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时间:2011-04-08 12:00来源:蓝天飞行翻译 作者:航空
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737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(e)  Install or tighten all of the clamps you removed or loosened on the ignition lead. 1) Tighten the bolts to 24-27 pound-inches
 (2.7-3.0 Newton meters).
 S 864-015-C00
 (6)  Remove the DO-NOT-CLOSE tags and close these circuit breakers:
 (a)  P6 Load Control Center
 1) L IGN
 2) R IGN

 S 754-017-C00
 (7)  Do an audible check of the operation of the spark igniter (AMM 74-00-00/501).
 S 414-018-C00
 WARNING: OBEY THE INSTRUCTIONS IN AMM 78-31-00/201 WHEN YOU CLOSE THE
_______ THRUST REVERSER. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
 (8)  
Close the right and left thrust reverser (AMM 78-31-00/201).

 (9)  
Close the right and left fan cowl panel (AMM 71-11-02/201).


 S 414-019-C00
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 74-21-02
 ALL  ú ú C01 Page 413 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SPARK IGNITER - INSPECTION/CHECK
________________________________
 1. General
_______
 A. This procedure provides an inspection/check for the spark igniters.
 TASK 74-21-02-206-001-C00
 2. Spark Igniter Inspection
________________________
 A. Standard Tools and Equipment
 (1)  3/8 inch medium grit abrasive impregnated rubber rod Craytex Manufacturing Company 7754 Arjohns Drive San Diego, CA 92126
 B. Consumable Materials
 (1)  
Methyl Ethyl Ketone (MEK) - CP1040 (local purchase)

 (2)  
Solvent - Stoddard - CP2011 (AMM 70-10-01/201)

 (3)  
Trichloroethane - 1, 1, 1 - CP1011 (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 74-21-02/401, Igniter Plug

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


 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
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 74-21-02
 ALL  ú ú C01 Page 601 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
3 O'CLOCK STRUT
LEFT IGNITER RIGHT IGNITER G-M56-MM-0173(1)-00-B
PLUG  PLUG
VIEW IN THE FORWARD DIRECTION
NON-REMOVABLE GASKET
GMM-1077427-03-B 
CONNECTOR PIN 
CERAMIC 
SEE  A  B  INSULATION 
TYPE 3 IGNITER PLUG 
BUSHING 
INSTALLATION  IGNITION LEAD 
THREADS  INSTALLATION THREADS 
SEE  A B  GMM-1077521-02-B 
CAPTIVE 
GASKET 
TYPE 4 IGNITER PLUG 
Spark Igniter Check 
Figure 601 (Sheet 1) 

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 74-21-02
 ALL  ú ú C01 Page 602 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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