74-21-01
 ALL  ú ú C01 Page 408 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(f)
Remove the two O-rings from the ignition lead.

 (g)
Discard the two O-rings from the ignition lead.

 TASK 74-21-01-404-011-C00
 3. Install the Ignition Lead
_________________________
 A. Equipment
 (1)  Tool - Ignition Lead Nut Removal,
 No. 856A2007P01,
 (Required for Type 3 ignition lead only)
 CFM International,

 P.O. Box 15514
 Cincinnati, OH 45215

 B. Consumable Materials
 (1)  
Graphite Grease - CP2101 (AMM 70-10-01/201)

 (2)  
Parting Agent - Refer to Boeing Process Specification BAC5000, General Sealing, for a list of suitable parting agents and their suppliers.

 (3)  
Penetrating Oil - CP2162 (AMM 70-10-01/201)

 (4)  
Petrolatum - CP2102 (AMM 70-10-01/201)

 (5) Primer and Sealant - BMS5-63, Type 1, Class B-4 ú (6) Primer and Sealant - BMS5-63, Type 2, Class B-4 (Optional to ú BMS5-63, Type 1, Class B-4 primer and sealant)
 (7)  
Primer, Red - 1200 (AMM 70-10-01/201)

 (8)  
Sealant - 93-006-1 (AMM 70-10-01/201)

 (9)  
Sealant - 93-006-6 (AMM 70-10-01/201)

 (10)
 Solvent - Trichloroethane 1, 1, 1, CP1011
 (AMM 70-10-01/201)

 (11)
 Solvent - Methyl Ethyl Ketone (MEK), CP1040
 (AMM 70-10-01/201)

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

 (2)  
AMM 71-11-02/201, Fan Cowl Panels

 (3)  
AMM 74-00-00/501, Ignition

 (4)  
AMM 78-31-00/201, Thrust Reverser System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ALL  ú ú C02.1 Page 409 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
D.  Access
 (1)  
Location Zones 503 Engine No. 1 - Forward Side of the Accessory Gearbox at the 9 o'clock position 504 Engine No. 1 - Forward Side of the Accessory Gearbox at the 9 o'clock position 505 Engine No. 1 - Forward Side of the Accessory Gearbox at the 9 o'clock position 502 Engine No. 1 - Forward Side of the Accessory Gearbox at the 9 o'clock position 603 Engine No. 2 - Forward Side of the Accessory Gearbox at the 9 o'clock position 604 Engine No. 2 - Forward Side of the Accessory Gearbox at the 9 o'clock position 605 Engine No. 2 - Forward Side of the Accessory Gearbox at the 9 o'clock position

 602  Engine No. 2 - Forward Side of the Accessory Gearbox at the 9 o'clock position

 (2)  
Access Panels
 5737L Engine No. 1 - Right Fan Cowl Panel
 5738L Engine No. 1 - Left Thrust Reverser
 5739L Engine No. 1 - Right Thrust Reverser
 5746L Engine No. 1 - Left Fan Cowl Panel
 5837R Engine No. 2 - Right Fan Cowl Panel
 5838R Engine No. 2 - Left Thrust Reverser
 5839R Engine No. 2 - Right Thrust Reverser
 5846R Engine No. 2 - Left Fan Cowl Panel

 E.  Install the Ignition Leads
 S 864-012-C00
 (1)  If the left ignition lead was removed, make sure this circuit breaker is open:
 (a)  P6 Load Control Center
 1) L IGN

 S 864-013-C00
 (2)  If the right ignition lead was removed, make sure this circuit breaker is open:
 (a)  P6 Load Control Center
 1) R IGN

 S 424-014-C00
 (3)  Do these steps to install the ignition leads (Fig. 401):
 (a) Install the two new O-rings on the ignition lead fitting.
 1)  Apply a layer of petrolatum (CP2102) to the O-rings (AMM 70-10-01/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 74-21-01
 ú  ALL  ú
　
中國航空網 m.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 點火 IGNITION(14)