LEFT OUTBOARD ELEVATOR
NOTE:LEFT SIDE ELEVATORS SHOWN TYPICAL FOR RIGHT SIDE
A
Elevator Control Cables
Figure 4 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú ú 02 Page 8 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
LENGTH FITTINGS 1
CABLE NO. (TO NEAREST TENTH
REF REQ INCH) 1 2 1 2
E1A-1 1 731.2 3 MS21260L4RH BACT14A4
E1B-1 752.2 3 BACT14A4
E2A-1 752.45 MS20658-4
E2B-1 733.45 MS21260L4RH MS20658-4
E1A-2 448.2 3 MS21260L4LH MS21260L4RH
E1B-2 398.2 3
E2A-2 447.1
E2B-2 397.8
E1A-3 784.5 3
E1A-3A 317.5
E1B-3 784.5 3
E1B-3A 361.0
E2A-3 784.5
E2A-3A 324.1
E2B-3 764.2
E2B-3A 363.1 MS21260L4RH
E1A-4 25.8 BACT14A4
E1B-4 12.2
E2A-4 17.3
E2B-4 1 28.8 MS21260L4LH BACT14A4
RIGHT OUTBD ELEVATOR
POWER PACKAGE
E2B-4 E2A-4
RIGHT INBD ELEVATOR AFT QUADRANTS
POWER PACKAGE
AND FEEL UNIT E2B-3A
POSITION TRANSMITTER
E2A-3A (4 LOCATIONS)
E2B-3
E2A-3
CONTROL E1B-4E2B-2
COLUMNS
E2A-2 E1A-4
E2B-1 E1B-3A
E2A-1
FEEL
COMPUTER
E1A-3A
E1B-3
E1B-2
LEFT INBD E1B-1 ELEVATOR POWER
LEFT OUTBD
PACKAGEE1A-3
ELEVATOR E1A-2 POWER E1A-1 PACKAGE
FWD QUADRANT AND
TENSION REGULATOR
(2 LOCATIONS)
Elevator Control Cables
Figure 4 (Sheet 3)
M48822
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú ú 02 Page 9 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
Elevator Control Cables
Figure 4 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú ú 02 Page 10 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M48842
A
747-400
MAINTENANCE MANUAL
WS1B-3
WS2B-3 (WS1B-4, RIGHT WING)
WS1A-3 (WS2B-4,
(WS1A-4, RIGHT WING) RIGHT WING)
TURNBUCKLE WS2A-3 (WS2A-4,WS2A-7
WS1A-5 RIGHT WING)
(WS2A-8, RIGHT WING)(WS1A-6, RIGHT WING) WS2A-5
WS2A-9 (WS2A-10, RIGHT WING) (WS2A-6, RIGHT WING)
FWD
INBOARD SPOILER INBOARD SPOILERDIFFERENTIAL DIFFERENTIALMECHANISM MECHANISM(LEFT WING (RIGHT WINGQUADRANT)
QUADRANT) WS2B-3
WS2B-1 OUTBOARD SPOILER
DIFFERENTIAL
MECHANISM OUTBOARD SPOILER
(LEFT WING DIFFERENTIAL
WS1B-3 QUADRANT) MECHANISM
WS1B-1 (RIGHT WING
QUADRANT)
WS2A-3
WS1A-3 WS1B-2
WS1A-1 WS2A-1 WS2B-2
WS2B-4 WS1B-4 WS1A-2 WS2A-2 WS1A-4
WS2A-4
FWD
AILERON QUADRANTS (REF) AILERON QUADRANTS (REF)
Flight Spoiler Control Cables
Figure 5 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú ú 02 Page 11 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
CABLE SCHEMATIC
Flight Spoiler Control Cables Figure 5 (Sheet 2)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(19)
