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[91]:
(a) Apply primer, C00259 to the mating surfaces of the shim [88].
(b) Put the fairing attach fitting assembly [95] and shim [88] in their location on the
transmission attach fitting [91].
(c) Apply compound, C00528 to the holes for the bolts [89].
(d) Install the bolts [89] and washers [90] to attach the fairing attach fitting assembly [95].
(e) Install lockwire between the bolts [89] and the fairing attach fitting assembly [95].
SUBTASK 27-51-28-420-005
(2) Install the forward fairing assembly [81]:
(a) Connect the jumper wires [103]:
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1) Lift the forward fairing assembly [81] until you can put the jumper wires [103] on the
studs.
2) Install the washers [93] and nuts [92] to attach the jumper wires [103].
3) Apply sealant, A02315 to the nuts [92].
(b) Apply primer, C00259 to the mating surfaces of the shims [96] and shim [104].
(c) If you removed the shims [96] or shim [104], put the shims [96] or shim [104] in its position.
(d) Apply compound, C00528 to the holes for the bolts [84] and bolts [86].
(e) Install the bolts [84] and washers [85] to attach the forward fairing assembly [81] to the
fairing attach fitting assembly [95].
(f) Install the bolts [86] to attach the forward end of the forward fairing assembly [81].
SUBTASK 27-51-28-820-003
(3) Do this task: Outboard Flap Inboard Support Fairing Adjustment, TASK 27-51-28-820-802.
NOTE: The aft fairing assembly [82] must be installed and adjusted before you can do the
adjustment of the forward fairing assembly [81].
SUBTASK 27-51-28-390-002
(4) Fill the clearance between the front of the forward fairing assembly [81] and the lower surface of
the wing with sealant, A02315.
G. Put the Airplane Back to Its Usual Condition
SUBTASK 27-51-28-440-003
(1) Do this task: Trailing Edge Flap System Reactivation, TASK 27-51-00-440-801.
------------------------- END OF TASK ---------------------------
TASK 27-51-28-000-804
8. Outboard Flap Inboard Support Aft Fairing Removal
(Figure 402)
A. General
(1) This task is applicable to the aft fairing at flap supports No. 2 and 7.
B. References
Reference Title
27-51-00-040-801 Trailing Edge Flap System Deactivation (P/B 201)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
C. Location Zones
Zone Area
543 Left Wing - Fairing Flap Support No. 2
643 Right Wing - Fairing Flap Support No. 7
D. Access Panels
Number Name/Location
543CL Flap Support No. 2 Access Cover
543CR Flap Support No. 2 Access Cover
543DR Flap Support No. 2 Access Door
643CL Flap Support No. 7, Access Cover
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(Continued)
Number Name/Location
643CR Flap Support No. 7, Access Cover
643DL Flap Support No. 7, Access Door
E. Procedure
SUBTASK 27-51-28-860-003
(1) Extend the trailing edge flaps to the 40-unit position. To extend them, do this task: Extend the
Trailing Edge Flaps, TASK 27-51-00-860-803.
NOTE: If you cannot extend the flaps, it will be necessary to open the access door [113] on the
aft fairing assembly [82].
SUBTASK 27-51-28-010-004
(2) If it is necessary, open the access door [113] on the aft fairing assembly [82]:
(a) These are the doors:
Number Name/Location
543DR Flap Support No. 2 Access Door
643DL Flap Support No. 7, Access Door
(b) Remove the bolts [145] that attach the access door [113] to the aft fairing assembly [82].
(c) Loosen the screw [146] on the access door [113].
NOTE: The screw [146] has a cotter pin installed on the inboard side.
(d) Turn the access door [113] around the screw [146].
SUBTASK 27-51-28-040-004
(3) Do this task: Trailing Edge Flap System Deactivation, TASK 27-51-00-040-801.
SUBTASK 27-51-28-010-005
(4) Remove the access cover [83] and access cover [102] from the forward end of the aft fairing
assembly [82]:
(a) These are the covers:
Number Name/Location
543CL Flap Support No. 2 Access Cover
543CR Flap Support No. 2 Access Cover
643CL Flap Support No. 7, Access Cover
643CR Flap Support No. 7, Access Cover
(b) Remove the bolts [94] that attach the access cover [83] and access cover [102] to the aft
fairing assembly [82].
(c) Remove the access cover [83] and access cover [102].
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737-600-700-800-900 飞机维护手册5 AIRCRAFT MAINTENANCE MANUA(35)
