Page 3
EFFECTIVITY
LEXIS
Dec 00
ALL CFM56-5B ENGINES FOR A319-A320-A321
CFMI PROPRIETARY INFORMATION
(自
FI FLA FLX TO FMGC
FMS FMV FOD FPA FPI FRV FWC FWD
G
GE GEM GI g.in GMT GSE
H
HCF HCU HDS HMU HP HPC HPCR FLIGHT IDLE (F/I) FORWARD LOOKING AFT FLEXIBLE TAKE-OFF FLIGHT MANAGEMENT AND GUIDANCE COMPUTER FLIGHT MANAGEMENT SYSTEM FUEL METERING VALVE FOREIGN OBJECT DAMAGE FRONT PANEL ASSEMBLY FLUORESCENT PENETRANT INSPECTION FUEL RETURN VALVE FLIGHT WARNING COMPUTER FORWARD
GENERAL ELECTRIC GROUND-BASED ENGINE MONITORING GROUND IDLE (G/I) GRAM x INCHES GREENWICH MEAN TIME GROUND SUPPORT EQUIPMENT
HIGH CYCLE FATIGUE HYDRAULIC CONTROL UNIT HORIZONTAL DRIVE SHAFT HYDROMECHANICAL UNIT HIGH PRESSURE HIGH PRESSURE COMPRESSOR HIGH PRESSURE COMPRESSOR ROTOR
CFM56-5B TRAINING MANUAL
HPSOV HIGH PRESSURE SHUTOFF VALVE
HPT HIGH PRESSURE TURBINE
HPTC HIGH PRESSURE TURBINE CLEARANCE
HPTCC HIGH PRESSURE TURBINE CLEARANCE
CONTROL
HPTCCV HIGH PRESSURE TURBINE CLEARANCE
CONTROL VALVE
HPTR HIGH PRESSURE TURBINE ROTOR
Hz HERTZ (CYCLES PER SECOND)
I
IDG INTEGRATED DRIVE GENERATOR
ID PLUG IDENTIFICATION PLUG
IFSD IN FLIGHT SHUT DOWN
IGB INLET GEARBOX
IGN IGNITION
IGV INLET GUIDE VANE
in. INCH
I/O INPUT/OUTPUT
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