(2)
The second task installs the aft fairing panel.
B. Aft Fairing Panel - Pylon Overwing Location
(1)
The aft fairing is found immediately aft of the nacelle fairing panel.
(2)
The aft fairing is aft of the wing leading edge, and is installed on top of the wing surface, but it is not part of the wing.
C. To remove the nacelle fairing panel refer to 54-32-01/401.
TASK 57-33-01-004-001-B00
2. Aft Fairing Panel Removal_________________________
A. Equipment
(1) Bit - PHILLIPS ACR Removal, size #3, SDM263R,
commercially available.
Snap-on Tools Corp., Kenosha, Wi 53140
B. References
(1)
27-61-00/201, Spoiler Control System
(2)
27-62-00/201, Speedbrake Control System
(3)
27-81-00/201, Leading Edge Slats
(4)
54-32-01/401, Forward Fairing Removal/Installation
C. Access
(1) Location Zones
500 Left Nacelle
600 Right Nacelle
D. Prepare for the Removal of the Aft Fairing Panel.
S 044-003-B00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE LEADING EDGE FLAPS AND
_______ SLATS (AMM 27-81-00/201) IF WORK WILL BE DONE NEAR THE WING LEADING EDGE. ACCIDENTAL OPERATION OF THE LEADING EDGE FLAPS AND SLATS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do the deactivation procedure for the leading edge slats and flaps (AMM 27-81-00/201).
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57-33-01
ALL ú ú B01 Page 401 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AFT FAIRING -
AND TORQUE VALUES
Aft Fairing - Pylon Overwing Installation Figure 401 (Sheet 1)
A60196
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57-33-01
ALL ú ú B01 Page 402 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
AFT
NACELLE FAIRING
FAIRING PANEL (REF) PANEL
AND THE MATING FAIRING PANEL.
Aft Fairing - Pylon Overwing Installation Figure 401 (Sheet 2)
A60197
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57-33-01
ALL ú ú B01 Page 403 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 044-013-B00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE SPEED BRAKE CONTROL
_______ SYSTEM (AMM 27-62-00/201) IF WORK WILL BE DONE NEAR THE GROUND SPOILERS (SPOILERS 0, 1, 4, 5, 8 AND 9). ACCIDENTAL OPERATION OF THE GROUND SPOILERS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Do the deactivation of the speed brake control (Ref 27-62-00/201).
S 044-014-B00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE SPOILER CONTROL SYSTEM
_______ (AMM 27-61-00/201) IF WORK WILL BE DONE NEAR THE FLIGHT SPOILERS (SPOILERS 2, 3, 6, AND 7). ACCIDENTAL OPERATION OF THE FLIGHT SPOILERS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3) Do the deactivation of the spoiler (Ref 27-61-00/201).
E. Procedure
S 024-004-B00
(1) Do these steps to remove the aft fairing panel (Figure 401):
(a)
Remove the bolts that attach the aft fairing panel to the wing.
(b)
Measure the bolt diameter.
(c)
Make a record of the bolt diameter.
(d)
Remove the fairing from the wing.
TASK 57-33-01-404-006-B00
3. Aft Fairing Panel Installation______________________________
A. Equipment
(1)
Bit - PHILLIPS ACR Installer, size #3, SDM263I,
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