Page 4
EFFECTIVITY
LEXIS
Dec 00
ALL CFM56-5B ENGINES FOR A319-A320-A321
CFMI PROPRIETARY INFORMATION

(自
LP LPC LPT LPTC LPTCC
LPTR LRU LVDT
M
MO MCD MCL MCDU
MCL MCT MDDU mm. MMEL MTBF MTBR
N
N1 (NL)
CFM56-5B  TRAINING MANUAL 
LOW PRESSURE  N1ACT  ACTUAL N1 
LOW PRESSURE COMPRESSOR  N1DMD  DEMANDED N1 
LOW PRESSURE TURBINE  N1CMD  COMMANDED N1 
LOW PRESSURE TURBINE CLEARANCE  N2 (NH)  HP ROTOR ROTATIONAL SPEED 
LOW PRESSURE TURBINE CLEARANCE  N2ACT  ACTUAL N2 
CONTROL  NVM  NON VOLATILE MEMORY 
LOW PRESSURE TURBINE ROTOR  O 
LINE REPLACEABLE UNIT  OAT  OUTSIDE AIR TEMPERATURE 
LINEAR VARIABLE DIFFERENTIAL  OGV  OUTLET GUIDE VANE 
TRANSFORMER  OSG  OVERSPEED GOVERNOR 
P 
AIRCRAFT SPEED MACH NUMBER  P0  AMBIENT STATIC PRESSURE 
MASTER CHIP DETECTOR  P25  HPC INLET TOTAL AIR TEMPERATURE 
MAXIMUM CLIMB  PCU  PRESSURE CONVERTER UNIT 
MULTIPURPOSE CONTROL AND  PLA  POWER LEVER ANGLE 
DISPLAY UNIT  PMC  POWER MANAGEMENT CONTROL 
MAXIMUM CLIMB  PMUX  PROPULSION MULTIPLEXER 
MAXIMUM CONTINUOUS THRUST  PS12  FAN INLET STATIC AIR PRESSURE 
MULTIPURPOSE DISK DRIVE UNIT  PS13  FAN OUTLET STATIC AIR PRESSURE 
MILLIMETERS  PS3HP  COMPRESSOR DISCHARGE STATIC AIR 
MAIN MINIMUM EQUIPMENT LIST  PRESSURE 
MEAN TIME BETWEEN FAILURES  psi  POUNDS PER SQUARE INCH 
MEAN TIME BETWEEN REMOVALS  psia  POUNDS PER SQUARE INCH ABSOLUTE 
psid  POUNDS PER SQUARE INCH 
DIFFERENTIAL 
LOW PRESSURE ROTOR  psig  POUNDS PER SQUARE INCH GAUGE 
ROTATIONAL SPEED 

Page 5
EFFECTIVITY
LEXIS
Dec 00
ALL CFM56-5B ENGINES FOR A319-A320-A321

CFMI PROPRIETARY INFORMATION
(自  CFM56-5B  TRAINING MANUAL 
PSM  POWER SUPPLY MODULE  SDU  SOLENOID DRIVER UNIT 
PSS  (ECU) PRESSURE SUB-SYSTEM  SER  SERVICE EVALUATION REQUEST 
PSU  POWER SUPPLY UNIT  SFC  SPECIFIC FUEL CONSUMPTION 
PT  TOTAL PRESSURE  SG  SPECIFIC GRAVITY 
PT2  FAN INLET TOTAL AIR PRESSURE  SLS  SEA LEVEL STANDARD 
(PRIMARY FLOW)  (CONDITIONS : 29.92 in. Hg/59 F) 
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：TRAINING MANUAL CFM56-5B BASIC ENGINE(4)