(3)
C27012-1 - Leading Edge Slat Actuator Lockout Set
C.
Standard Tools and Equipment
(1)
Spring Scale - 60 to 110 pound capacity
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-00
ALL ú ú 03 Page 529 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D.
E.
F.
G.
H.
A
737-300/400/500MAINTENANCE MANUAL
Consumable Materials
(1)
A00028 Adhesive - BMS 5-92, Type 1
(2)
A00247 Sealant - BMS 5-95, Class B
(3)
C00259 Primer - BMS 10-11, Type IReferences
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 27-51-00/501, Trailing Edge FLap Control System
(3)
AMM 27-81-00/201, Leading Edge FLap and Slat Control System
(4)
AMM 27-81-41/401, Leading Edge Slat ActuatorAccess
(1)
Location Zone 101 Control Cabin, LH 102 Control Cabin, RH 302 Wing Outboard Leading Edge Including Slats, LH 402 Wing Outboard Leading Edge Including Slats, RH 303 Wing Inboard Leading Edge Including Slats, LH 403 Wing Inboard Leading Edge Including Slats, RH
Prepare the System for Adjustment
S 865-009
(1)
Supply electrical power (AMM 24-22-00/201).
S 865-010
(2)
Pressurize the hydraulic system B (AMM 27-81-00/201).Adjust the Leading Edge Flap Control Valve
S 865-045
(1)
Move the flap control lever to the FLAPS UP detent.
S 865-046
(2)
After 5 minutes, release the pressure from hydraulic system B (AMM 27-81-00/201).
S 035-047
(3)
Remove the lower pan from the flap control unit of the trailing edge.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-00
ALL ú ú 04 Page 530 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 285-048
(4)
Make sure that the rig pin F-1 moves freely in the flap control unit.
(a)
If the rig pin F-1 does not move freely, adjust the trailing edge flap system (AMM 27-51-00/501).
S 225-049
(5)
Make sure the valve slide and the index surface of the control valve align to a limit of |0.010 inch (Fig. 502).
(a)
Adjust the leading edge link if it is necessary: 1) Remove the lockwire. 2) Loosen the checknut. 3) Remove the rod end bolt at the cam follower arm. 4) Turn the rod end in 1/2-turn increments to adjust the
leading edge link.
5) Install the rod end bolt.
6) Make sure the valve slide and the index surface align to a
limit of |0.010 inch.
7) Install the washer and locknut.
8) Tighten the checknut.
9) Install the lockwire.
10) Make sure the thread on the rod end is not out of
tolerance.
S 085-050
(6)
Remove the rig pin F-1.
S 435-051
(7)
Install the lower pan on the flap control unit.
I.
Adjust the Leading Edge Flaps
(1)
Pressurize the hydraulic system B (AMM 27-81-00/201).
S 865-053
(2)
Move the flap control lever to the 1-unit detent to extend the leading edge flaps.
(3)
Release the pressure from hydraulic system B (AMM 27-81-00/201).
S 865-052
S 865-054
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-00
ALL ú ú 02 Page 531 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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(38)
