曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 2)  Loosen the down-stop adjustment bolt and rotate the main track down-stops to the flat stop surface that let you set the correct clearances, and/or turn the adjustment nut of each aft auxiliary track an additional maximum of one (1) turn, as viewed looking down.
 NOTE: If the adjustment nut of the aft auxiliary track
____ was already turned an additional one (1) maximum turn for cruise position adjustment, then no additional adjustment turns are permitted.
 3)  Make sure you get the correct clearances as shown in Table II (View C-C, Fig. 505), and in View B-B (Detail "D", Fig. 505): a) Do the down-stop adjustment several times, if
 necessary, until you get the permitted clearances.
 4)  Apply locking compound sealer to the down-stop bolt threads after you completed the adjustment of the main track down-stops.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-00
 ALL  ú ú 02 Page 561 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 5) Hold the bolthead while you tighten the nut to 50-75 pound-inches. 6) Tighten the upper aft auxiliary track support bolt.
 S 285-179
 (45)
 At all the slat positions, make sure the clearances and the surfaces align to the specified tolerance.

 (a)  
Use a sufficient quantity of adhesive to make a 0.12 inch adhesive fillet around the upstop.

 NOTE: Do not apply the adhesive directly to the shim faying
____ surfaces, or the faying surfaces on the upstop and rib.
 (b)  Tighten the fastener to 90-100 pound-inches before the adhesive is dry.
 S 285-237
 (46)
 Make sure the clearances between the slat proximity sensors and the slat auxiliary track targets are correct and adjust any out of adjustment clearance if necessary (AMM 27-88-11/401).

 S 735-235

 (47)
 Do the flap and slat system tests (in primary and alternate modes) and the usual operation time test for flaps and slats given in this airplane maintenance manual.

 L.
Put the Airplane Back to Its Usual Condition

 (1)
Install the access plate and seal at the slat actuator rod end.

 S 085-198

 (2)  
Remove the leading edge slat actuator locks from the leading edge slat (AMM 27-81-00/201).

 (3)  
Move the flap control lever to the FLAPS UP position.

 S 425-015
 S 865-014
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-00
 ALL  ú ú 02 Page 562 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-012
 (4)  Release the pressure from the hydraulic system B (AMM 27-81-00/201).
 TASK 27-81-00-735-013
 5.  System Test - Leading Edge Flaps and Slats__________________________________________
 A. References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 27-81-00/201, Leading Edge Flap and Slat Control System

 B.
Access

 (1)  
Location Zone
 101 Control Cabin, LH
 102 Control Cabin, RH

 C.
Prepare the Leading Edge Flaps and Slats for Test

 S 865-028
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 865-029

 (2)  
Pressurize the hydraulic system B (AMM 27-81-00/201).

 S 865-042

 (3)  
Make sure these circuit breakers are closed:

 (a)  
P6 Circuit Breker Panel
 1) BATT BUS and IND LTS
 2) SECTION 1
 3) LE FLAP POS IND AC
 4) LE FLAP POS IND DC
 5) FLAP SHUTOFF VALVES
 6) STBY RUD and STBY HYDR PUMP CONT
 7) NO. 1 GEN BUS IND
 8) STBY HYD PUMP (normal)
 9) SECTION 4
 10) NO. 1 DC IND LTS

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 6(53)