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A
737-300/400/500MAINTENANCE MANUAL
0.10 INCH MIN
C-C
Leading Edge Slat Adjustment
Figure 505 (Sheet 3)
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A 737-300/400/500MAINTENANCE MANUAL
MISMATCH FROM THE SLAT LOWER TRAILING TRAILING EDGE AND THE FIXED LEADINGEDGE TO THE FIXED LEADING EDGE: EDGE PANEL: 0.06 +0.12/-0.03 INCH
|0.02 INCH FOR A MINIMUM OF 75% OF THE SPAN
|0.04 INCH FOR A MAXIMUM OF 25% OF THE SPAN
(SLAT SHOWN RETRACTED)
(AIRPLANES WITH WASHERS BELOW THE UPSTOP ADJUSTMENT BOLT HEAD)
D-D
|0.02 INCH FOR A MINIMUM OF 75% OF THE SPAN
|0.04 INCH FOR A MAXIMUM OF 25% OF THE SPAN
(SLAT SHOWN RETRACTED)
(AIRPLANES WITH SHIMS BELOW THE UPSTOP ADJUSTMENT BOLT HEAD)
D-D
Leading Edge Slat Adjustment Figure 505 (Sheet 4)
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A
737-300/400/500MAINTENANCE MANUAL
MAIN
BOLT
TRACK
WASHER
DOWNSTOP
RIB
MAIN
WASHER
TRACK
BOLT/WASHER
NUT GUIDE/STOP RETAINER
(AIRPLANES WITHOUT THREE-WAY ADJUSTABLE DOWNSTOPS) NUT E-E
MAIN
BOLT
TRACK
BOLT
WASHER
DOWNSTOP
CLAMP-UP BUSHINGSTOP LOCATOR
DOWNSTOPRIB
WASHER RIB
F-F
NUT GUIDE/STOP FIXED LEADING EDGE
(AIRPLANES WITH THREE-WAY ADJUSTABLE DOWNSTOPS)
E-E
UPSTOP ADJUSTMENT BOLT
SLAT ASSEMBLY
SHIM
UPSTOP
CONTACT REQUIRED
(SLAT SHOWN RETRACTED) (AIRPLANES WITH SHIMS UNDER UPSTOP ADJUSTMENT BOLT HEAD) K-K Leading Edge Slat Adjustment Figure 505 (Sheet 5)
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A 737-300/400/500MAINTENANCE MANUAL
AUXILIARY
TRACK
FORWARD LOWER AUXILIARY TRACK SUPPORT ADJUSTMENT
H-H
NOT ON AIRPLANES WITH SELF-LUBRICATED BEARINGS
Leading Edge Slat Adjustment
Figure 505 (Sheet 6)
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E36587
A 737-300/400/500MAINTENANCE MANUAL
Leading Edge Slat Adjustment
Figure 505 (Sheet 7)
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737-300/400/500MAINTENANCE MANUAL
0.26 +O.14/-0.06 INCH BETWEEN
0.26 |0.06 INCH BETWEEN THE THE ADJACENT SLATS IN THE
ADJACENT SLATS WITH THE SLATS RETRACTED POSITION. MISMATCH BETWEEN
IN RETRACTED POSITION AND 0.20 INCH MINIMUM BETWEEN THE ADJACENT SLATS
(AIRPLANES WITH BLADE SEALS) (AIRPLANES WITH SPRING LOADED SEALS) M-M M-M
2A MARK SEAL AT THIS LOCATION WITH SEAL COMPRESSED BY ADJACENT SLAT OR STRUCTURE. 中國航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 6(34)
