R 1EFF : 201-202, 1 31-37-00Page A12 1 1 May 01/05 1 1 1CES 1
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ALPHA PARAMETER NAME UNIT CALL-UP NUMBER -------------------------------------------------------------------------------
R MN 06.1.205.01 R 06.2.205.10 R MN3 06.3.205.11 R MW1 7C.1.350.01 R 7C.2.350.10 R MW2 7C.1.351.01 R 7C.2.351.10 R MW3 7C.1.352.01 R 7C.2.352.10 R MW4 7C.1.353.01 R 7C.2.353.10 R MW5 7C.1.354.01 R 7C.2.354.10 R N1C 7C.1.341.01 R 7C.2.341.10 R N1L 7C.1.337.01 R 7C.2.337.10 R N1MX 7C.1.342.01 R 7C.2.342.10 R NA 7A.1.176.01 R NPA 0D.1.075.00 R OIK 0D.1.071.01 R 0D.1.071.10 R OIP 26.1.317.01 R 26.2.317.01 R 26.1.317.10 R 26.2.317.10 R OIQ 29.1.073.00 R 29.2.073.00 R 29.1.073.11 R 29.2.073.11 R OIQH 0D.1.062.01 R 0D.1.062.10 R OIT 26.1.316.01 R 26.2.316.01 R 26.1.316.10 R 26.2.316.10 R OTA 7A.1.247.01 R OVP 5C.1.153.01 R 5C.2.153.10 R P25 7C.1.262.01 R 7C.2.262.10 R P2A 7A.1.112.01
MACH
MACH
MAINTENANCE DATA #1
MAINTENANCE DATA #2
MAINTENANCE DATA #3
MAINTENANCE DATA #4
MAINTENANCE DATA #5
N1 COMMAND
N1 LIMIT
N1 MAXIMUM
RPM APU
N APU PEAK
Oil quant corrected Eng 1 Oil quant corrected Eng 2 ENG 1 OIL PRESSURE
ENG 2 OIL PRESSURE ENG 2 OIL QUANTITY ENG 1 OIL QUANTITY Oil consumpt prev. flight eng1
Oil consumpt prev. flight eng2 ENG 1 OIL TEMPERATURE
ENG 2 OIL TEMPERATURE APU OIL SUMP TEMP OUTFLOW VALVE POS
P25 (LPC EXIT PRESSURE) INLET PRESSURE (APU)
Mach
Mach
% rpm % rpm % rpm % rpm Quart PSI PSI Quart Quart Quart/Hour Deg C Deg C Deg C
% psia psia bar
R 1EFF : 201-202, 1 31-37-00Page A13 1 1 May 01/05 1 1 1CES 1
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ALPHA PARAMETER NAME UNIT CALL-UP NUMBER -------------------------------------------------------------------------------
R P3 7C.1.264.01 PB BURNER PRESSURE psia
R 7C.2.264.10 psia
R PBV 8E.1.112.11 PACK BYPASS VALVE POSITION %
R 8E.2.112.00
R PCSW 5C.1.057.01 STATUS + FAULT INFO
R 5C.2.057.10
R PD 6F.1.142.01 PRECOOLER ENG 2 INLET PRESS PSI
R 6F.2.142.10
R 6F.1.143.01 PRECOOLER ENG 1 INLET PRESS PSI
R 6F.2.143.10
R PDC 5C.1.144.01 CABIN DIFF. PRESS PSI
R 5C.2.144.10
R PF 8E.1.126.11 PACK FLOW kg/sec
R 8E.2.126.00
R PFAD 7A.1.004.01 PERFORMANCE ADJUSTMENTS (APU)
R PH 0D.1.050.00 Flight Phase (DMU)
R PHA 3D.1.226.01 N 1 PHASE OF UNBALANCE ENG 1 Deg
R 3D.1.226.10 N 1 PHASE OF UNBALANCE ENG 2 Deg
R PO 7C.1.114.01 SELECTED PO psia
R 7C.2.114.10
R PS13 7C.1.127.01 PS13 (FAN EXIT PRESSURE) psia
R 7C.2.127.10
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