A 737-300/400/500MAINTENANCE MANUAL
3/16 INCH (4.76 mm)
DIA BOLTS
(18 LOCATIONS)
5
(16 LOCATIONS)
6
1/4 INCH (6.35 mm) DIA BOLTS (2 LOCATIONS)
6
FWD
AFT PANEL OF THE AFT FAIRING
D
3/16 INCH (4.76 mm)
DIA BOLTS
5
(31 LOCATIONS)
(29 LOCATIONS) 6
1/4 INCH (6.35 mm) DIA BOLTS
6
FWDFLAP TRACK FAIRING - LEFT SIDE
E 3/16 INCH (4.76 mm)
DIA BOLTS 5
(28 LOCATIONS) (26 LOCATIONS) 6
1/4 INCH
(6.35 mm) DIA BOLTS
FWD 6
FLAP TRACK FAIRING - RIGHT SIDE
NOTE: LEFT SIDE SHOWN. RIGHT SIDE EQUIVALENT UNLESS SPECIFIED
5 ORIGINAL CONFIGURATION E ____
6 ALTERNATE CONFIGURATION DIFFERENTLY.
Aft Fairings
Figure 401 (Sheet 3)
A13579
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 044-007-B00
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE WHEN YOU DO THE
_______ DEACTIVATION PROCEDURE FOR THE LEADING EDGE SLATS. IF YOU DO NOT OBEY THESE INSTRUCTIONS, INJURIES TO PERSONS CAN OCCUR.
(4)
Do the deactivation procedure for the leading edge slats (AMM 27-81-00/201).
S 024-008-B00
(5)
Do these steps to remove the aft fairings (Fig. 401):
(a)
Remove the bolts that attach the fairings to the strut.
(b)
Remove the fairings.
TASK 54-32-02-404-002-B00
3. Aft Fairings Installation
_________________________
A. General
(1) These fairings are found below the wing.
B. Equipment
(1) Torque Control Tool -"HERBIE", P/N VST 15-50,
Commercially available
(Voi-Shan, Culver City CA 90230) or similar
C. Consumable Materials
(1)
A00247 Sealant-Pressure and environmental-Chromate type, BMS 5-95
(2)
G00315 Compound-Fiberglass Resin, BMS 8-201, Type II
D. References
(1)
AMM 27-81-00/201, Leading Edge Slats
(2)
AMM 54-10-00/501, Nacelle Strut
(3)
AMM 78-31-00/201, Thrust Reverser System
E. Access
(1) Location Zones
507 Nacelle Strut - Aft Section
607 Nacelle Strut - Aft Section
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A
737-300/400/500MAINTENANCE MANUAL
(2) Access Panels
5742L/5842R Aft Fairing - Forward Panel
5743L/5843R Aft Fairing - Center Panel
5744L/5844R Aft Fairing - Aft Panel
F. Install the Aft Fairings
S 944-006-B00
CAUTION: MAKE SURE THE STRUT COMPARTMENTS ARE FREE OF TOOLS, LOOSE
_______ MATERIALS, AND CONTAMINATION. DAMAGE TO THE STRUT COULD OCCUR.
(1)
Before you install the access panel, remove, all tools, loose material, and contamination from the strut compartment.
S 424-003-B00
(2)
Do these steps to install the aft fairings:
(a)
Make sure the mating faces of the fairings are clean.
(b)
ON ALL THE FAIRINGS EXCEPT THE REAR PANEL OF THE AFT FAIRING AND THE FORWARD PIN ACCESS PANEL, if not already done, apply the fiberglass resin compound to all the edges of the fairing.
NOTE: It is not necessary to apply the fiberglass resin
____ compound to the rear aft fairing and the access panel for the forward pin.
1) If the fairing is new, it can be necessary to use a small sander to put a small bevel on the inside edge.
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