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 Engine #2 control word #4
 ECW5  Engine #1 control word #5
 Engine #2 control word #5
 ECYC  Engine # 1 cycles (DMU computed)
 Engine # 2 cycles (DMU computed)
 EGT  7C 1 345 01  DEGC  EGT LPT exit temp engine #1
 7C 2 345 10  DEGC  EGT LPT exit temp engine #2
 EGTA  7A 1 175 01  DEGC  APU EGT
 EGTF  DEGC  EGT LPT exit temp engine #1:Filtered parameter
 DEGC  EGT LPT exit temp engine #2:Filtered parameter
 EGTK  EGT corrected left (DMU computed)
 EGT corrected right (DMU computed)
 EGTP  DEGC  APU EGT PEAK during APU start
 EGTR  DEG  delta EGT reference value in climb
 delta EGT reference value in cruise
 EHRS  Engine #1 hours (DMU computed)
 Engine #2 hours (DMU computed)
 ELEV  6C 1 314 01  DEG  Elevator position left
 6C 1 334 01  DEG  Elevator position right
 ENGFA  17 1 304 00  A/C type engine
 ENTYP  Engine type (DMU computed)
 ERT  7C 1 050 01  H  Engine #1 running time
 7C 2 050 10  H  Engine #2 running time
 ESN  Engine #1 serial number (DMU computed)
 Engine #2 serial number (DMU computed)
 ESN1  7C 1 047 01  Engine serial number (First half) engine #1
 7C 1 046 01  Engine serial number (Last half) engine #1
 ESN2  7C 2 047 10  Engine serial number (First half) engine #2
 7C 2 046 10  Engine serial number (Last half) engine #2
 EVM  3D 1 035 01  EVM discrete word #1 engine #1
 3D 1 035 10  EVM discrete word #1 engine #2
 F319  1B 1 137 01  FLAP actual position left for A319
 1B 2 137 10  FLAP actual position right for A319
 F320  1B 1 137 01  FLAP actual position left for A320
 1B 2 137 10  FLAP actual position right for A320
 F321  1B 1 137 01  DEG  FLAP actual position left for A321
 1B 2 137 10  DEG  FLAP actual position right for A321
 FD  Fuel density left wing tank (DMU computed)
 Fuel density right, wing tank (DMU computed)
 FDC  Fuel density center wing tank (DMU computed)
 FDL  Fuel density left wing tank (DMU computed) 

R 1EFF : 001-049, 051-099, 101-105, 159-199, 1 31-37-00Page 20 1210-210, 1May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
Alpha Parameter Unit Comment -------------------------------------------------------------------------------
FDR 
FDRAW  5A 2 272 10 
FF  7C 1 244 01 
7C 2 244 10 
FFK 
FLAP 
FLAPW 
FLCNT 
FLNUM 
FLT 
FM 
FMB 
FMF  26 1 126 01 
26 2 126 01 
FMGD1  01 1 274 00 
01 2 274 00 
FMGD2  01 1 275 00 
01 2 275 00 
FMGD4  01 1 146 00 
01 2 146 00 
FMI 
FMV  7C 1 347 01 
7C 2 347 10 
FPA  04 1 322 01 
04 2 322 10 
FPAC  04 1 323 01 
04 2 323 10 
FPPU  1B 1 137 01 
1B 2 137 10 
FROM 
FRTO  ORIGIN 
FT  5A 2 177 10 
5A 2 201 10 
GLA  29 1 100 00 
29 2 100 00 
GLE  29 1 077 01 
29 1 077 10 
GLS  25 1 174 01 
25 1 174 10 
GS  04 1 312 01 
04 2 312 10 

PPH/KG PPH/KG
DEG DEG DEG
% % DEG DEG G G DEG DEG
DEGC DEGC % % % % DDM DDM KTS KTS Fuel density right wing tank (DMU computed)Fuel densityFuel mass flow rate engine #1Fuel mass flow rate engine #2Fuel flow corrected engine #1 Fuel flow corrected engine #2FLAP actual position leftFLAP actual position rightFLAP actual position switchedFlight counterFlight number (DMU computed)Flight number (DMU computed)Flight phase to display (DMU computed)Flight phase broadcasted to ACARS(DMU computed)FWC Flight phasesFWC Flight phasesFMGC discrete status word #1FMGC discrete status word #1FMGC discrete status word #2FMGC discrete status word #2FMGC discrete status word #4FMGC discrete status word #4Internal flight phase (DMU computed)Selected FMV position engine #1Selected FMV position engine #2Flight path angleFlight path angleFlight path accelerationFlight path accelerationFLAP actual position (FPPU angle value)FLAP actual position (FPPU angle value)Departure (DMU computed)Departure (DMU computed) Destination (DMU COMPUTED)Fuel temperature engine #1Fuel temperature engine #2APU Generator loadAPU Generator loadGenerator load engine #1Generator load engine #2ILS1 glideslope deviationILS2 glideslope deviationGround speedGround speed
　
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