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A. 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)
27-51-00-860-803 Extend the Trailing Edge Flaps (P/B 201)
27-51-00-860-804 Retract the Trailing Edge Flaps (P/B 201)
27-51-00-980-801 Trailing Edge Flap System Manual Operation (P/B 201)
27-51-11-820-801 Inboard Trailing Edge Flap Adjustment (P/B 501)
27-51-18-400-802 Inboard Flap Support Aft Fairing Installation (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-1679 Adapter - Drive, Flap Torque Tube Spline
(Part #: F70300-1, Supplier: 81205, A/P Effectivity: 737-100, -200,
-200C, -300, -400, -500, -600, -700, -700C, -700ER, -700QC, -800, -900,
-900ER, -BBJ)
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. Consumable Materials
Reference Description Specification
C00528 Compound - Corrosion Preventive, Petroleum Hot
Application (Soft Film)
MIL-C-11796,
Class III
C00913 Compound - Nondrying Resin Mix Corrosion
Inhibiting Material
BMS3-27
D00633 Grease - Aircraft General Purpose BMS3-33
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Flap assembly 27-51-11-01-005 GUN 001-020, 101-110,
115, 155-157, 201-999
27-51-11-01-010 GUN 001-020, 101-113,
115, 116, 118, 155-157,
201-999
27-51-11-01-015 GUN 001-020, 101-113,
115, 116, 118, 155-157,
201-999
27-51-14-02-065 GUN 001-020, 101-113,
115, 116, 118, 155-157,
201-999
57-52-00-06-035 GUN 101-108, 155-157,
204-999
57-52-00-06-040 GUN 101-108, 155-157,
204-999
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 412
Jun 10/2007
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
AMM Item Description AIPC Reference AIPC Effectivity
15 Bushing assembly 27-51-13-01-060 GUN 155
24 Pin 27-51-14-01-030 GUN 001-028, 101-121,
155-157, 201-999
26 Bushing assembly 27-51-13-01-070 GUN 155
106 Pin 57-42-51-02-155 GUN 001-028, 101-121,
155-157, 201-999
119 Pin 27-51-13-02-380 GUN 001-014, 101-108,
155-157, 201-999
27-51-13-02-470 GUN 001-014, 101-108,
155-157, 201-999
126 Pin 27-51-13-02-150 GUN 001-014, 101-108,
155-157, 201-999
27-51-13-02-380 GUN 001-014, 101-108,
155-157, 201-999
E. Location Zones
Zone Area
553 Left Wing - Inboard Flap
653 Right Wing - Inboard Flap
F. 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
G. Prepare for the Installation
SUBTASK 27-51-11-820-001
(1) Make sure the carriage roller cartridges are in the correct position (Figure 403):
NOTE: If you will install a different inboard flap assembly [1] than the one you removed, make
sure the carriage roller cartridges are in the same position as the flap you removed.
NOTE: If you did not record the position of the carriage roller from the flap you removed, then
adjust the carriage roller cartridges to the nominal position. The nominal position for
the carriage roller cartridges is -45 degrees for the left wing, and +30 for the right
wing.
NOTE: There is no mismatch or alignment dimension to the fixed structure or the outboard flap
that the flap is adjusted to meet. The carriage roller cartridges can be changed from the
nominal position to meet lateral trim tolerances.
NOTE: Make sure the carriage roller cartridge [116] and cartridge [125] for the inboard flap
assembly [1] are in the same position.
(a) If it is necessary, adjust the cartridges [125] on the inboard carriage [52]:
1) Loosen the nut [127] on the roller [123].
2) Turn the eccentric bushing [115] until the index mark [120] is in the correct position.
3) Tighten the nut [127] to 160-975 pound-inches (18.1-110.1 newton-meters).
4) Install the pin [126] in the nut [127].
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-51-11
Page 413
Jun 10/2007
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737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册4(86)
