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MAXIMUM
SERVICE
DIAMETRIC
CLEARANCE
#14 BOLT O.D. 0.2485 in
6.312 mm
0.2495 in
6.337 mm
0.2475 in
6.286 mm
0.076 mm
#15 BUSHING I.D. 0.3750 in
9.525 mm
0.3756 in
9.540 mm
0.3769 in
9.572 mm
0.0024 in
#15 BUSHING O.D. 0.3740 in
9.500 mm
0.3745 in
9.512 mm
0.3732 in
9.480 mm
0.060 mm
#16 BEARING I.D. 0.2500 in
6.350 mm
0.2505 in
6.362 mm
0.2525 in
6.413 mm
0.0030 in
#16 BOLT O.D. 0.2485 in
6.311 mm
0.2495 in
6.337 mm
0.2475 in
6.286 mm
0.076 mm
SUBTASK 27-81-11-420-006
(4) Do this task: Leading Edge Flap Installation, TASK 27-81-11-400-801.
------------------------- END OF TASK ---------------------------
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Leading Edge Flap Wear Limits
Figure 601 (Sheet 1 of 4)/27-81-11-990-802
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Leading Edge Flap Wear Limits
Figure 601 (Sheet 2 of 4)/27-81-11-990-802
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Leading Edge Flap Wear Limits
Figure 601 (Sheet 3 of 4)/27-81-11-990-802
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Leading Edge Flap Wear Limits
Figure 601 (Sheet 4 of 4)/27-81-11-990-802
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LEADING EDGE SLAT - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of the leading edge slat
(2) An installation of the leading edge slat.
B. There are four slats on each wing. This procedure is applicable for the leading edge slats 1 thru 8.
C. You can do this procedure with the airplane on jacks or off jacks, but the wing should not be
supported outboard of the engines.
TASK 27-81-21-000-801
2. Leading Edge Slat Removal
A. References
Reference Title
27-81-00-040-801 Deactivate the Leading Edge Flaps and Slats (P/B 201)
27-81-00-480-801 Leading Edge Flap and Slat Locks Installation (P/B 201)
27-81-00-860-804 Leading Edge Flaps and Slats Retraction (P/B 201)
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)
30-11-31-000-801 Wing Anti-Ice Telescoping Duct Seal 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-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)
SPL-2041 Sling - Leading Edge Slat Removal/Installation
(Part #: C27056-19, Supplier: 81205, A/P Effectivity: 737-600, -700,
-700C, -700ER, -700QC, -800, -900, -900ER, -BBJ)
C. 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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D. Access Panels
Number Name/Location
521AAB Lower Leading Edge Access Panel - Slat Station 508.31
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(69)
