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AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
Page 409
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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Leading Edge Flap Installation
Figure 401 (Sheet 7 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Leading Edge Flap Installation
Figure 401 (Sheet 8 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
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Feb 10/2006
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Leading Edge Flap Installation
Figure 401 (Sheet 9 of 10)/27-81-11-990-801
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-11
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Feb 10/2006
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Leading Edge Flap Installation
Figure 401 (Sheet 10 of 10)/27-81-11-990-801
737-600/700/800/900
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EFFECTIVITY
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TASK 27-81-11-400-801
3. Leading Edge Flap Installation
(Figure 401)
A. References
Reference Title
27-81-00-080-801 Leading Edge Flap and Slat Locks Removal (P/B 201)
27-81-11-200-801 Leading Edge Flap Inspection (P/B 601)
29-11-00-860-801 Hydraulic System A or B Pressurization (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
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
COM-1691 Protractor - Digital, Vertical or Horizontal
(Part #: KS5549, Supplier: 75245, A/P Effectivity: 737-ALL)
SPL-1734 Lockout Set - Leading Edge Slats and Krueger Flaps Actuators
(Part #: C27051-29, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
(Opt Part #: C27051-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -BBJ)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
D00633 Grease - Aircraft General Purpose BMS3-33
G01912 Lockwire - Monel (0.032 In. Dia.) NASM20995N~
C32
(QQ-N-281)
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
1 Leading edge flap 27-81-11-02-005 GUN 001-019, 101-110,
155-157, 201-999
2 Leading edge flap 27-81-11-01-005 GUN 001-028, 101-121,
155-157, 201-999
6 Pin 27-62-94-01-125 GUN ALL
15 Pin 27-62-94-01-125 GUN ALL
21 Pin 27-81-31-05-010 GUN 001-028, 101-121,
155-157, 201-999
34 Pin 27-41-71-01-035 GUN 001-028, 101-121,
155-157, 201-999
40 Pin 27-81-31-05-010 GUN 001-028, 101-121,
155-157, 201-999
55 Pin 27-81-31-05-010 GUN 001-028, 101-121,
155-157, 201-999
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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E. Location Zones
Zone Area
512 Left Wing - Krueger Flap No. 2
513 Left Wing - Krueger Flap No. 1
612 Right Wing - Krueger Flap No. 3
613 Right Wing - Krueger Flap No. 4
F. Leading Edge Flap Installation
SUBTASK 27-81-11-220-005
(1) If you install used bearings, bushings and bolts, do this task: Leading Edge Flap Inspection,
TASK 27-81-11-200-801.
SUBTASK 27-81-11-420-001
(2) If you removed the outboard Leading edge flap [2], connect the outboard Leading edge flap [2] to
the fixed leading edge:
(a) Connect hinges 1 thru 4 on the Leading edge flap [2] to the fixed leading edge.
1) Apply grease, D00633 on the mating surfaces of the bolts [23] and bolts [27].
2) At hinges 1 and 4, install the bolts [23], washers [24], bushings [19], washers [20] and
nuts [22].
NOTE: Install the bolts [23] with the head outboard.
3) Tighten the nuts [22] to 60-95 pound-inches (6.8-10.7 newton-meters).
4) Install the pin [21].
5) At hinges 2 and 3, install the bolts [27], washers [28], bushings [26], washers [25] and
　
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