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)
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本文链接地址：TRAINING MANUAL CFM56-5B BASIC ENGINE(4)
