WIRE ROPE: CARBON STEEL TYPE I, COMPOSITION A, 1/8-INCH DIA, 7 X 19 FITTINGS: CORROSION RESISTANT STEEL
Elevator Control Cables
Figure 204 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú
ú 02 Page 212
ú Jun 20/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
ELEVATOR FITTINGS
CABLE CODE NO. REQ. PART NUMBER "A" LENGTH (INCH) -1 -2
E1A-1 1 BACC2C4C03909FG 390.9 BACT14A4 MS21260L4RH
-2 1 BACC2C4C05174EF 517.4 MS21260L4RH MS21260L4LH
-3 1 BACC2C4C07436EF 743.6 MS21260L4RH MS21260L4LH
-4 1 BACC2C4C00230EG 23.0 BACT14A4 MS21260L4LH
E1B-1 1 BACC2C4C03675FG 367.5 BACT14A4 MS21260L4RH
-2 1 BACC2C4C05174EF 517.4 MS21260L4RH MS21260L4LH
-3 1 BACC2C4C07766EF 776.6 MS21260L4RH MS21260L4LH
-4 1 BACC2C4C00125EG 12.5 BACT14A4 MS21260L4LH
E2A-1 1 BACC2C4C03207FG 320.7 BACT14A4 MS21260L4RH
-1 1 BACC2C4C03187FG 318.7 4 BACT14A4 MS21260L4RH
-2 1 BACC2C4C04366EF 436.6 MS21260L4RH MS21260L4LH
-3 1 BACC2C4C07359EF 735.9 MS21260L4RH MS21260L4LH
-4 1 BACC2C4C01625EG 162.5 BACT14A4 MS21260L4LH
-4 1 BACC2C4C01605EG 160.5 4 BACT14A4 MS21260L4LH
E2B-1 1 BACC2C4C03394FG 339.4 BACT14A4 MS21260L4RH
-1 1 BACC2C4C03374FG 4337.4 BACT14A4 MS21260L4RH
-2 1 BACC2C4C03976EF 397.6 MS21260L4RH MS21260L4LH
-3 1 BACC2C4C07359EF 735.9 MS21260L4RH MS21260L4LH
-4 1 BACC2C4C01827EG 182.7 BACT14A4 MS21260L4LH
-4 1 BACC2C4C01809EG 4180.9 BACT14A4 MS21260L4LH
TABLE II
WIRE ROPE: CARBON STEEL TYPE I, COMPOSITION A (TZ), 1/8-INCH DIA, 7 X 19 FITTINGS: CORROSION RESISTANT STEEL
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.
____ELEVATOR CABLES ON TABLE I ARE INTERCHANGEABLE WITH CABLES ON TABLE II FOR THE SAME
NOTE: 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.
GUN 001-999;
THESE CABLES ARE THE RECOMMENDED REPLACEMENTS.
Elevator Control Cables
Figure 204 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-00-01
ALL ú
ú 13 Page 213
ú Dec 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
EXAMPLE OF THE CABLE LENGTH
AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND
Horizontal Stabilizer Trim Control Cables Figure 205 (Sheet 1)
中國航空網 www.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(17)
