757
MAINTENANCE MANUAL

WIRE ROPE: CARBON STEEL TYPE I, COMPOSITION A (TZ), 3/32-INCH DIA, 7 X 7 FITTINGS: CORROSION RESISTANT STEEL
NOTE:THE "B" LENGTH IS MEASURED FROM THE MS21260L3RH TERMINAL END.

THESE CABLES WERE INITIALLY INSTALLED ON GUN 001-003.
THESE CABLES WERE INITIALLY INSTALLED ON GUN 004-999.
THE CABLES SHOWN IN TABLE II ARE THE RECOMMENDED OPTION TO THE CABLES SHOWN IN TABLE I ON AIRPLANES.

NOTE:STABILIZER TRIM CONTROL CABLES ON TABLE I ARE INTERCHANGEABLE WITH CABLES ON TABLE II FOR THE SAME CABLE CODES IF THE OPPOSITE CABLES IN THE LOOP ARE REPLACED WITH CABLES OF THE SAME MATERIAL. THIS WILL PREVENT ASSYMETRIC CABLE STRETCH, WHICH CAN CAUSE PROBLEMS WITH SYSTEM RIGGING.
Stabilizer Trim Control Cables
Figure 205 (Sheet 5)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-00-01
 ALL  ú ú 12 Page 218 ú Dec 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

FLAP CONTROL LEVER
SEE

MS21260

BACT14A MS20664 EXAMPLE OF THE CABLE LENGTH
Flaps/Slats Control Cables Figure 206 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-00-01
 ALL  ú ú 02 Page 219 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

TURNBUCKLES WFA-3 BACT14B FITTING
WFA-2
WFA-1
WFB-2
WFB-1 
SHORT  WFB-3 
PART OF 
THE CABLE 
TRAILING-EDGE POWER-DRIVE-UNIT 
A-A 

FWD LESB-2 LESA-2
TURNBUCKLES
FLAP CONTROL LEVER
LESA-1
A
LESB-1
LESB-3
TRAILING-EDGE FLAP POWER-DRIVE-UNIT B-B
QUICK-DISCONNECT FITTING
LESA-3
LEADING-EDGE SLAT POWER-DRIVE-UNIT C-C
Flaps/Slats Control Cables Figure 206 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-00-01
 ALL  ú ú 02 Page 220 ú Sep 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

WIRE ROPE: CARBON STEEL TYPE I, COMPOSITION A (TZ), 3/32-INCH DIA, 7 X 7 FITTINGS: CORROSION RESISTANT STEEL
____THE "B" LENGTH IS MEASURED FROM THE MS21260L3RH TERMINAL END.
NOTE: THESE CABLES WERE INITIALLY INSTALLED ON GUN 001-003. THESE CABLES WERE INITIALLY INSTALLED ON GUN 004-999. THE CABLES SHOWN IN TABLE II ARE THE RECOMMENDED OPTION TO THE CABLES SHOWN IN TABLE I ON

AIRPLANES.
NOTE:FLAP/SLAT CONTROL CABLES ON TABLE I ARE INTERCHANGEABLE WITH CABLES ON TABLE II FOR THE SAME CABLE CODES IF THE OPPOSITE CABLES IN THE LOOP ARE REPLACED WITH CABLES OF THE SAME MATERIAL. THIS WILL PREVENT ASSYMETRIC CABLE STRETCH, WHICH CAN CAUSE PROBLEMS WITHSYSTEM RIGGING.
Flaps/Slats Control Cables
Figure 206 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-00-01
 ALL  ú ú 09 Page 221 ú Dec 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

CABLE SYSTEM  SEALS NO. OF  LOCATION  ACCESS PANEL NO. 
AILERON  4  SLOPING PRESSURE DECK  MAIN-GEAR WHEEL-WELLS/PASSENGER COMPARTMENT 
RUDDER  2  AFT PRESSURE BULKHEAD  311AL 
ELEVATOR  4  AFT PRESSURE BULKHEAD  311AL 
STABILIZER TRIM  4  AFT PRESSURE BULKHEAD  311AL 
FLAP/SLAT  2  RIGHT WHEEL-WELL CEILING  MAIN-GEAR WHEEL-WELL 

Air Pressure Seals
Figure 207

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(19)