曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(Continued)
Display State
S4 RETR GAP FAR
S5 OUTBD GAP FAR
S5 INBD GAP NEAR
S5 RETR GAP FAR
S6 OUTBD GAP FAR
S6 INBD GAP NEAR
S6 RETR GAP FAR
S7 OUTBD GAP FAR
S7 INBD GAP NEAR
S7 RETR GAP FAR
S8 OUTBD GAP FAR
S8 INBD GAP NEAR
F1 RETR GAP FAR
F1 EXT GAP NEAR
F2 RETR GAP FAR
F2 EXT GAP NEAR
F3 RETR GAP FAR
F3 EXT GAP NEAR
F4 RETR GAP FAR
F4 EXT GAP NEAR
4) Make sure the LE FLAPS EXT light on the center instrument panel, P2, is on.
5) Make sure the LE flaps and slats EXT lights on the aft overhead panel, P5, are on.
(e) Move the flap control lever to the 10-unit detent position.
1) Make sure these lights come on during the flaps and slats extension and go off after
extension.
a) The LE FLAPS TRANSIT light on the center instrument panel, P2
b) All the LE slats TRANSIT lights on the aft overhead panel.
2) Push the down arrow on the FSEU to step through the proximity sensor states.
3) Make sure these displays and the proximity sensor states show on the FSEU
(Table 506):
Table 506/27-81-00-993-817
Display State
S1 OUTBD GAP NEAR
S1 INBD GAP FAR
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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(Continued)
Display State
S2 OUTBD GAP NEAR
S2 INBD GAP FAR
S2 RETR GAP FAR
S3 OUTBD GAP NEAR
S3 INBD GAP FAR
S3 RETR GAP FAR
S4 OUTBD GAP NEAR
S4 INBD GAP FAR
S4 RETR GAP FAR
S5 OUTBD GAP NEAR
S5 INBD GAP FAR
S5 RETR GAP FAR
S6 OUTBD GAP NEAR
S6 INBD GAP FAR
S6 RETR GAP FAR
S7 OUTBD GAP NEAR
S7 INBD GAP FAR
S7 RETR GAP FAR
S8 OUTBD GAP NEAR
S8 INBD GAP FAR
F1 RETR GAP FAR
F1 EXT GAP NEAR
F2 RETR GAP FAR
F2 EXT GAP NEAR
F3 RETR GAP FAR
F3 EXT GAP NEAR
F4 RETR GAP FAR
F4 EXT GAP NEAR
4) Make sure the LE FLAPS EXT light on the center instrument pane, P2, is on.
5) Make sure the LE flaps EXTEND and slats FULL EXTEND lights on the aft overhead
panel, P5, are on.
(f) Push the ON/OFF button on the front panel of the FSEU to turn the display off.
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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F. Put the Airplane Back to Its Usual Condition
SUBTASK 27-81-00-860-040
(1) Move the flap control lever to the UP position.
SUBTASK 27-81-00-860-041
(2) To remove power from hydraulic system B, do this task: Hydraulic System A or B Power
Removal, TASK 29-11-00-860-805.
SUBTASK 27-81-00-410-002
(3) Close this access panel:
Number Name/Location
117A Electronic Equipment Access Door
------------------------- END OF TASK ---------------------------
737-600/700/800/900
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EFFECTIVITY
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Flap/Slat Electronics Unit
Figure 504 (Sheet 1 of 2)/27-81-00-990-807
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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Flap/Slat Electronics Unit
Figure 504 (Sheet 2 of 2)/27-81-00-990-807
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-81-00
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Leading Edge Flap and Slat Position Indicator
Figure 505/27-81-00-990-808
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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TASK 27-81-00-700-802
6. Leading Edge Flap and Slat Timing Test in Primary Mode
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
29-11-00-860-804 Hydraulic System A or B Pressurization with an Engine-Driven Pump
(EDP) (P/B 201)
29-11-00-860-805 Hydraulic System A or B Power Removal (P/B 201)
B. Location Zones
Zone Area
133 Main Landing Gear Wheel Well, Body Station 663.75 to Body Station
727.00 - Left
211 Flight Compartment - Left
212 Flight Compartment - Right
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(55)
