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时间:2011-04-08 11:53来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

20,000 pounds
One
Annular
Two spool, 13 stage compressor, consisting of a 4 stage low pressure compressor (in-cludes 1st-stage fan) and a 9 stage high pressure compressor
Clockwise (as viewed from the rear looking forward)
5 stage, split, consisting of a 1 stage high pressure turbine and a 4 stage low pressure turbine
4290 pounds dry (approximate) 5390 pounds (approximate)
Engine Length (with flame arrestor) 114.5 inches (approximate)Installed Engine Length (with
192.6 inches (approximate)  Inlet Cowl)
Engine Specifications
Figure 1 (Sheet 1)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////

Engine Diameter Largest Diameter (without Inlet Cowl - including Accessory Gearbox)Largest Diameter (with Inlet
Cowl)
IGNITION SYSTEM Ignition ExciterIgniter Plug
LUBRICATION SYSTEM Oil Specification Oil Tank Capacity
FUEL SYSTEM Fuel Specification
87.6
 inches (approximate)

88.4
 inches (approximate)


Two (per engine)
Two (per engine)
Refer to 70-10-01
Refer to 79-11-00, Description and Operation
Specification D1655-JET-A,-A1,-B; MIL-T-5624G JP-1,JP-4,JP-5; MIL-T-83133 JP-8
Engine Specifications
Figure 1 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////


NOTE: DIMENSIONS ARE IN INCHES WITH MILLIMETERS IN PARENTHESES.
S-M56-MM-0903-(1)-02-B
Engine Overall Dimensions Figure 2
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
VBV SYSTEM 
IGB AND 
NO. 3 BRG 
BOOSTER  NO. 2 BRG 
NO. 1 BRG  HP COMPRESSOR  CHAMBER COMBUSTION 
NO. 4 BRG 
SECONDARY  CORE MAJOR  LPT  NO. 5 BRG 
AIR STREAM  MODULE 
PRIMARY 
AIR STREAM 
FAN 

SUMP FORWARD 
MODULE FAN MAJOR  ACTUATOR VSV  HPT  MODULE TURBINE MAJOR LOW PRESSURE AFT SUMP  FRAME TURBINE 
DRIVE SYSTEM ACCESSORY CASE FAN INLET  FRAME FAN  BRG SUPPORT NO. 1 & 2 

S-M56-MM-0900-(1)-01-B
Engine Major Section Components Location Figure 3
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
GEARBOX ACCESSORY  GEARBOX TRANSFER 
HEAT EXCHANGER MAIN OIL/FUEL  HEATER SERVO FUEL 
FUEL PUMP CONTROL ENGINE MAIN 
FWD 
Engine Accessory Components Location Figure 4 

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 ALL  ú ú C01 Page 6 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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