Alpha Call-ups A320

 AIRB  A IRBUS US A319/320/32 A 319/320/321 1 Call UP

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AMM AMM 31-37-00

 A/C Type (DMU (DMU computed) computed)  APU control word word #1 (DMU computed)  APU control word word #2 (DMU computed)  APU control word word #3 (DMU computed)  APU control word word #4 (DMU computed)  APU cycles (DMU (DMU computed) computed)  APU start cycles cycles  APU:Discrete status status word #1 #1  APU operating hours  APU hours (DMU (DMU computed) computed)  Aileron position position left  Aileron position position right  AIL  A ILL L  Aileron position position left  AIL  A ILR R  Aileron position position right  AL  A L T  Altitude  AL  A L T3 altitude 3  AL  A L TR  Altitude rate FT/MIN  AMW1  A MW1  APU:Maintenance  APU:Maintenance word #1  AMW2  A MW2  APU:Maintenance  APU:Maintenance word #2  AMW3  A MW3  APU:Maintenance  APU:Maintenance word #3  AOA  A OA Corrected angle of attack system #1 Corrected angle of attack system #2  A0A  A 0A3 3 Corrected angle of attack 3  AP  A P  Auto pilot status status (AP) left  Auto pilot status status (AP) right  APL  A PLA A T  A/P lateral mode mode left  A/P lateral mode mode right  APL  A PLON ON  A/P longitudinal longitudinal mode left  A/P longitudinal mode right  ASN  A SN  APU serial number  number   ACTYP  A CTYP  ACW1  A CW1  ACW2  A CW2  ACW3  A CW3  ACW4  A CW4  ACYC  A CYC  ACYI  A CYI  ADW1  A DW1  AHRI  A HRI  AHRS  A HRS  AIL  A IL

BP1 BP2 BP3 BP4 BT1 BT2 BT3 BT4 BVP

brake 1 pressure brake 2 pressure brake 3 pressure brake 4 pressure Brake 1 temperature Brake 2 temperature Brake 3 temperature Brake 4 temperature Scavenge valve open engine #1 Scavenge valve open engine #2

CAS CAS3 CFPG

Computed air speed calibrated air speed 3 Calculated flight path acceleration system #1  Calculated flight path acceleration system #2 %MAC Calculated inertial vertical speed system #1 Calculaied inertial vertical speed system #2 report count Pack compr. outlet temperature LH Pack compr. outlet temperature RH current SVN1 current SVN2 current SVN3 current SVN4

CG CIVV CNT COT CSV1 CSV2 CSV3 CSV4

DSW1 DSW2 DSW3

Drift angle GMT date DME 1 frequency DME 2 frequency BSCU discrete status word 1 BSCU discrete status word 2 BSCU discrete status word 3

ECW1

Engine #1 control word #1

DA DATE DMEF

Engine #2 control word #1 ECW2 Engine #1 control word #2 Engine #2 control word #2 ECW3 Engine #1 control word #3 Engine #2 control word #3 ECW4 Engine #1 controi word #4 Engine #2 control word #4 ECW5 Engine #1 control word #5 Engine #2 control word #5 ECYC Engine # 1 cycles Engine # 2 cycles EGT EGT LPT exit temp engine #1 EGT LPT exit temp engine #2 EGTA  APU EGT EGTF EGT LPT exit temp engine #1:Filtered parameter  EGT LPT exit temp engine #2:Filtered parameter  EGTK EGT corrected left EGT corrected right EGTP  APU EGT PEAK during APU start EGTR delta EGT reference value in climb delta EGT reference value in cruise EHRS Engine #1 hours (DMU computed) Engine #2 hours (DMU computed) ELEV Elevator position left Elevator position right ENGFA  A/C type engine ENTYP Engine type ERT Engine #1 running time Engine #2 running time ESN Engine #1 serial number  Engine #2 serial number (DMU computed) ESN1 Engine serial number (First half) engine #1

ESN2 EVM

Engine serial number (Last half) engine #1 Engine serial number (First half) engine #2 Engine serial number (Last half) engine #2 EVM discrete word #1 engine #1 EVM discrete word #1 engine #2

FLAP actual position left for A319 FLAP actual position right for A319 F320 FLAP actual position left for A320 FLAP actual position right for A320 F321 FLAP actual position left for A321 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) FDR Fuel density right wing tank (DMU computed) FDRAW Fuel density FF Fuel mass flow rate engine #1 Fuel mass flow rate engine #2 FFK Fuel flow corrected engine #1 Fuel flow corrected engine #2 FLAP FLAP actual position left FLAP actual position right FLAPW FLAP actual position switched FLCNT Flight counter  FLNUM Flight number (DMU computed) FLT Flight number FM Flight phase to display FMB Flight phase broadcasted to ACARS FMF FWC Flight phases FMGD1 FMGC discrete status word #1 FMGD2 FMGC discrete status word #2 F319

FMGD4 FMI FMV FPA FPAC FPPU FROM FRTO FT GLA GLE GLS GS GW GWFK GWFL HPT HPTC IALT IGV ILS IVV K

FMGC discrete status word #4 Internal flight phase Selected FMV position engine #1 Selected FMV position engine #2 Flight path angle Flight path acceleration FLAP actual position Departure Departure Destination Fuel temperature engine #1 Fuel temperature engine #2  APU Generator load Generator load engine #1 Generator load engine #2 ILS1 glideslope deviation ILS2 glideslope deviation Ground speed  Actual Gross Weight gross weight FAC Kg gross weight FAC Lbs Selected HPTC position engine #1 Selected HPTC position engine #2 HPTC demand #1 HPTC demand #2 Inertial altitude  APU IGV position ILS 1 frequency ILS 2 frequency Initial vertical speed K value for divergence (EGT or TN) computing

LATA LATG LATP LCDT LCIT LGDW LOC LONA LONG LONP LOPP LPT MFDI MH MN MN3 MW1 MW2 MW3 MW4 MW5 N1

Lateral acceleration body lateral acceleration Present position latitude system 1 Present position latitude system 2  APU Bleed air temperature  APU Load compressor inlet temperature LGCIU discrete word #2 ILS1 localizer deviation ILS2 localizer deviation Longitudinal acceleration body longitudinal acceleration Present position longitude System 1 Present position longitude System 2 Left brake pedal angle Selected LPTC position engine #1 Selected LPTC position engine #2 FDIU maintenance word Magnetic heading Mach Mach 3 ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word ECU Maintenance data word

#1 #1 #2 #2 #3 #3 #4 #4 #5 #5

engine engine engine engine engine engine engine engine engine engine

N1 actual low rotor speed engine #1 N1 actual low rotor speed engine #2

#1 #2 #1 #2 #1 #2 #1 #2 #1 #2

N1C N1F N1K N1L N1MX N1R N2 N2F N2K NA NAI NPA NRA NSVC NWSA OIP OIQ OIQH OIT

N1 command engine #1 N1 command engine #2 N1 Actual (low rotor speed) engine #1 N1 Actual (low rotor speed) engine #2 N1 corrected left N1 corrected right N1 limit engine #1 N1 limit engine #2 N1 maximun engine #1 N1 maximun engine #2 N1 left rate N1 right rate N2 actual (high rotor speed) engine #1 N2 actual (high rotor speed) engine #2 N2 actual high rotor speed engine #1 N2 actual high rotor speed engine #2 N2 corrected left N2 corrected right  APU RPM Nacelle anti-ice engine #1 open Nacelle anti-ice engine #2 open  APU RPM at APU EGT peak during APU start NWS reference angle current servo valve NWS NWS angle OIL pressure engine #1 OIL pressure engine #2 OIL quantity engine #1 OIL quantity engine #2 OIL consumption from the previous flight Eng.#1 OIL consumption from the previous flight Eng.#2 OIL temperature engine #1

OTA OVP PO P2 P25 P2A P3 PB PBV PCSW PD PDC PF PFAD PH PHA PHT PS13 PSB

OIL temperature engine #2  APU OIL sum temperature Outflow valve position Selected PO (Ambient pressure) engine #1 Selected PO (Ambient pressure) engine #2 PT2 (FAN inlet pressure) engine #1 PT2 (FAN inlet pressure) engine #2 P2.5 (Low Pressure Compressor exit pressure) #1 P2.5 (Low Pressure Compressor exit pressure) #2  APU inlet pressure Pb burner pressure engine #1 Pb burner pressure engine #2 Pb burner pressure engine #1 Pb burner pressure engine #2 Pack bypass valve position system #1 Pack bypass valve position system #2 Press control bus:Status + Fault info Precooler inlet pressure engine #1 Precooler inlet pressure engine #2 Cabin differential pressure Pack flow system #1 Pack flow system #2  APU:Performance adjustments Flight phase to display N1 phase unbalance brg1 engine #1 N1 phase unbalance brg1 engine #2 N1 phase unbalance TRF engine #1 N1 phase unbalance TRF engine #2 PS13 (FAN exit pressure) engine #1 PS13 (FAN exit pressure) engine #2 No4 bearing pressure engine #1 No4 bearing pressure engine #2

PSEL PSW1 PT PT2 PTCH PTCR

Status of different FADEC sensor engine #1 Status of different FADEC sensor engine #2 Discrete data word (Label 062) of pack #1 Discrete data word (Label 062) of pack #2 Bleed air pressure PT2 (FAN inlet pressure) engine #1 PT2 (FAN inlet pressure) engine #2 Pitch angle Body axis pitch rate

RUDD RUDT

Rotor active clearance control position Eng. #1 Rotor active clearance control position Eng. #2 Radio height (R/A1) Radio height (R/A2) Pack ram inlet position LH Pack ram inlet position RH Pack ram outlet position LH Pack ram outlet position RH ROLL angle Body axis roll rate Right brake pedal angle Reference speed command channel LH spoiler #2 position RH spoiler #2 position LH spoiler #3 position RH spoiler #3 position LH spoiler #4 position RH spoiler #4 position LH spoiler #5 position RH spoiler #5 position Rudder position Rudder trim

SAT

Static air temperature

RAC RALT RI RO ROLL ROLR ROPP RSCC RSP2 RSP3 RSP4 RSP5

SC1 SC2 SC3 SCC SCFD SDS1 SDS2 SLAT SLP SM SSEL1 SSEL2 SSEL3 SSEL4 STA STA01 STA02 STAB STVC STVO SV SW1 SW2 SW3

Selected ckpt compt temp Sel fwd cab compt temp Sel aft cab compt temp steering command captain steering command F/0 SDAC discrete word #1 SDAC discrete word #2 SLAT actual position system #1 SLAT actual position system #2 Estimd sideslip (side slip angle) system #1 Estimd sideslip (side slip angle) system #2  Autostart sequence in progress engine #1  Autostart sequence in progress engine #2 Status of different FADEC sensor: part 1 Status of different FADEC sensor: part 2 Status of different FADEC sensor: part 3 Status of different FADEC sensor: part 4  APU start time Stability status for report 01 monitoring Stability status for report 02 monitoring Stabilizer position #1 Scavenge valve stuck closed engine #1 Scavenge valve stuck closed engine #2 Scavenge valve stuck open engine #1 Scavenge valve stuck open engine #2 Starter air valve open (local switch) engine #1 Starter air valve open (local switch) engine #2 ECU Discrete status word #1 engine #1 ECU Discrete status word #1 engine #2 ECU Discrete status word #2 engine #1 ECU Discrete status word #2 engine #2 ECU Discrete status word #3 engine #1

SW4 SW5 T12 T25 T3 T5 TAIL1 TAIL2 TAT THDG TLA TN TNR TO TP TPO TR TW

ECU Discrete status word #3 engine #2 ECU Discrete status word #4 engine #1 ECU Discrete status word #4 engine #2 ECU Discrete status word #5 engine #1 ECU Discrete status word #5 engine #2 T12 (Fan inlet temperature) engine #1 T12 (Fan inlet temperature) engine #2 T2.5 (LPC exit) engine #1 T2.5 (LPC exit) engine #2 T3 (HPCexit) engine #1 T3 (HPCexit) engine #2 T5 (LPT exit) engine #1 T5 (LPT exit) engine #2  A/C ident word #1 (DMU computed)  A/C ident word #2 (DMU computed) Total air temperature TRUE HEADING system #1 TRUE HEADING system #2 Selected TLA angle Eng.#1 Selected TLA angle Eng.#2 Nacelle temperature engine #1 Nacelle temperature engine #2 delta TN reference value in climb Destination Pack outlet temperature LH Pack outlet temperature RH Precooler eng #1 outlet temperature Precooler eng #2 outlet temperature 4 T/R Doors (stowed and locked+deployed) Eng #1 4 T/R Doors (stowed and locked+deployed) Eng #2 Pack water extr. temperature LH Pack water extr. temperature RH

UTC

UTC (Universal time coordinated)

V3 V4 VA VACC VB1

VW

V3 (min speed flaps retracted ) V4 (min speed slats retracted ) CAB temp reg vlv pos group 3 Vertical acceleration N1 vibration eng #1 N1 vibration eng #2 N2 vibration eng #1 N2 vibration eng #2 Selected VBV position #1 Selected VBV position #2 Displace unbalance TRF (LPT) engine #1 Displace unbalance TRF (LPT) engine #2 CAB temp reg vlv pos group 1 N2 veloc unbalance BRG1 (HPC) engine #1 N2 veloc unbalance BRG1 (HPC) engine #2 TRF pick up N1 track vibration engine #1 TRF pick up N1 track vibration engine #2 VLS (Min. airspeed) Vman (maneuvering speed ) V Max (Max. allowable airspeed) Displace unbalance BRG1 or TRF engine #1 Displace unbalance BRG1 or TRF engine #2 VOR 1 frequency VOR 1 frequency Normal acceleration body normal acceleration Cabin v/s Selected VSV position (VSV) engine #1 Selected VSV position (VSV) engine #2 CAB temp reg viv pos group 2

WAI

LH wing anti ice valve closed system #1

VB2 VBV VC VF VH VL VLS VMAN VMAX VN VORF VRTA VRTG VSCB VSV

WARN WB WD WFQ WS WS1 WS2 WS3 WS4

RH wing anti ice valve closed system #2 FWC Discrete status word (Label=1 26 SDI=00)  APU bleed air flow WIND DIRECTION true system #1 WIND DIRECTION true system #2 Fuel quantity LH inner cell system #1 Fuel quantity LH inner cell system #2 WIND SPEED system #1 WIND SPEED system #2 wheel 1 speed wheel 2 speed wheel 3 speed wheel 4 speed

YAW

Body axis YAW rate

ZCB ZDW1 ZLD

Cabin altitude Discrete data word(Label 060) Zone Controller bus2 Landing elevation