S 034-014-C00
 (13)
 Remove the loop clamps from the cables.

 S 034-015-C00

 (14)
 Disconnect the end of the VBV feedback cable from the MEC feedback arm as follows:

 (a)  
Loosen the fillister head screw.

 (b)  
Remove the retainer clip from the MEC feedback arm.

 (c)  
Remove the pin to release the rod end bearing from the MEC
 feedback arm.

 S 864-016-C00
 (15) Move the cable inner member to the fully retracted position at the MEC end.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-32-05
 ALL  ú ú C02 Page 405 ú Jul 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 034-017-C00
 (16)
 If the feedback cable is to be replaced, remove the rod end bearing and the jamnut, and keep them for the installation.

 S 034-018-C00

 (17)
 Loosen the nose cap and carefully move the conduit cap free from the MEC slotted bracket.

 S 024-019-C00

 (18)
 Remove the VBV feedback cable as follows:

 CAUTION: MAKE SURE THAT BENDS IN THE CABLE ARE NOT LESS THAN SIX
_______ INCHES (152 MM) RADIUS DURING THE REMOVAL. DO THIS WHEN YOU INSTALL THE CABLE THROUGH THE SIX O'CLOCK STRUT. SMALL RADIUS BENDS CAN CAUSE PERMANENT DAMAGE TO THE CABLE.
 (a)  Hold the cable with your hand and carefully pull the cable up the 6 o'clock strut and through the junction plate.
 NOTE: Do this while you hold the cable end to prevent damage.
____
 (b)  Remove the feedback cable from the engine.
 TASK 75-32-05-404-020-C00
 3.  Install the Variable Bleed Valve Feedback Cable_______________________________________________
 A. Consumable Materials
 (1)  
D00004 Grease - Graphite (CP2101) (AMM 70-10-01/201)

 (2)  
A00003 Primer- Red, 1200 (AMM 70-10-01/201)

 (3)  
A00081 Sealant - DC 93-006-1 (AMM 70-10-01/201)

 (4)  
B00148 Methyl Ethyl Keytone (MEK) - (CP1040)

 B. References
 (1)  
AMM 70-10-01/201, Consumable Materials

 (2)  
AMM 72-33-03/401, Fan Duct Panels

 (3)  
AMM 75-32-00/201, Variable Bleed Valve System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 75-32-05
 ALL  ú ú C01 Page 406 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(4)  
AMM 75-32-05/501, Variable Bleed Valve Feedback Cable

 (5)  
AMM 78-31-00/201, Thrust Reverser System

 C. Access
 (1)  
Location Zones
 506 Engine No. 1 - Aft end of MEC
 606 Engine No. 2 - Aft end of MEC

 (2)  
Access Panels
 5783L/5739L Engine No. 1 - Thrust Reverser Half
 5838R/5839R Engine No. 2 - Thrust Reverser Half

 D. Procedure (Fig. 401)
 S 424-021-C00
 CAUTION: MAKE SURE THAT BENDS IN THE CABLE ARE NOT LESS THAN SIX INCHES
_______ (152 MM) RADIUS DURING THE REMOVAL. DO THIS WHEN YOU INSTALL THE CABLE THROUGH THE SIX O'CLOCK STRUT. SMALL RADIUS BENDS CAN CAUSE PERMANENT DAMAGE TO THE CABLE.
 (1)  With the MEC end of the cable retracted, supply the cable through the junction plate at the six o'clock strut.
 NOTE:____The MEC end of the cable is the longer end. This is measured from the two bolt flange that is attached to the cable.
 S 424-022-C00
 (2)  
Carefully put the cable down the six o'clock strut until the fixed flange touches against the junction plate.

 S 434-023-C00

 (3)  
Attach the flange to the junction plate with two bolts and two nuts.

 (a)  
Lightly lubricate the bolt threads with grease.
　
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 空氣 AIR(110)