12
LENGTH
EA AND EB -1,-3,-4,-6
12
EA AND EB -2,-5
MATERIAL
FITTINGS - CORROSION RESISTANT STEEL PER MIL-T-781
CABLES - CARBON STEEL PER BMS 7-265, TYPE I, COMP A (TZ) (RECOMMENDED)
-CARBON STEEL PER BMS 7-265, TYPE I, COMP A (OPTIONAL)
____ZINC-ONLY AND TIN-OVER-ZINC COATED CABLES ARE INTERCHANGEABLE, AND MAY BE INTERMIXED WITH A
NOTE: SYSTEM (AILERON, SPOILER, STABILIZER, ETC.), PROVIDING OPPOSITE CABLES WITHIN A GIVEN CABLE LOOP ARE REPLACED WITH CABLES OF THE SAME TYPE. (FOR EXAMPLE, IN 737 MM27-09-14 FIGURE 202, CABLES EA-2 AND EB-2 SHOULD BE REPLACED TOGETHER WITH BOTH NEW CABLES EITHER ZINC-ONLY OR TIN-OVER-ZINC.) THIS WILL PREVENT ASYMMETRIC CABLE STRETCH THAT CAN DEGRADE SYSTEM RIGGING.
REFERENCE ONLY. FOR SPECIAL PART NUMBER, LENGTH, MATERIAL,
AND END FITTINGS, REFER TO THE IPC.
Elevator Control Cables Figure 202 (Sheet 2)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
Rudder Control Cables
Figure 203 (Sheet 1)
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27-09-14
ALL ú ú 02 Page 206 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CABLE NO. LENGTH (INCHES) CABLE SIZE FITTINGS 1
REF REQ. 1 AND MATERIAL 1 2
RA-1 1 1040.5 1/8 - 7X19 MS21260L4RH BACT14A4
RB-1 1 1033.2 1/8 - 7X19 MS21260L4LH BACT14A4
RA-2 1 18.0 1/8 - 7X19 MS21260L4RH MS21260L4LH
RB-2 1 18.0 1/8 - 7X19 MS21260L4RH MS21260L4LH
RA-3 1 66.5 1/8 - 7X19 MS21260L4LH BACT14A4
RB-3 1 79.4 1/8 - 7X19 MS21260L4RH BACT14A4
RA AND RB -1,-3
12
RA-2, RB-2
MATERIAL
FITTINGS - CORROSION RESISTANT STEEL PER MIL-T-781
CABLES - CARBON STEEL PER BMS 7-265, TYPE I, COMP A (TZ) (RECOMMENDED)
- CARBON STEEL PER BMS 7-265, TYPE I, COMP A (OPTIONAL)
____NOTE: ZINC-ONLY AND TIN-OVER-ZINC COATED CABLES ARE INTERCHANGEABLE, AND MAY BE INTERMIXED WITH A
SYSTEM (AILERON, SPOILER, STABILIZER, ETC.), PROVIDING OPPOSITE CABLES WITHIN A GIVEN CABLE
LOOP ARE REPLACED WITH CABLES OF THE SAME TYPE. (FOR EXAMPLE, IN 737 MM27-09-14 FIGURE 202,
CABLES EA-2 AND EB-2 SHOULD BE REPLACED TOGETHER WITH BOTH NEW CABLES EITHER ZINC-ONLY OR
TIN-OVER-ZINC.) THIS WILL PREVENT ASYMMETRIC CABLE STRETCH THAT CAN DEGRADE SYSTEM RIGGING.
1 REFERENCE ONLY. FOR SPECIAL PART NUMBER, LENGTH, MATERIAL,
AND END FITTINGS, REFER TO THE IPC.
Rudder Control Cables
Figure 203 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 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 飞行操纵 FLIGHT CONTROLS 1(17)