S 865-188

 (27)
 Move the flap control lever to 1-unit position to extend the leading edge slats to the intermediate position.

 S 495-203

 (28)
 Install the leading edge slat actuator locks when you adjust the leading edge slats with the actuator connected (AMM 27-81-00/201).

 S 225-215

 (29)
 Align the noses of the slats to get a mismatch of 0.0 to 0.06 inch between adjacent slats.

 S 225-216

 (30)
 Make sure the clearance between the slat upper trailing edge and the fixed leading edge is 0.0 to 0.06 inch at the slat ends.

 S 225-217

 (31)
 Adjust the cam plate:

 (a)  
Loosen the nuts that attach the cam plate to the detent arm.

 (b)  
Move the cam plate forward or aft until you get these conditions: 1) The detent arm roller touches the root of each detent arm. 2) Make sure the clearance between the detent arm roller and

 WARNING:_______ CAREFULLY INSTALL THE LEADING EDGE SLAT ACTUATOR LOCKS.  THE
 LEADING EDGE SLATS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE
 LOCKS CORRECTLY.  THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO
 EQUIPMENT.

 the forward surface of the cam plate is 0.0 to 0.03 inch. 3) Tighten the nuts.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-00
 ALL  ú ú 02 Page 555 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 085-262
 (32)
 Remove the leading edge slat actuator locks from the leading edge slat (AMM 27-81-00/201).

 S 865-263

 (33)
 Move the flap control lever to UP position to fully retract the slats.

 S 495-264

 (34)
 Install the leading edge slat actuator locks when you adjust the leading edge slats with the actuator connected (AMM 27-81-00/201).

 S 825-258

 (35)
 Adjust the detent arm torsion to a load of 50 pounds (22.68 Kgms) +/-5 pounds (2.268 Kgms) at the auxiliary track locations with the steps that follow:

 (a)  
Install a dummy weight of 50 pounds (22.68 kgms) +/- 5 pounds

 WARNING:_______ CAREFULLY INSTALL THE LEADING EDGE SLAT ACTUATOR LOCKS.  THE
 LEADING EDGE SLATS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE
 LOCKS CORRECTLY.  THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO
 EQUIPMENT.

 (2.268 kgms) on the detent arm cam plate as shown in Fig. 506, View C-C.
 (b)  
With the dummy weight installed, turn the torsion rod bolt (at the other end of the torsion rod opposite to the detent arm/torsion rod connection) until you get a clearance of 0.1 inch (2.54 mm) between the stop and the lower edge inside the slot of the detent arm.

 (c)  
Remove the dummy weight from the detent arm cam plate after you have adjusted the load.

 S 085-271
 (36) Remove the leading edge slat actuator locks from the leading edge slat (AMM 27-81-00/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-00
 ALL  ú ú 02 Page 556 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-272
 (37)
 Move the flap control lever to the 1-unit detent to extend the slats.

 S 825-267

 (38)
 Install the leading edge slat actuator locks when you adjust the leading edge slats with the actuator connected (AMM 27-81-00/201).

 S 225-218

 (39)
 Adjust the forward lower auxiliary track support:

 WARNING:_______ CAREFULLY INSTALL THE LEADING EDGE SLAT ACTUATOR LOCKS.  THE
 LEADING EDGE SLATS CAN MOVE QUICKLY IF YOU DO NOT INSTALL THE
 LOCKS CORRECTLY.  THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO
 EQUIPMENT.

 CAUTION: YOU CAN TELL IF YOU HAVE LOADED TOO MANY SHIMS IF THE
_______ AUXILIARY TRACK CLEVIS IS ABOVE THE FORWARD FLANGE OF THE LOWER FORWARD SUPPORT FITTING. THIS IS TO PREVENT THE FORWARD AUXILIARY TRACK CLEVIS FROM DAMAGE.
　
中國(guó)航空網(wǎng) m.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(50)