T52404 F95236
574 Stabilizer Trim Control Cables
Aug 01/96 Figure 205 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 27-09-111 Page 209
Flight Spoiler Control Cables 500
27-09-111 Figure 206 (Sheet 1) May 15/68
Page 210
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
CABLE REF NO. REQ. LENGTH 1 (INCHES) CABLE SIZE AND MATERIAL FITTINGS 1
1 2
WSA1-1 1 61.4 3/32 - 7x7 MS21260L3RH BACT14A3
WSA1-2 1 33.8 3/32 - 7x7 MS21260L3LH BACT14A3
WSA1-3 1 242.8 3/32 - 7x7 MS21260L3LH BACT14A3
WSA1-4 1 257.2 3/32 - 7x7 MS21260L3RH BACT14A3
WSA2-1 1 66.3 3/32 - 7x7 MS21260L3LH BACT14A3
WSA2-2 1 38.5 3/32 - 7x7 MS21260L3RH BACT14A3
WSA2-3 1 185.3 3/32 - 7x7 MS21260L3RH BACT14A3
WSA2-4 1 199.9 3/32 - 7x7 MS21260L3LH BACT14A3
WSB1-1 1 86.4 3/32 - 7x7 MS21260L3RH BACT14A3
WSB1-2 1 58.5 3/32 - 7x7 MS21260L3LH BACT14A3
WSB1-3 1 279.4 3/32 - 7x7 MS21260L3LH BACT14A3
WSB1-4 1 262.5 3/32 - 7x7 MS21260L3RH BACT14A3
WSB2-1 1 91.2 3/32 - 7x7 MS21260L3LH BACT14A3
WSB2-2 1 63.0 3/32 - 7x7 MS21260L3RH BACT14A3
WSB2-3 1 321.6 3/32 - 7x7 MS21260L3RH BACT14A3
WSB2-4 1 305.1 3/32 - 7x7 MS21260L3LH BACT14A3
MATERIAL
FITTINGS - CORROSION RESISTANT STEEL PER MIL-T-781
CABLES - CARBON STEEL PER BMS 7-265, TYPE I, COMP A (TZ) (PREFERRED)
-
CARBON STEEL PER MIL-W-83420, TYPE I, COMP A (FIRST OPTION)
-
CARBON STEEL PER MIL-W-1511, (SECOND OPTION)
NOTE: ZINC-ONLY AND TIN-OVER-ZINC COATED CABLES ARE INTERCHANGEABLE, AND MAY BE INTERMIXED WITHIN A SYSTEM (AILERON, SPOILER, STABLIZER, ETC.), PROVIDING OPPOSITE CABLES WITHIN A GIVEN CABLE LOOP ARE REPLACED WITH CABLES OF THE SAME TYPE. (FOR EXAMPLE, IN 737 MM 27-09-111 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.
T52406
502 Flight Spoiler Control Cables
Aug 01/96 Figure 206 (Sheet 2) 27-09-111
Page 211
B
O
E
I
NG P
R
OP
RI
E
T
A
R
Y
- Copyri
ght
. - Unpubl
i
s
hed W
o
rk
- S
ee t
i
t
l
e page f
o
r det
ai
l
s
.
F95435 F95942 T52423 F95944 T52428
Trailing Edge Flap Control Cables 535
27-09-111 Figure 207 (Sheet 1) May 01/00
Page 212
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
535 Trailing Edge Flap Control Cables
Aug 15/78 Figure 207 (Sheet 2) 27-09-111
Page 213
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Trailing Edge Flap Control Cables 535
27-09-111 Figure 207 (Sheet 3) Aug 01/96
Page 214
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
504 Trailing Edge Flap Boom Cables
May 15/70 Figure 208 (Sheet 1) 27-09-111
Page 215
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
Trailing Edge Flap Boom Cables 511
27-09-111 Figure 208 (Sheet 2) Aug 01/96
Page 216
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
FLIGHT CONTROL CABLES AIR PRESSURE SEALS - MAINTENANCE PRACTICES
1. General
A. This subject provides the information necessary to locate all flight control cable air pressure seals. Refer to Chapter 20, Control Cable Air Pressure Seals, for removal and Installation.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(20)