27-81-01
ALL ú ú 01 Page 413 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(f)
Attach the Krueger flap (1) to the rotary actuators (5) with the bolts (4, 11, and 12), bushings (6), washers (7 and 13), antirotation clip (10) and nuts (8 and 14) (Section B-B, Fig. 401).
(g)
Tighten the nuts to 290-410 pound-inches.
(h)
Install the bonding jumper (2) on each hinge (15).
S 094-040
WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ LE FLAP SAFETY LOCKS. THE LE FLAPS CAN MOVE QUICKLY IF YOU DO NOT DO THE STEPS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(4) Do this task: "Safety Lock Removal and Leading Edge Flap Activation" (AMM 27-81-00/201).
S 864-014
CAUTION: DO NOT ELECTRICALLY EXTEND OR RETRACT THE FLAPS MORE THAN ONE
_______ TIME IN 5 MINUTES. DAMAGE TO THE MOTOR CAN OCCUR IF THE MOTOR BECOMES TOO HOT.
(5)
For the applicable system, Remove the DO-NOT-CLOSE tags and close these circuit breakers:
(a)
P6 Main Power Distribution Panel
1) 6L21 LE FLAP ELEC CONT GRP B DRIVE 1
2) 6L22 LE FLAP ELEC CONT GRP A DRIVE 2
3) 6L23 LE FLAP ELEC CONT GRP A DRIVE 3
4) 6L24 LE FLAP ELEC CONT GRP A DRIVE 4
5) 6E3 PRIM LE FLAP CONT GRP A AC
6) 6E4 PRIM LE FLAP CONT GRP A DC
7) 6E5 PRIM LE FLAP CONT GRP B AC
8) 6E6 PRIM LE FLAP CONT GRP B DC
(b)
P7 Overhead Circuit Breaker Panel
1) 7C10 FLT CONT ELEC 2L-AC
2) 7C11 FLT CONT ELEC 2L-DC
3) 7C12 FLT CONT ELEC 1L-AC
4) 7C13 FLT CONT ELEC 1L-DC
5) 7C14 FLT CONT ELEC 1R-AC
6) 7C15 FLT CONT ELEC 1R-DC
7) 7C16 FLT CONT ELEC 2R-AC
8) 7C17 FLT CONT ELEC 2R-DC
(c)
P414 Power Distribution Center - Left
1) 414A5 LE FLAP ELEC DRIVE 1
2) 414A2 LE FLAP ELEC DRIVE 4
(d)
P415 Power Distribution Center - Right 1) 415M35 LE FLAP ELEC DRIVE 2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-81-01
ALL ú ú 01 Page 414 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
2) 415B32 LE FLAP ELEC DRIVE 3
(6) S 864-041Operate the Krueger flaps electrically: (a) Push the ALTN FLAPS ARM switch. (b) Turn the ALTN FLAPS EXT/RET switch to the RET position then the EXT position. (c) Push the ALTN FLAPS ARM switch to put the flap system in the usual control. (d) Turn the ALTN FLAPS EXT/RET switch to the OFF position.
(7) S 714-016Make sure the flap moves smoothly with no unusual noise.
(8) S 094-017Remove the safety locks from all the flaps.
(9) S 864-018Do this task to pressurize hydraulic systems No. 1 and 4: "Hydraulic System Pressurization" (AMM 29-11-00/201).
S 864-019
(10)
Move the flap control lever to a minimum of 5-unit detent to extend the trailing edge flaps.
S 864-020
(11)
Do this task: "Supply Pneumatic Power" (AMM 36-00-00/201).
S 864-038
WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED , THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
(12)
Move the flap control lever to the full UP detent to retract the LE flaps pneumatically.
S 224-022
(13)
Do a check of the difference between the aft end of the flap and the wing structure (Detail B, Fig. 402):
NOTE: The difference must be | 0.02 inch for 75% of the flap span
____ and | 0.04 inch for 25% of the span.
(a)
Move the flap control lever to the 5-unit detent to extend the Krueger flaps.
(b)
Remove the shims attached to the structure.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 7(78)
