390-003
(6) Apply the corrosion inhibiting compound, G00009, to the area on the structure and the body
skin which touches the fairing.
(a) If necessary, refer to the STANDARD PREVENTIVE MAINTENANCE PROCEDURES,
SUBJECT 51-00-59.
G. Aft Wing-To-Body Fairing Panels Installation Procedure
SUBTASK 53-51-21-400-001
(1) Install the fasteners that do not have a designated electrical bond on the applicable panel.
CAUTION
DO NOT APPLY CORROSION-PREVENTATIVE COMPOUND TO THE
BOND-BOLTS AND THEIR HOLES. THE COMPOUND PREVENTS
CORRECT INSTALLATION OF THE BONDING BOLT. IF YOU DO NOT
INSTALL THE BONDING BOLT CORRECTLY, DAMAGE TO THE
AIRPLANE CAN OCCUR.
(a) Apply primer, C00259 to the hole of all non-designated electrical bond fasteners in the
structure as necessary.
(b) Let the primer to dry.
(c) Put the panel into its position.
1) Install the non-designated electrical bond fasteners for this access panel [57]:
Number Name/Location
194AL Aft Wing To Body Fairing Panel
2) Install the non-designated electrical bond fasteners for this access panel [50]:
Number Name/Location
194AR Aft Wing To Body Fairing Panel
3) Install the non-designated electrical bond access fasteners for this panel [56]:
Number Name/Location
194BL Flap Track Lubrication Panel - Aft
4) Install the non-designated electrical bond fasteners for this access panel [51]:
Number Name/Location
194BR Flap Track Lubrication Panel - Aft
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
53-51-21
Page 425
D633A101-ILF Feb 15/2019
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ILF ALL

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