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clearance.
3) Tighten the bolts [23].
4) Install lockwire on bolts [23].
(b) If the mismatch is not in the limit on the bottom of the forward fairing assembly [3], change
the thickness of the shims [25].
1) Apply primer, C00259 to the mating surfaces of the shim [25] and the fairing attach
fitting [24].
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SUBTASK 27-51-28-820-010
(5) If the seals [26] are not compressed evenly against the lower surface of the main flap [2], then
adjust the position of the seals [26]:
(a) Loosen the nuts [27] on the retainer [28].
(b) Move the seal [26] and the retainer [28].
(c) Tighten the nuts [27] that hold the retainer [28].
SUBTASK 27-51-28-420-007
(6) If you removed the forward fairing assembly [3], do this task: Outboard Flap Outboard Support
Forward Fairing Installation, TASK 27-51-28-400-801.
J. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-28-440-005
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
------------------------- END OF TASK ---------------------------
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Outboard Flap Outboard Support Fairing Adjustment
Figure 501 (Sheet 1 of 4)/27-51-28-990-803
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Outboard Flap Outboard Support Fairing Adjustment
Figure 501 (Sheet 2 of 4)/27-51-28-990-803
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Outboard Flap Outboard Support Fairing Adjustment
Figure 501 (Sheet 3 of 4)/27-51-28-990-803
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Outboard Flap Outboard Support Fairing Adjustment
Figure 501 (Sheet 4 of 4)/27-51-28-990-803
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TASK 27-51-28-820-802
3. Outboard Flap Inboard Support Fairing Adjustment
(Figure 502)
A. General
(1) This task is applicable to the fairings at flap supports No. 2 and 7.
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-440-801 Trailing Edge Flap System Reactivation (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-28-000-803 Outboard Flap Inboard Support Forward Fairing Removal (P/B 401)
27-51-28-400-803 Outboard Flap Inboard Support Forward Fairing Installation (P/B 401)
C. Consumable Materials
Reference Description Specification
C00259 Primer - Chemical And Solvent Resistant Finish,
Epoxy Resin
BMS10-11,
Type I
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
43 Fairing assembly 27-51-28-04-020 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-04-025 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-05-005 GUN 001-019, 101-110,
155-157, 201-999
44 Fairing assembly 27-51-28-04-210 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-04-215 GUN 001-028, 101-121,
155-157, 201-999
27-51-28-06-005 GUN 001-019, 101-110,
155-157, 201-999
E. Location Zones
Zone Area
543 Left Wing - Fairing Flap Support No. 2
643 Right Wing - Fairing Flap Support No. 7
F. Access Panels
Number Name/Location
543DR Flap Support No. 2 Access Door
643DL Flap Support No. 7, Access Door
G. Prepare for the Adjustment
SUBTASK 27-51-28-860-006
(1) If the trailing edge flaps are not in the retracted position, do this task: Retract the Trailing Edge
Flaps, TASK 27-51-00-860-804.
SUBTASK 27-51-28-040-006
(2) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(41)
