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. 

PROOF LOAD AT THE SAME LOAD AS 3/32 INCH CABLES AIRPLANES WITH TWO-PIECE WFA-2/WFB-2 CABLE AIRPLANES WITH ONE-PIECE WFA/B-2 CABLE REFERENCE ONLY. FOR SPECIAL PART NUMBER, LENGTH, MATERIAL
AND END FITTINGS, REFER TO THE IPC.
Trailing Edge Flap Control Cables Figure 207 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-09-14
 ALL  ú
 ú  03  Page 214
 ú  Nov 15/98 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

EXHAUST
FWD
GATE

INBD
Trailing Edge Flap Boom Cables
Figure 208 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-09-14
 ALL  ú ú 01 Page 215 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
CABLE  LENGTH 4  CABLE SIZE  FITTINGS 4 
REF  (INCHES)  AND MATERIAL  1  2  3 
BC-1A/B BC-2A/B BC-3 BC-4  19.60 25.91 69.45 80.25 2 2 1 1  1/8 - 7X19 1/8 - 7X19 3/32 - 7X19 3/32 - 7X19  MS20667-4 BACT14A3 BACT14A3 MS20667-4  MS21260S4LH MS21260S4RH 69-43546-1 69-43546-1  BACT14A3 BACT14A3 

1 2

BC-1A/B, BC-2A/B

MATERIAL
FITTINGS:
CABLES:
CARBON STEEL PER BMS 7-265, TYPE I, COMP A (TZ)
RECEPTACLE FITTING (2) MOVES DOWN OVER END FITTING (3) FOR INSTALLATION
REFERENCE ONLY. FOR SPECIAL PART NUMBER, LENGTH, MATERIAL,

AND END FITTINGS, REFER TO THE IPC.
Trailing Edge Flap Boom Cables Figure 208 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-09-14
 ALL  ú ú 01 Page 216 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 C. Access
 (1)  
Location Zone
 208 Forward Cargo Compartment
 218 Aft Cargo Compartment
 216 Main Wheel Well, LH
 217 Main Wheel Well, RH

 D.
Adjust the Control Cables

 S 832-005
 (1)  
Tighten the control cable of the system to two times the usual tension.

 S 832-006

 (2)  
Adjust the cable system.

 (a)  
Use the table below for the number of test cycles that are necessary for a system.

 ~............................................................... | | NUMBER OR | | | TEST CYCLES AT TWICE | | CABLE SYSTEM | WORKING TENSION | ................................................................. | AILERON | 20 | | ELEVATOR | 25 | | TRAILING EDGE FLAPS | 25 | | RUDDER | 25 | | SPEED BRAKE | 20 | | SPOILER | 20 | | STABILIZER TRIM | 5 | 2.............................….................................1
 S 822-009
 (3)  
Do this task to adjust the aileron cable system: "Aileron and Aileron Trim Control System Adjustment" (AMM 27-11-00/501).

 S 822-010

 (4)  
Do this task to adjust the rudder cable system: "Rudder and Rudder Trim Control System Adjustment" (AMM 27-21-00/501).

 S 822-011

 (5)  
Do this task to adjust the elevator and tab cable system: "Elevator and Tab Control System Adjustment" (AMM 27-31-00/501).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 1(20)