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时间:2010-08-24 13:01来源:蓝天飞行翻译 作者:admin
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[13]:
(a) Put the upper side cover [7] and the lower side cover [11] in their position on the control
stand [13].
NOTE: The lower side cover [11] goes under the upper side cover [7].
(b) Install the screws [6] that attach the upper side cover [7] and lower side cover [11] to the
control stand [13].
(c) Install the pocket assembly [12] with the screws [10] on the lower side cover [11].
SUBTASK 27-51-08-410-006
(4) Install the stabilizer trim wheel [8] on the right side of the control stand [13]:
(a) Put the stabilizer trim wheel [8] on the shaft.
NOTE: Make sure the handle on the stabilizer trim wheel is 75 to 105 degrees from the
handle on the left stabilizer trim wheel.
(b) Install the bolt [9] to attach the stabilizer trim wheel [8].
SUBTASK 27-51-08-860-009
(5) Remove the safety tag and close this circuit breaker:
F/O Electrical System Panel, P6-3
Row Col Number Name
C 10 C00284 PANEL & INSTR ELEX PANEL
------------------------- END OF TASK ---------------------------
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AIRCRAFT MAINTENANCE MANUAL
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Flap Lever Position Switch Adjustment
Figure 501 (Sheet 1 of 5)/27-51-08-990-802
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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Flap Lever Position Switch Adjustment
Figure 501 (Sheet 2 of 5)/27-51-08-990-802
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EFFECTIVITY
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Flap Lever Position Switch Adjustment
Figure 501 (Sheet 3 of 5)/27-51-08-990-802
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Flap Lever Position Switch Adjustment
Figure 501 (Sheet 4 of 5)/27-51-08-990-802
737-600/700/800/900
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EFFECTIVITY
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Figure 501 (Sheet 5 of 5)/27-51-08-990-802
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INBOARD TRAILING EDGE FLAP - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the inboard trailing edge flap
(2) An installation of the inboard trailing edge flap.
B. This procedure includes the removal and installation of the inboard main flap with the aft flap. You
can remove and install the main flap with the aft flap either removed or installed. For procedures to
remove and install the aft flap only, refer to (TASK 27-51-12-000-801).
C. The inboard main flap and aft flap together weigh approximately 333 pounds (151 kilograms). The
main flap alone weighs approximately 300 pounds (136 kilograms).
TASK 27-51-11-000-801
2. Inboard Trailing Edge Flap Removal
A. 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)
27-51-00-980-801 Trailing Edge Flap System Manual Operation (P/B 201)
27-51-18-000-802 Inboard Flap Support Aft Fairing Removal (P/B 401)
B. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
SPL-1729 Sling - Equipment, Trailing Edge Flaps
(Part #: C27052-25, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
STD-1095 Crane - Lift, 2000 Lb Capacity, 30 Foot Height
C. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
D. Access Panels
Number Name/Location
194BL Flap Track Lubrication Panel - Aft
194BR Flap Track Lubrication Panel - Aft
194CL Aft Wing To Body Fairing Panel
194CR Aft Wing To Body Fairing Panel
 
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