S 992-020-C00
(2)
Do not apply grease to corrosion resistant steel wire rope.
D. Proof load.
S 992-021-C00
(1) The proof load for 3/32 inch cable assembly is 552-577 pounds.
(a) The proof load for the T1A/T1B-1, the T2A/T2B-1, the ESS1A/ESS2A-1 and the ESS1B/ESS2B-1 cables is 400-425 pounds.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-04
ALL ú ú C02 Page 206 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(2) S 992-022-C00The proof load for a cable assembly with a 1/16 inch segment is 288-313 pounds.
(3) S 992-023-C00Proof load the cable assembly from end to end in straight lengths.
(4) S 992-024-C00Proof load the cable assemblies with intermediate terminals as follows: (a) Proof load the cable between the intermediate fittings and one end fitting. (b) Proof load the cable between one end fitting and the other end fitting.
(5) S 992-025-C00Kinks, popped cores, protruding wire ends, and broken wires are not permitted.
(6) S 992-026-C00Slippage between the wire rope and the fitting is not permitted.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-04
ALL ú ú C02 Page 207 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SERVOMECHANISM
Engine Control Cables Figure 201
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
76-11-04
ALL ú ú C04 Page 208 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ESS2A-2
ESS1A/ESS1B-1
Fuselage Engine Control Cables
Figure 202 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH OPTIONAL CABLES ú
76-11-04
OR WITHOUT SB 76-1023 OR SL 76-15 ú ú C01 Page 209 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
ESS2B
TURNBUCKLE
T2B
TURNBUCKLE ESS2A CABLET1B
TURNBUCKLE ESS2B CABLE FWD
ESS1B CABLE ESS1A CABLE T1B CABLE T1A CABLE
A-A
Fuselage Engine Control Cables
Figure 202 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH RECOMMENDED CABLES ú
76-11-04
OR WITH SB 76-1023 AND SL 76-15 ú ú C04 Page 210 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 发动机控制 ENGINE CONTROLS(58)