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Splat
27th Oct 2004, 16:49
Horrible name I know, but does anyone have a list of parameter alpha codes, or some idea where to get a list?

I have seen one, and would like my own copy..... too much time in the cruise.

Cheers

Splat

woderick
27th Oct 2004, 22:16
Should be able to do something - I'll respond again after the weekend (next visit to work and the books) unless someone beats me to it !

woderick
2nd Nov 2004, 06:33
Have you had a response yet as suggested by ASFKAP if not I now have available as a Word Doc. PM your e-mail for a copy.

idg
2nd Nov 2004, 10:57
Woderick,
Could you PM one to me please...many thanks!
idg

woderick
2nd Nov 2004, 16:23
idg
I don't know if I can, can't see a way do what the others are doing PM your e-mail and I'll send it.

IFixPlanes
3rd Nov 2004, 10:57
Some Alpha Call Ups are exclusive for IAE-, CFM-Engines, A319, A320 or A321 and so dosnīt work on all A/Cs.
Also Software Configuration can Inhibit some call ups.


################################
ALPHA PARAMETER

ACID TAIL NUMBER
ACTYP A/C Type (DMU computed)
ACW1 APU CONTROL WORD #1
ACW2 APU CONTROL WORD #2
ACW3 APU CONTROL WORD #3
ACW4 APU CONTROL WORD #4
ACYC APU STRT CYC COMPUTED
ACYI START CYCLES (APU)
ADW1 DISCRETE STATUS WORD #1 (APU)
AHRI OPERATING HOURS (APU) hrs
AHRS APU OP HRS COMPUTED (APU)
AIL AILERON POSITION LH + RH
AILL AILERON POSITION LH
AILR AILERON POSITION RH
ALT ALTITUDE (1013.25mb) ft
ALT3 ALTITUDE (1013.25mb) ft
ALTR ALTITUDE RATE (VZBI) ft/sec
AMW1 MAINTENANCE WORD #1 (APU)
AMW2 MAINTENANCE WORD #2 (APU)
AMW3 MAINTENANCE WORD #3 (APU)
AOA CORRECTED ANGLE OF ATTACK Deg
AOA3 CORRECTED ANGLE OF ATTACK Deg
AP AP Status
APLAT A/P lateral mode
APLON A/P longitudinal mode
ASN APU SERIAL NUMBER
BLST Bleed status
BAF 2.5 Bleed actuator feedback engine %
BNR SELECTED AIR SPEED Kts
SELECTED VERTICAL SPEED Ft/min
SELECTED MACH Mach
FLEX T.D.TEMP. Deg C
BP1 brake 1 pressure BAR
BP2 brake 2 pressure BAR
BP3 brake 3 pressure BAR
BP4 brake 4 pressure BAR
BT1 Brake 1 temperature DEGC
BT2 Brake 2 temperature DEGC
BT3 Brake 3 temperature DEGC
BT4 Brake 4 temperature DEGC
BVP ENG SCAVENGE VLV OPEN
CAS COMPUTED AIRSPEED Kts
CAS3 COMPUTED AIRSPEED Kts
CFPG Calculated flight path acceleration system
CG LONG CENTER OF GRAVITY %
CIVV Calculated inertial vertical speed system
CNT Report count + previous report number
COT PACK COMPR. OUTLET TEMP. Deg C
CSV1 current SVN1 MA
CSV2 current SVN2 MA
CSV3 current SVN3 MA
CSV4 current SVN4 MA
DA DRIFT ANGLE Deg
DATE GMT date
DMEF DME 1 frequency MHz
DMU DMU software version
DSW1 BSCU discrete status word 1
DSW2 BSCU discrete status word 2
DSW3 BSCU discrete status word 3
ECW1 ENGINE CONTROL WORD #1
ECW2 ENGINE CONTROL WORD #2
ECW3 ENGINE CONTROL WORD #3
ECW4 ENGINE CONTROL WORD #4
ECW5 ENGINE CONTROL WORD #5
ECYC Start cycles Engine
EECD1 EEC Discrete status word #1 engine
EECD2 EEC Discrete status word #2 engine
EECD3 EEC Discrete status word #3 engine
EECD7 EEC Discrete status word #7 engine
EECD8 EEC Discrete status word #8 engine
EECM2 EEC Maintenance data word #2 engine
EECM6 EEC Maintenance data word #6 engine
EGT Selected T49.5 - EGT ACTUAL
EGTA EGT (APU) Deg C
EGTF EGT LPT exit temp engine :Filtered parameter DEGC
EGTK EGT corrected (DMU computed)
EGTP EGT APU PEAK
EGTR EGT REFERENCE PH 5.1
EHRS Flight Hours Eng
ELEV ELEVATOR POSITION Deg
ENGFA A/C type engine
ENTYP Engine type (DMU computed)
EPR EPR actual engine #1
EPRC EPR command engine
EPRT EPR Take Off engine
EPRTG Target EPR (echo) (send by AT) engine
ERT ENGINE RUNNING TIME hrs
ESN ENGINE S/N
ESN1 Engine serial number (First half) engine #1
ESN2 Engine serial number (First half) engine #2
EVM EVM DISCRETE WORD ENG
F319 FLAP actual position left for A319 DEG
F320 FLAP actual position left for A320 DEG
F321 FLAP actual position left for A321 DEG
FD Fuel density left 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 FLOW pph
FFK Fuel flow corrected engine
FLAP FLAP ACTUAL POSITION Deg
FLAPW FLAP actual position switched DEG
FLCNT Flight counter
FLNUM Flight number (DMU computed)
FLT Flight number (DMU computed)
FM Flight phase to display (DMU computed)
FMB Flight phase broadcasted to ACARS(DMU computed)
FMF FWC Flight phases
FMGD1 FMGC discrete status word #1
FMGD2 FMGC discrete status word #2
FMGD4 FMGC discrete status word #4
FMI Internal flight phase (DMU computed)
FMV SELECTED FMV POSITION %
FPA FLIGHT PATH ANGLE Deg
FPAC FLIGHT PATH ACCEL g
FPPU FLAP actual position (FPPU angle value) DEG
FROM Departure (DMU computed)
FRTO CITY PAIR FROM/TO
FT FUEL TEMPERATURE C
GLA APU GEN LOAD %
GLE GEN LOAD %
GLS ILS GLIDESLOPE DEVIATION DDM
GS GROUND SPEED Kts
GV APU IGV position
GW GROSS WEIGHT (1bs) lbs
GWFK GROSS WEIGHT FAC (kg)
GWFL GROSS WEIGHT FAC (lbs)
HPT SELECTED HPTC POSITION %
HPTC HPTC DEMAND %
IALT Inertial altitude FEET
IGV IGV POSITION (APU) Deg
ILS ILS frequency MHz
INST CONFIGURATION WORD
IVV INERTIAL VERTICAL SPEED ft/sec
K Actual K for Diverg. Rep.
LATA LATERAL ACCEL . G
LATG BODY LATERAL ACCEL. G
LATP PRESENT POSITION LATITUDE Deg
LCDT BLEED AIR TEMP (APU) Deg C
LCIT LOAD COMPRESSOR INLET Deg C
LGDW LGCIU DISCRETE WORD #2
LOC ILS LOCALIZER DEVIATION DDM
LONA LONGITUDINAL ACCEL. G
LONG BODY LONGITUDINAL ACCEL. g
LONP PRESENT POSITION LONGITUDE Deg
LOPP BRAKE PEDAL POSITIONANGLE DEG
LPT SELECTED LPTC POSITION %
MDMU MAINTENANCE WORD #1
MFDI MAINTENANCE WORD #1
MH MAGNETIC HEADING Deg
MN MACH Mach
MN3 MACH Mach
MW1 MAINTENANCE DATA #1
MW2 MAINTENANCE DATA #2
MW3 MAINTENANCE DATA #3
MW4 MAINTENANCE DATA #4
MW5 MAINTENANCE DATA #5
MW6 MAINTENANCE DATA #6
MW7 MAINTENANCE DATA #7
MW8 MAINTENANCE DATA #8


end Part one

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Part two

N1 Actual (low rotor speed) engine %RPM
N1C N1 COMMAND % rpm
N1F N1 Actual (low rotor speed) engine (Filtered Parameter)
N1K N1 corrected left (DMU computed)
N1L N1 LIMIT % rpm
N1MX N1 MAXIMUM % rpm
N1R N1 RATE %RPM
N2 N2 Actual (high rotor speed) engine %RPM
N2F N2 Actual (high rotor speed) engine :Filtered
N2K N2 corrected left (DMU computed)
NA RPM APU % rpm
NAI Nacelle anti-ice engine open
NPA N APU PEAK
NRA NWS reference angle DEG
NSVC current servo valve NWS MA
NWSA NWS angle DEG
OIK Oil quant corrected Eng Quart
OIP ENG OIL PRESSURE PSI
OIQ ENG OIL QUANTITY Quart
OIQH Oil consumpt prev. flight eng Quart/Hour
OIT ENG OIL TEMPERATURE Deg C
OTA APU OIL SUMP TEMP Deg C
OVP OUTFLOW VALVE POS %
P125 P12.5 (FAN exit pressure) engine PSIA
P2 PT2 (FAN inlet pressure) engine PSIA
P25 P25 (LPC EXIT PRESSURE) psia
P2A INLET PRESSURE (APU) bar
P3 PB BURNER PRESSURE psia
P49 Low Pressure Turbine exit pressure engine PSIA
PB Pb burner pressure engine PSIA
PB10 P10 engine PSIA
PBV PACK BYPASS VALVE POSITION %
PCSW STATUS + FAULT INFO
PD PRECOOLER ENG 2 INLET PRESS PSI
PDC CABIN DIFF. PRESS PSI
PF PACK FLOW kg/sec
PFAD PERFORMANCE ADJUSTMENTS (APU)
PH Flight Phase (DMU)
PHA N 1 PHASE OF UNBALANCE ENG Deg
PHT N1 phase unbalance TRF engine DEG
PO SELECTED PO psia
PS13 PS13 (FAN EXIT PRESSURE) psia
PSB ENG no 4 bearing pressure psia
PSEL Status of different FADEC sensor engine
PSW1 DISCRETE DATA WORD
PT BLEED AIR PRESSURE (APU) bar
PT2 PT2 (FAN INLET PRESSURE) psia
PTCH PITCH ANGLE Deg
PTCR BODY AXIS PITCH RATE Deg/sec
RAC ROT. ACT. CLEAR. CONTR. %
RALR RADIO ALTITUDE RATE
RALT RADIO HEIGHT (R/A) ft
RI PACK RAM AIR INLET POSITION %
RO PACK RAM AIR OUTLET POSITION %
ROLL ROLL ANGLE Deg
ROLR BODY AXIS ROLL RATE Deg/sec
ROPP Right brake pedal angle DEG
RSCC reference speed command channel KTS
RSP2 SPL 2 POSITION Deg
RSP3 SPL 3 POSITION Deg
RSP4 SPL 4 POSITION Deg
RSP5 6C 1 365 01 DEG LH spoiler #5 position
RUDD RUDDER POSITION Deg
RUDT RUDDER TRIM Deg
SAT STATIC AIR TEMPERATURE (BNR) Deg C
SC1 SELECTED CKPT COMPT TEMP Deg C
SC2 SELECTED FWD CAB COMPT TEMP Deg C
SC3 SELECTED AFT CAB COMPT TEMP Deg C
SCC steering command captain DEG
SCFD steering command F/0 DEG
SDMU DMU STATUS WORD
SDS1 DISCRETE STATUS WORD
SDS2 DISCRETE STATUS WORD
SLAT SLAT ACTUAL POSITION Deg
SLP Estimd Sideslip Deg
SM Autostart sequence in progress
SSEL1 Status of different FADEC sensor: part 1
SSEL2 Status of different FADEC sensor: part 2
SSEL3 Status of different FADEC sensor: part 3
SSEL4 Status of different FADEC sensor: part 4
STA APU START TIME
STA01 Stability status for report 01 monitoring
STA02 Stability status for report 02 monitoring
STAB STABILIZER POSITION Deg
STVC Scavenge valve stuck closed engine
STVO Scavenge valve stuck open engine
SV Starter air valve open (local switch) engine
SVA SVA (stator vane actuator feedback) engine %
SW1 ECU STATUS WORD #1
SW2 ECU STATUS WORD #2
SW3 ECU STATUS WORD #3
SW4 ECU STATUS WORD #4
SW5 DISCRETE STATUS WORD #5
SW6 ECU Discrete status word #6 engine
SW7 ECU Discrete status word #7 engine
SW8 ECU Discrete status word #8 engine
SW9 ECU Discrete status word #9 engine
T12 T12 (FAN INLET TEMP) Deg C
T25 T25 (LPC EXIT TEMPERATURE) Deg C
T2 T2 (FAN inlet temp) engine DEGC
T3 HPC EXIT TEMPERATURE Deg C
T5 T5 (LPT EXIT TEMP) Deg C
TAIL1 A/C ident word #1 (DMU computed)
TAIL2 A/C ident word #2 (DMU computed)
TAT TOTAL AIR TEMPERATURE (BNR) Deg C
THDG TRUE HEADING Deg
TLA SELECTED TLA Deg
TN ENG NACELLE TEMPERATURE Deg
TNR TN REFERENCE PH 5.1 Deg C
TO Destination (DMU COMPUTED)
TP PACK OUTLET TEMPERATURE Deg C
TPO PRECOOLER ENG OUTLET TEMP Deg C
TR 4 T/R Doors (stowed and locked+deployed)
TRA TRA (Throttle resolver angle)
TRP Thrust reserver pos.
TW PACK WATER EXTR. TEMPERATURE Deg C
UTC UTC (UNIVERSAL TIME hour/min/sec
V3 V 3 (MIN SPEED FLAPS RETR.) Kts
V4 V 4 (MIN SPEED SLATS RETR.) Kts
VA CAB TEMP REG VLV POS GROUP 3 %
VACC VERTICAL ACCEL g
VB1 N1 VIBRATION ENG
VB2 N2 VIBRATION ENG
VBV SELECTED VBV POSITION Deg
VC Displace unbalance TRF (LPT) eng IPS
VF CAB TEMP REG VLV POS GROUP 1 %
VH N2 veloc unbalance BRG1 (HPC)engine IPS
VL TRF pick up N1 track vibration engine MILS
VLS VLS (MIN AIRSPEED) Kts
VMAN V Man (MANEUVERING SPEED) Kts
VMAX V Max (MAX.ALLOW.AIRSPEED) Kts
VN Displace unbalance BRG1 or TRF engine MILS
VORF VOR frequency MHz
VRTA Normal acceleration G
VRTG BODY NORMAL ACCEL g
VSCB CABIN V/S ft/min
VSV SELECTED VSV POSITION Deg
VW CAB TEMP REG VLV POS GROUP 2 %
WAI wing anti ice valve closed
WARN DISCRETE STATUS WORD
WB BLEED AIR FLOW (APU) Kg/sec
WD WIND DIRECTION - TRUE Deg
WFQ FUEL QUANTITY - INNER CELL Lbs
WS WIND SPEED Kts
WS1 wheel 1 speed
WS2 wheel 2 speed
WS3 wheel 3 speed
WS4 wheel 4 speed
YAW BODY AXIS YAW RATE Deg/sec
ZCB CABIN ALTITUDE ft
ZDW1 DISCRETE DATA WORD
ZLD LANDING ELEVATION ft


################################################

HIH

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And Then
3rd Nov 2004, 13:34
IFix
Appreciate that effort!

A-3TWENTY
4th Nov 2004, 10:36
And you have to know all of them by heart....:8 :8 :8

Splat
5th Nov 2004, 10:41
Many thanks for that.

I was hoping that GPS Time would be in there, but I don't see it.

Splat

woderick
5th Nov 2004, 14:25
I need to confirm, I don't have 320 schematics at home for a GPS equipped A/C, but on a GPS equipped 330 the time on the clock, and displayed by the aids parameter UTC is GPS derived time.
I expect the GPS equipped 320 to be the same.

Splat
5th Nov 2004, 14:54
Re the clock, my understanding is that is true only for the later model clocks.

woderick
7th Nov 2004, 21:49
I have now looked at the schematics for all the aircraft that I have access to. These range from a MSN in the 400s to some in the 2000s and, without exception, when fitted with GPS then the clock uses GPS system time as it's input.

Now I'm not saying that this will be the case for all 320s fitted with GPS, that's what options are for, but Airbus are less free with their options and differences than that other manufacturer.

It seems to me that it is logical to use the best time source available and if you have GPS then that's it.

Sick Squid
8th Nov 2004, 08:25
I use the SC1/2/3 Alpha commands a lot in cruise; checks the 'dialed' cockpit/cabin temperature against the actual zone temperature.

Thanks for the complete list, IFP. Am I right in thinking that the LGDW (LGCIU Discrete Word2) prompt will return an answer of air/ground mode? Just that the multitude of failures that can arise with a failure of that mode in the air are so many and disconcerting that it would be nice to keep a simple resolution of that issue in the back pocket just in case... yeah, I know it would be a very busy little cockpit if it happened, just thinking out loud really, and remembering the nightmare checklist on the 777 (a few years ago, at least) if there was a confusion between the modes.

Squid

IFixPlanes
8th Nov 2004, 14:08
@ Sick Squid
I will try to find out more about the LGDW. But it might take some time because we normally we donīt use
the "Discrete Word" so often.

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