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Alpha Parameter Unit Comment -------------------------------------------------------------------------------
OIP 26 1 317 01 26 1 317 10 OIQ 26 1 073 01 26 1 073 10 OIQH
OIT 26 1 316 01 26 1 316 10 OTA 7A 1 247 01 OVP 5C 1 153 01 5C 2 153 10 PO 7C 1 114 01 7C 2 114 10 P2 7C 1 131 01 7C 2 131 10 P25 7C 1 262 01 7C 2 262 10 P2A 7A 1 112 01 P3 7C 1 264 01 7C 2 264 10 PB 7C 1 264 01 7C 2 264 10 PBV 8E 1 112 11 8E 2 112 00 PCSW 5C 1 057 01 5C 2 057 10 PD 6F 1 143 01 6F 1 142 01 PDC 5C 1 144 01 5C 2 144 10 PF 8E 1 126 11
8E 2 126 00 PFAD 7A 1 004 01 PH PHA 3D 1 226 01
3D 1 226 10 PHT 3D 1 226 11 3D 1 226 00 PS13 7C 1 127 01 7C 2 127 10 PSB 26 1 320 01 26 1 320 10 PSEL
PSI PSI QUART QUART QTS/H QTS/H DEGC DEGC DEGC % % PSIA PSIA PSIA PSIA PSIA PSIA BAR PSIA PSIA PSIA PSIA % %
PSI PSI PSI PSI KG/S KG/S
DEG DEG DEG DEG PSIA PSIA PSIA PSIA OIL pressure engine #1OIL pressure engine #2OIL quantity engine #1OIL quantity engine #2OIL consumption from the previous flight Eng.#1OIL consumption from the previous flight Eng.#2OIL temperature engine #1OIL temperature engine #2APU OIL sum temperatureOutflow valve positionOutflow valve positionSelected PO (Ambient pressure) engine #1Selected PO (Ambient pressure) engine #2PT2 (FAN inlet pressure) engine #1PT2 (FAN inlet pressure) engine #2P2.5 (Low Pressure Compressor exit pressure) #1P2.5 (Low Pressure Compressor exit pressure) #2APU inlet pressurePb burner pressure engine #1Pb burner pressure engine #2Pb burner pressure engine #1Pb burner pressure engine #2Pack bypass valve position system #1Pack bypass valve position system #2Press control bus:Status + Fault infoPress control bus:Status + Fault infoPrecooler inlet pressure engine #1Precooler inlet pressure engine #2Cabin differential pressureCabin differential pressurePack flow system #1Pack flow system #2APU:Performance adjustmentsFlight phase to display (DMU computed)N1 phase unbalance brg1 engine #1N1 phase unbalance brg1 engine #2N1 phase unbalance TRF engine #1N1 phase unbalance TRF engine #2PS13 (FAN exit pressure) engine #1PS13 (FAN exit pressure) engine #2No4 bearing pressure engine #1No4 bearing pressure engine #2Status of different FADEC sensor engine #1 Status of different FADEC sensor engine #2
R 1EFF : 001-049, 051-099, 101-105, 159-199, 1 31-37-00Page 24 1210-210, 1May 01/05 1 1 1CES 1
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Alpha Parameter Unit Comment -------------------------------------------------------------------------------
PSW1 8E 1 062 11
8E 2 062 00
PT 7A 1 166 01
PT2 7C 1 131 01
7C 2 131 10
PTCH 04 1 324 01
04 2 324 10
PTCR 04 1 326 01
04 2 326 10
RAC 7C 1 055 01
7C 2 055 10
RALT 25 1 164 01
25 1 164 10
RI 8E 1 130 11
8E 2 130 00
RO 8E 1 124 11
8E 2 124 00
ROLL 04 1 325 01
04 2 325 10
ROLR 04 1 327 01
04 2 327 10
ROPP 6E 1 330 01
6E 2 330 10
RSCC 6E 1 332 01
6E 2 332 10
RSP2 6C 1 362 01
6C 1 372 01
RSP3 6C 1 363 01
6C 1 373 01
RSP4 6C 1 364 01
6C 1 374 01
RSP5 6C 1 365 01
6C 1 375 01
RUDD 29 1 312 00
29 2 312 00
RUDT 0A 1 313 00
0A 2 313 00
SAT 06 1 213 01
06 2 213 10
SC1 29 1 242 01
SC1 29 2 242 01
SC2 29 1 244 01
BAR PSIA PSIA DEG DEG DEG/S DEG/S % % FEET FEET % % % % DEG DEG DEG/S DEG/S DEG DEG KTS KTS DEG DEG DEG DEG DEG DEG DEG DEG DEG DEG DEG DEG DEGC DEGC DEGC/F DEGC/F DEGC/F Discrete data word (Label 062) of pack control bus system #1Discrete data word (Label 062) of pack control bus system #2Bleed air pressurePT2 (FAN inlet pressure) engine #1PT2 (FAN inlet pressure) engine #2Pitch anglePitch angleBody axis pitch rateBody axis pitch rateRotor active clearance control position Eng. #1Rotor active clearance control position Eng. #2Radio height (R/A1)Radio height (R/A2)Pack ram inlet position LHPack ram inlet position RHPack ram outlet position LHPack ram outlet position RHROLL angleROLL angleBody axis roll rateBody axis roll rateRight brake pedal angleRight brake pedal anglereference speed command channelreference speed command channelLH spoiler #2 positionRH spoiler #2 positionLH spoiler #3 positionRH spoiler #3 positionLH spoiler #4 positionRH spoiler #4 positionLH spoiler #5 positionRH spoiler #5 positionRudder positionRudder positionRudder trimRudder trimStatic air temperature (BNR)Static air temperature (BNR)Selected ckpt compt tempSelected ckpt compt tempSel fwd cab compt temp 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM 指示/记录系统 4(45)
