EFFECTIVITY
ALL CFM56-5B ENGINES FOR A319-320-321
CFMI PROPRIETARY INFORMATION LEXIS Page 8
Nov 02
CFM56-5B TRAINING MANUAL
TBC THERMAL BARRIER COATING TSN TIME SINCE NEW (HOURS)
TBD TO BE DETERMINED TTL TRANSISTOR TRANSISTOR LOGIC
TBO TIME BETWEEN OVERHAUL
TBV TRANSIENT BLEED VALVE U
TC(TCase) HP TURBINE CASE TEMPERATURE UER UNSCHEDULED ENGINE REMOVAL
TCC TURBINE CLEARANCE CONTROL UTC UNIVERSAL TIME CONSTANT
TCCV TURBINE CLEARANCE CONTROL VALVE
TCJ TEMPERATURE COLD JUNCTION V
T/E TRAILING EDGE VAC VOLTAGE, ALTERNATING CURRENT
TECU ELECTRONIC CONTROL UNIT INTERNAL VBV VARIABLE BLEED VALVE
TEMPERATURE VDC VOLTAGE, DIRECT CURRENT
TEO ENGINE OIL TEMPERATURE VDT VARIABLE DIFFERENTIAL TRANSFORMER
TGB TRANSFER GEARBOX VIB VIBRATION
Ti TITANIUM VLV VALVE
TLA THROTTLE LEVER ANGLE AIRBUS VRT VARIABLE RESISTANCE TRANSDUCER
TLA THRUST LEVER ANGLE BOEING VSV VARIABLE STATOR VANE
TM TORQUE MOTOR
TMC TORQUE MOTOR CURRENT W
T/O TAKE OFF WDM WATCHDOG MONITOR
TO/GA TAKE OFF/GO AROUND Wf WEIGHT OF FUEL OR FUEL FLOW
T/P TEMPERATURE/PRESSURE SENSOR WFM WEIGHT OF FUEL METERED
TPU TRANSIENT PROTECTION UNIT WOW WEIGHT ON WHEELS
TR TRANSFORMER RECTIFIER WTAI WING THERMAL ANTI-ICING
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 LEXIS Page 9
Nov 02
CFM56-5B TRAINING MANUAL
IMPERIAL / METRIC CONVERSIONS METRIC / IMPERIAL CONVERSIONS
1 mile 1 ft
1 in.
1 mil. = 1,609 km = 30,48 cm = 25,4 mm = 25,4 μ 1 km 1 m
1 cm 1 mm = 0.621 mile
= 3.281 ft. or 39.37 in. = 0.3937 in.
= 39.37 mils.
1 sq.in.
= 6,4516 cm2 1 m2 = 10.76 sq. ft.
1 cm2 = 0.155 sq.in.1 USG = 3,785 l (dm3) 1 m3 = 35.31 cu. ft.
1 cu.in.
= 16.39 cm3 1 dm3 = 0.264 USA gallon
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