CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(3)
Move the flap control lever to the flaps position 0 (flaps up) detent to retract the flaps.
S 864-029
(4)
Do this task to depressurize hydraulic system B: "Depressurize Hydraulic System A, B, or Standby" (AMM 29-15-00/201).
(a)
Install the access panel 8215L or 8715R on the inboard end of the outboard midflap.
(b)
Install the tailcone on the inboard flap, outboard track fairing.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-86
ALL ú ú 01 Page 406 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
FLAP DEFLECTION CONTROL PLUNGER - ADJUSTMENT/TEST
_________________________________________________
1. General_______
A. There is one task in this procedure, an adjustment of the flap deflection control plunger.
TASK 27-51-86-825-001
2. Flap Deflection Control Plunger Adjustment (Fig. 501)__________________________________________
A. References
(1)
AMM 12-31-01/201, Zone Diagrams
(2)
AMM 12-31-61/201, Wing Lower Surface Access Doors and Panels
(3)
AMM 27-51-00/201, Trailing Edge Flap System
(4)
AMM 29-15-00/201, Hydraulic Systems A, B, and Standby
B.
Access
(1)
Location Zone 307 Left Wing Trailing Edge Outboard Flap and Spoilers 407 Right Wing Trailing Edge Outboard Flap and Spoilers
(2)
Access Panels
8215L Exhaust-Gate Linkage Access Panel
8715R Exhaust-Gate Linkage Access Panel
C.
Prepare for the Adjustment
S 865-048
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(1) Do this task to pressurize hydraulic system B: "Pressurize Hydraulic System A, B, or Standby" (AMM 29-15-00/201).
S 865-049
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE TRAILING
_______ EDGE FLAPS, THE LEADING EDGE FLAPS AND SLATS AND THE DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Move the flap control lever to the flaps position 0 (flaps up) detent to retract the flaps.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-86
ALL ú ú 01 Page 501 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
A-A
Flap Deflection Control Plunger Adjustment
Figure 501
H18289
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-86
ALL ú ú 01 Page 502 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 865-050
(3)
Do this task to depressurize hydraulic system B: "Depressurize Hydraulic System A, B, or Standby" (AMM 29-15-00/201).
S 865-051
(4)
Do this task: "Trailing Edge Flap System Deactivation"
(AMM 27-51-00/201).
D.
Procedure
S 225-027
(1)
At the inboard end of the midflap, examine the clearances between the roller and the fairing track:
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 4(152)
