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时间:2011-09-23 15:40来源:蓝天飞行翻译 作者:航空
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Ti  TITANIUM 
TLA  THROTTLE LEVER ANGLE AIRBUS 
TLA  THRUST LEVER ANGLE BOEING 
TM  TORQUE MOTOR 
TMC  TORQUE MOTOR CURRENT 
T/O  TAKE OFF 
TO/GA  TAKE OFF/GO AROUND 
T/P  TEMPERATURE/PRESSURE SENSOR 
TPU  TRANSIENT PROTECTION UNIT 
TR  TRANSFORMER RECTIFIER 
TRA  THROTTLE RESOLVER ANGLE  AIRBUS 
TRA  THRUST RESOLVER ANGLE  BOEING 
TRDV  THRUST REVERSER DIRECTIONAL VALVE 
TRF  TURBINE REAR FRAME 
TRPV  THRUST REVERSER PRESSURIZING 
VALVE 
TSI  TIME SINCE INSTALLATION (HOURS) 

EFFECTIVITY ALL CFM56-5B ENGINES FOR A319-A320-A321

CFMI PROPRIETARY INFORMATION
TSN  TIME SINCE NEW (HOURS) 
TTL  TRANSISTOR TRANSISTOR LOGIC 

UER  UNSCHEDULED ENGINE REMOVAL 
UTC  UNIVERSAL TIME CONSTANT 

VAC  VOLTAGE, ALTERNATING CURRENT 
VBV  VARIABLE BLEED VALVE 
VDC  VOLTAGE, DIRECT CURRENT 
VDT  VARIABLE DIFFERENTIAL TRANSFORMER 
VIB  VIBRATION 
VLV  VALVE 
VRT  VARIABLE RESISTANCE TRANSDUCER 
VSV  VARIABLE STATOR VANE 

WDM  WATCHDOG MONITOR 
Wf  WEIGHT OF FUEL OR FUEL FLOW   
WFM  WEIGHT OF FUEL METERED 
WOW  WEIGHT ON WHEELS 
WTAI  WING THERMAL ANTI-ICING 

LEXIS Page 9 Nov 02
CFM56-5B TRAINING MANUAL
EFG
IMPERIAL / METRIC CONVERSIONS METRIC / IMPERIAL CONVERSIONS
1 mile 1 ft 1 in. 1 mil.
1 sq.in.
1 USG 1 cu.in.
1 lb.
1 psi.
°F = 1,609 km = 30,48 cm = 25,4 mm = 25,4 μ
= 6,4516 cm2
= 3,785 l (dm3) = 16.39 cm3
= 0.454 kg
= 6.890 kPa
= 1.8 x °C + 32 1 km 1 m 1 cm 1 mm
1 m2 1 cm2
1 m3 1 dm3 1 cm3
1 kg
1 Pa 1 kPa 1 bar
°C = 0.621 mile = 3.281 ft. or 39.37 in. = 0.3937 in. = 39.37 mils.
= 10.76 sq. ft. = 0.155 sq.in.
= 35.31 cu. ft. = 0.264 USA gallon = 0.061 cu.in.
= 2.205 lbs
= 1.45 10-4 psi. = 0.145 psi = 14.5 psi
= ( °F - 32 ) /1.8

EFG
FADEC SYSTEM INTRODUCTION

EFFECTIVITY
INTRO Page 1
ALL CFM56-5B ENGINES FOR A319-A320-A321
ENGINE SYSTEMS Jan 03

CFMI PROPRIETARY INFORMATION
CFM56-5B TRAINING MANUAL
EFG
FADEC SYSTEM INTRODUCTION
FADEC purpose.
The CFM56-5B operates through a system known as FADEC (Full Authority Digital Engine Control).
It takes complete control of engine systems in response to command inputs from the aircraft. It also provides information to the aircraft for flight deck indications, engine condition monitoring, maintenance reporting and troubleshooting.
 
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