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(d) On slat 2, 3 or 4, do these steps to remove hydraulic lines [53] and [54] from the slat
actuator assembly [2];
1) Remove the nut [51], washer [50] and bolt [49] and the clamp [52].
2) Remove the nut [28] and bolt [27] and the clamps [26] and [52].
(e) Remove the nuts [39], washers [38], bolts [37] and clamps [36] that attach the hydraulic
lines [29], [30] or [53], [54] with [40] and [41] to the bracket [32].
(f) Install caps on the hydraulic ports on the slat actuator assembly [2].
(g) Install plugs in the open ends of the hydraulic lines [29], [30] or [53], [54] with [40] and [41].
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Figure 401 (Sheet 1 of 4)/27-81-41-990-802
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Figure 401 (Sheet 2 of 4)/27-81-41-990-802
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Figure 401 (Sheet 3 of 4)/27-81-41-990-802
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TASK 27-81-41-400-801
3. Leading Edge Slat Actuator Installation
(Figure 401)
A. References
Reference Title
27-81-00-080-801 Leading Edge Flap and Slat Locks Removal (P/B 201)
27-81-00-700-802 Leading Edge Flap and Slat Timing Test in Primary Mode (P/B 501)
27-81-00-710-801 Leading Edge Flap and Slat System Standby Actuation Operational
Test (P/B 501)
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
SPL-1739 Kit - Slat Rigging Tools
(Part #: C27045-1, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. Consumable Materials
Reference Description Specification
A00247 Sealant - Pressure And Environmental - Chromate
Type
BMS5-95
C00528 Compound - Corrosion Preventive, Petroleum Hot
Application (Soft Film)
MIL-C-11796,
Class III
D. Expendables/Parts
AMM Item Description AIPC Reference AIPC Effectivity
2 Actuator assembly 27-81-41-10-100 GUN 001-028, 101-121,
155-157, 201-999
13 Pin 57-40-00-33A-050 GUN 001-099, 101-122,
156, 201-999
E. Location Zones
Zone Area
521 Left Wing - Leading Edge to Front Spar
522 Left Wing - Slat No. 4
523 Left Wing - Slat No. 3
524 Left Wing - Slat No. 2
525 Left Wing - Slat No. 1
621 Right Wing - Leading Edge to Front Spar
622 Right Wing - Slat No. 5
623 Right Wing - Slat No. 6
624 Right Wing - Slat No. 7
625 Right Wing - Slat No. 8
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F. Access Panels
Number Name/Location
521DB Lower Leading Edge Access Panel - Slat Station 71.38
521EB Lower Leading Edge Access Panel - Slat Station 98.95
521KB Lower Leading Edge Access Panel - Slat Station 188.12
521LB Lower Leading Edge Access Panel - Slat Station 216.76
521RB Lower Leading Edge Access Panel - Slat Station 307.75
521SB Lower Leading Edge Access Panel - Slat Station 337.62
521XB Lower Leading Edge Access Panel - Slat Station 435.91
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(84)
