S 865-134
(5)
Pressurize the hydraulic system B (AMM 27-81-00/201).
S 865-135
(6)
Move the flap control lever to the 10-unit detent to fully extend the leading edge slats.
S 865-136
WARNING: MAKE SURE THAT YOU RELEASE THE PRESSURE FROM THE HYDRAULIC
_______ SYSTEM WHEN YOU DO THE ADJUSTMENT OF THE LEADING EDGE SLATS. WITH THE HYDRAULIC SYSTEM PRESSURIZE, THE LEADING EDGE FLAPS AND SLATS CAN MOVE. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(7) Release the pressure from hydraulic system B (AMM 27-81-00/201).
S 495-137
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.
(8)
Install the leading edge slat actuator locks when you adjust the leading edge slats with the actuator connected (AMM 27-81-00/201).
S 825-209
(9)
Adjust the forward lower auxiliary track support (initial adjustment):
(a)
Loosen the nut.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-00
ALL ú ú 02 Page 551 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
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.
(b)
If it is necessary install below the forward auxiliary track clevis, three laminated shims (equal to 0.186 inch total thickness maximum), or five laminated shims (equal to 0.310 inch total thickness maximum) in the lower forward support fitting with taller forward flange.
(c)
Tighten the nut to 160-240 pound-inches.
S 825-143
CAUTION: MAKE SURE YOU SET THE LOWER AUXILIARY TRACK SUPPORTS TO THE
_______ HIGH SIDE. THIS IS TO PREVENT THE SLAT UPPER TRAILING EDGE AND/OR THE FIXED LEADING EDGE FROM DAMAGE DURING THE SLAT RETRACTION.
(10)
Adjust the aft lower auxiliary track support (initial adjustment):
(a)
Loosen the bolt of the upper aft auxiliary track support.
(b)
Loosen the jamnut.
(c)
Loosen the lock bolt and nut until the tapered lock is free (approximately one turn).
(d)
Extend the aft auxiliary track clevis (not fully) with the adjustable nut.
(e)
Tighten the jamnut and nut on the lock bolt finger-tight.
S 085-196
(11)
Remove the leading edge slat actuator locks from the leading edge slat (AMM 27-81-00/201).
S 865-145
(12)
Pressurize the hydraulic system B (AMM 27-81-00/201).
S 865-185
(13)
Move the flap control lever to UP position to fully retract the slats.
S 495-191
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.
(14) Install the leading edge slat actuator locks when you adjust the leading edge slats with the actuator connected (AMM 27-81-00/201).
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-00
ALL ú ú 02 Page 552 ú Nov 12/00
中國航空網 www.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(48)
