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)
Number Name/Location
621YB Lower Leading Edge Access Panel - Slat Station
488.04
SUBTASK 27-81-00-820-011
(3) Adjust the auxiliary arm skin tabs [92] at the auxiliary track locations:
(a) Adjust the skin tab [92] to get the correct gap to the flex skin and the access panels [93];
1) Loosen the nuts [95] on the bolts [102].
2) Adjust the position of the skin tab [92] to get a gap of 0.1000 inch (2.54 millimeters)
between the skin tab [92] and the flex skin.
3) Adjust the position of the skin tab [92] to get a gap of 0.1000 -0.0400/+0.0800 inch (2.54 -
1.02/+2.03 millimeters) between the skin tab [92] and the access panels [93].
4) Tighten the nuts [95].
(b) Adjust the position of the skin tab [92] on the skin tab supports [97] to get the correct
misfair;
1) Loosen the nuts [101] on the bolts [98].
2) Adjust the position of the skin tab [92] until you get these misfairs between the slat and
the skin tab [92];
a) -0.0100 +/- 0.0200 inch (-0.25 +/- 0.51 millimeters) for a minimum of 75 percent of
the slat span.
b) -0.0100 +/- 0.0400 inch (-0.25 +/-1.02 millimeters) for a maximum of 25 percent of
the slat span.
3) Tighten the nuts [101].
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TASK 27-81-00-700-801
5. Leading Edge Flap and Slat Operational Test in Primary Mode
A. References
Reference Title
24-22-00-860-811 Supply Electrical Power (P/B 201)
27-51-00-740-801 FSEU Display and Existing Faults 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. Location Zones
Zone Area
117 Electrical and Electronics Compartment - Left
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737-600-700-800-900 飞机维护手册7 AIRCRAFT MAINTENANCE MANUA(53)
