Ata 31 Alpha Call Up

Explanations to the Parameter List The parameter list is organized according to the connected ARINC 429 data buses. The connected systems (e.g. FAC, ECU, EEC, etc.) and the corresponding ATA chapter numbers are stated in the header on the left side of each page of the parameter lists. The columns are described as follows: -------------------------------------------------------------------Column | Description -------------------|-----------------------------------------------1st | EQ.SYS.LAB.SDI = Parameternumber SYS.LAB.SDI | | System number: According to the system which is | sending out the corresponding parameter: | 1 for system one | 2 for system two | 3 for system three | Label of the parameter, octal value | according to ARINC 429. | SDI states the Source/Destination Identifier | which is used by the system for the | corresponding parameter: | 00 means SDI 00 (0) | 01 means SDI 01 (1) | 10 means SDI 10 (2) | 11 means SDI 11 (3) -------------------|-----------------------------------------------2nd | PARAMETER PARAMETER | Parameter Name -------------------|-----------------------------------------------3rd | RANGE RANGE | | Three different types of ranges are shown in | this column: | The first one, indicated by a W (WORDRANGE), | is related to the ARINC 429 data bus. This | shows the maximum value of the parameter that

-------------------------------------------------------------------Column | Description -------------------|-----------------------------------------------| can be transferred on the bus. This | depends on the number of data bits (see | column DATA BITS) and the resolution (R) of | the parameter (see column ACCURACY). | The second one, with no specific indication, | shows the normal operational range of the | parameter. | The third one is related to the ARINC 429 | Discrete Data Words. There are two states: | bit status 0 or bit status 1. They | indicate the true condition of the | corresponding data word bit position.

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-------------------|-----------------------------------------------Column | Description -------------------|-----------------------------------------------4th | ACCURACY ACCURACY | Two different types of values are shown | in this column: | The first one, indicated with an R | (RESOLUTION) is related to the ARINC | 429 data bus. It also shows the | resolution of the data word. The second | one, with no specific indication, shows | the total accuracy of the parameter. -------------------|-----------------------------------------------5th | SIGN BIT SIGN BIT | | This column shows whether a sign bit | is available and in which bit position | of the data word it is situated. -------------------|-----------------------------------------------6th | DATA BITS DATA BITS | | Describes the number of data bits not | including the sign bit. A and a number | means the discrete bit position in the | ARINC 429 data word. | For BCD coded data words the number of | significant data digits is shown, | indicated by (1).

-------------------|-----------------------------------------------Column | Description -------------------|-----------------------------------------------7th | UPD/s UPD/s | | This column shows how many times the | parameter will be transmitted by the source | system. -------------------|-----------------------------------------------8th | CODE CODE | | BNR = binary data word | BCD = binary coded decimal data word | ISO = data word coded in ISO 5 Code | DIS = discrete data word | HEX = hexadecimal coded | OCT = octal coded | HYB = mixed code; | e.g. : bit 11 to 16 DIS | bit 17 to 28 BNR -------------------|-----------------------------------------------9th | ALPHA CODING ALPHA CODING | | This column shows the mnemonic for the | parameter (if available). By entering | this code via the MCDU, the current | parameter-value will be shown on the | display. The value from both systems | (if available) will be shown. -------------------|-----------------------------------------------10th | This column shows the source origin, its Source | bus number, ATA Ref., and its label. EQPT | BUS NR | ATA. REF | CONV | -------------------|------------------------------------------------

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F. Parameter List NOTE : Each set of parameters is in the applicable chapter. ____

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-------------------------------------------------------EQ | SYSTEM | CHAPTER ---|------------------------------------|--------------0A | FAC 1 & 2 | 22-66-00 7C | ECU 1 & 2 | 73-25-00 1B | SFCC 1 & 2 | 27-51-00 23 | GPWS | 34-48-00 26 | FWC 1 & 2 | 31-52-00 6E | BSCU (optional) | 32-42-00 7A | ECB APU | 49-61-00 6C | FCDC 1 & 2 | 27-95-00 04 | ADIRU (IRS PART) 1 & 2 & 3 | 34-14-00 06 | ADIRU (ADC PART) 1 & 2 & 3 | 34-13-00 01 | FMGC (FGC PART) 1 & 2 | 22-86-00 02 | FMGC (FMC PART) 1 & 2 | 22-86-00 5D | ZONE CONTROLLER | 21-63-00 8E | PACK CONTROLLER LH/RH | 21-61-00 5C | PRESSURE CONTROLLER 1 & 2 | 21-30-00 6F | BMC 1 & 2 | 36-11-00 25 | DMC 1 & 2 | 31-62-00 5A | FQIS | 28-42-00 6D | LGCIU 1 & 2 | 32-61-00 29 | SDAC 1 & 2 | 31-54-00 3D | EVM | 77-30-00 A1 | FCU | 22-81-00 7E | CFDIU | 31-32-00 17 | FDIU | 31-33-00 39 | MCDU | 22-82-00 40 | PRINTER | 31-35-00 -------------------------------------------------------OD | DMU | 31-37-00 --------------------------------------------------------

G. Parameter List +-----------------------------------------------------------------------------+ | PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) | |-----------------------------------------------------------------------------| |EQ.SYS.LAB.SDI| PARAMETER | RANGE |SIGN|DATA|UPD/|CODE|ALPHA| | | DEFINITION | ACCURACY |BIT |BITS|SEC | |CODE | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.172.-| System Address | | | | | | | | | Label (SAL) | | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.220.| MCDU 1 DATA | File Data | | 23 | 1 | ISO| | | | Label *1| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.221.| MCDU 2 DATA | File Data | | 23 | 1 | ISO| | | | Label *1| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.222.| MCDU 3 DATA | File Data | | 23 | 1 | ISO| | | | Label *1| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.223.| Printer Label | File Data | | 23 | 1 | ISO| | | | *1| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.226.| MDDU Data | File Data | | 23 | 1 | ISO| | | | *2| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.304.| ACARS Data | File Data | | 23 | 1 | ISO| | | | *3| Transfer | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| |0D.1.350.00 | Maintenance | | | 4 | 2 | DIS|MDMU | | | Word # 1 *1| | | | | | | | |-----------------|------------------|----|----|----|----|-----| | | DMU FAIL | bit status 1 | | #11| | | | | |-----------------|------------------|----|----|----|----|-----| | | DAR FAIL | bit status 1 | | #12| | | | | |-----------------|------------------|----|----|----|----|-----| | | DAR Tape Low | bit status 1 | | #13| | | | | |-----------------|------------------|----|----|----|----|-----| | | DAR Manual On | bit status 1 | | #14| | | | | |-----------------|------------------|----|----|----|----|-----| | | DAR On | bit status 1 | | #15| | | | | |-----------------|------------------|----|----|----|----|-----| | | PCMCIA FAIL | bit status 1 | | #16| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #17| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #18| | | |



+-----------------------------------------------------------------------------+ | PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) | |-----------------------------------------------------------------------------| |EQ.SYS.LAB.SDI| PARAMETER | RANGE |SIGN|DATA|UPD/|CODE|ALPHA| | | DEFINITION | ACCURACY |BIT |BITS|SEC | |CODE | |--------------|-----------------|------------------|----|----|----|----|-----| | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #19| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #20| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #21| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #22| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #23| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #24| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #25| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #26| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #27| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #28| | | | | |-----------------|------------------|----|----|----|----|-----| | | SPARE | | | #29| | | | |--------------|-----------------|------------------|----|----|----|----|-----| | 0D.1.356.00 | Maintenance | | | | | | | | | Message *1| | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| | 0D.1.377.00 | Equipment *1| bits: | |2(1)| 2 | HEX| | | | Identification | 11-14 low part | | | | | | | | | 15-18 high part | | | | | | | | | 19-29 logic 0 | | | | | | |--------------|-----------------|------------------|----|----|----|----|-----| *1 = *2 = *3 = (1)=

Only DMU output bus A Only DMU output bus C Only DMU output bus B Significant Data Digits

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H. Alpha Call-up List Alpha Parameter Unit Comment ------------------------------------------------------------------------------ACTYP A/C Type (DMU computed) ACW1 APU control word #1 (DMU computed) ACW2 APU control word #2 (DMU computed) ACW3 APU control word #3 (DMU computed) ACW4 APU control word #4 (DMU computed) ACYC APU cycles (DMU computed) ACYI 7A 1 133 01 CYCLES APU start cycles ADW1 7A 1 037 01 APU:Discrete status word #1 AHRI 7A 1 132 01 H APU operating hours AHRS H APU hours (DMU computed) AIL 6C 1 310 01 DEG Aileron position left 6C 1 330 01 DEG Aileron position right AILL 6C 1 310 01 DEG Aileron position left 6C 2 310 10 DEG Aileron position left AILR 6C 1 330 01 DEG Aileron position right 6C 2 330 10 DEG Aileron position right ALT 06 1 203 01 FEET Altitude (1013.25mb) (switched parameter) 06 2 203 10 FEET Altitude (1013.25mb) (switched parameter) ALT3 26 1 203 11 FEET altitude 3 (1013.25 ha) ALTR 01 1 365 00 FT/MIN Altitude rate (VZBI) 01 2 365 00 FT/MIN Altitude rate (VZBI) AMW1 7A 1 353 01 APU:Maintenance word #l AMW2 7A 1 351 01 APU:Maintenance word #2 AMW3 7A 1 352 01 APU:Maintenance word #3 AOA 06 1 241 01 DEG Corrected angle of attack system #l 06 2 241 10 DEG Corrected angle of attack system #2 A0A3 26 1 241 11 DEG Corrected angle of attack 3 AP Auto pilot status (AP) left Auto pilot status (AP) right APLAT A/P lateral mode left A/P lateral mode right APLON A/P longitudinal mode left A/P longitudinal mode right ASN 7A 1 050 01 APU serial number BAF 7C 1 335 01 % 2.5 Bleed actuator feedback engine #1 7C 2 335 10 % 2.5 Bleed actuator feedback engine #2 BP1 6E 1 300 01 BAR brake 1 pressure 6E 2 300 10 BAR brake 1 pressure BP2 6E 1 301 01 BAR brake 2 pressure 6E 2 301 10 BAR brake 2 pressure BP3 6E 1 302 01 BAR brake 3 pressure 6E 2 302 10 BAR brake 3 pressure

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------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------BP4 6E 1 303 01 BAR brake 4 pressure 6E 2 303 10 BAR brake 4 pressure BT1 6E 1 114 01 DEGC Brake 1 temperature 6E 2 114 10 DEGC Brake 1 temperature BT2 6E 1 115 01 DEGC Brake 2 temperature 6E 2 115 10 DEGC Brake 2 temperature BT3 6E 1 116 01 DEGC Brake 3 temperature 6E 2 116 10 DEGC Brake 3 temperature BT4 6E 1 117 01 DEGC Brake 4 temperature 6E 2 117 10 DEGC Brake 4 temperature BVP 26 1 031 01 Scavenge valve open engine #1 26 1 031 10 Scavenge valve open engine #2 CAS 06 1 206 01 KTS Computed air speed (switched parameter) 06 2 206 10 KTS Computed air speed (switched parameter) CAS3 26 1 206 11 KTS calibrated air speed 3 CFPG Calculated flight path acceleration system #1 CG 02 1 077 00 %MAC Calculated flight path acceleration system #2 02 2 077 00 %MAC Long center of gravity (switched parameter) CIVV Calculated inertial vertical speed system #1 Calculaied inertial vertical speed system #2 CNT report count COT 8E 1 123 11 DEGC Pack compr. outlet temperature LH 8E 2 123 00 DEGC Pack compr. outlet temperature RH CSV1 6E 1 310 01 MA current SVN1 6E 2 310 10 MA current SVN1 CSV2 6E 1 311 01 MA current SVN2 6E 2 311 10 MA current SVN2 CSV3 6E 1 312 01 MA current SVN3 6E 2 312 10 MA current SVN3 CSV4 6E 1 313 01 MA current SVN4 6E 2 313 10 MA current SVN4 DA 04 1 321 01 DEG Drift angle 04 2 321 10 DEG Drift angle DATE 17 1 260 00 GMT date DMEF 25 1 035 01 MHz DME 1 frequency 25 1 035 10 MHz DME 2 frequency DSW1 6E 1 270 01 BSCU discrete status word 1 6E 2 270 10 BSCU discrete status word 1 DSW2 6E 1 026 01 BSCU discrete status word 2 6E 2 026 10 BSCU discrete status word 2 DSW3 6E 1 027 01 BSCU discrete status word 3 6E 2 027 10 BSCU discrete status word 3 ECW1 Engine #1 control word #1 Engine #2 control word #1



------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------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 (DMU computed) Engine # 2 cycles (DMU computed) EECD1 7C 1 270 01 EEC Discrete status word #1 engine #1 7C 2 270 10 EEC Discrete status word #1 engine #2 EECD2 7C 1 271 01 EEC Discrete status word #2 engine #1 7C 2 271 10 EEC Discrete status word #2 engine #2 EECD3 7C 1 272 01 EEC Discrete status word #3 engine #1 7C 2 272 10 EEC Discrete status word #3 engine #2 EECD7 7C 1 276 01 EEC Discrete status word #7 engine #1 7C 2 276 10 EEC Discrete status word #7 engine #2 EECD8 7C 1 145 01 EEC Discrete status word #8 engine #1 7C 2 145 10 EEC Discrete status word #8 engine #2 EECM2 7C 1 351 01 EEC Maintenance data word #2 engine #1 7C 2 351 10 EEC Maintenance data word #2 engine #2 EECM6 7C 1 155 01 EEC Maintenance data word #6 engine #1 7C 2 155 10 EEC Maintenance data word #6 engine #2 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) EPR 7C 1 340 01 EPR actual engine #1 7C 2 340 10 EPR actual engine #2 EPRC 7C 1 341 01 EPR command engine #1 7C 2 341 10 EPR command engine #2



------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------EPRT 7C 1 342 01 EPR Take Off engine #1 7C 2 342 10 EPR Take Off engine #2 EPRTG 7C 1 343 01 Target EPR (echo) (send by AT) engine #1 7C 2 343 10 Target EPR (echo) (send by AT) engine #2 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) FDR Fuel density right wing tank (DMU computed) FDRAW 5A 2 272 10 Fuel density FF 7C 1 244 01 PPH/KG Fuel mass flow rate engine #1 7C 2 244 10 PPH/KG Fuel mass flow rate engine #2 FFK Fuel flow corrected engine #1 Fuel flow corrected engine #2 FLAP DEG FLAP actual position left DEG FLAP actual position right FLAPW DEG FLAP actual position switched FLCNT Flight counter FLNUM Flight number (DMU computed) FM Flight phase to display (DMU computed) FMB Flight phase broadcasted to ACARS(DMU computed) FMF 26 1 126 01 FWC Flight phases 26 2 126 01 FWC Flight phases FMGD1 01 1 274 00 FMGC discrete status word #1 01 2 274 00 FMGC discrete status word #1 FMGD2 01 1 275 00 FMGC discrete status word #2 01 2 275 00 FMGC discrete status word #2 FMGD4 01 1 146 00 FMGC discrete status word #4 01 2 146 00 FMGC discrete status word #4 FMI Internal flight phase (DMU computed)



------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------FPA 04 1 322 01 DEG Flight path angle 04 2 322 10 DEG Flight path angle FPAC 04 1 323 01 G Flight path acceleration 04 2 323 10 G Flight path acceleration FPPU 1B 1 137 01 DEG FLAP actual position (FPPU angle value) 1B 2 137 10 DEG FLAP actual position (FPPU angle value) FROM Departure (DMU computed) FRTO ORIGIN Departure (DMU computed) Destination (DMU COMPUTED) FT 5A 2 177 10 DEGC Fuel temperature engine #1 5A 2 201 10 DEGC Fuel temperature engine #2 GLA 29 1 100 00 % APU Generator load 29 2 100 00 % APU Generator load GLE 29 1 077 01 % Generator load engine #1 29 1 077 10 % Generator load engine #2 GLS 25 1 174 01 DDM ILS1 glideslope deviation 25 1 174 10 DDM ILS2 glideslope deviation GS 04 1 312 01 KTS Ground speed 04 2 312 10 KTS Ground speed GW 02 1 075 00 10Kg Actual Gross Weight 02 2 075 00 10Kg Actual Gross Weight GWFK 0A 1 074 00 KG gross weight FAC (kg) 0A 2 074 00 KG gross weight FAC (kg) GWFL 0A 1 074 00 LBS gross weight FAC (lbs) 0A 2 074 00 LBS gross weight FAC (lbs) HPT 7C 1 330 01 % ACC feedback engine #1 7C 2 330 10 % ACC feedback engine #2 HPTC 7C 1 063 01 % HPTC demand #1 7C 2 063 10 % HPTC demand #2 IALT 04 1 361 FEET Inertial altitude 04 2 361 FEET Inertial altitude IGV 7A 1 130 01 DEG APU IGV position ILS 25 1 033 01 MHz ILS 1 frequency 25 1 033 10 MHz ILS 2 frequency IVV 04 1 365 01 FT/MIN Initial vertical speed 04 2 365 10 FT/MIN Initial vertical speed K K value for divergence (EGT or TN) computing LATA 29 1 332 01 G Lateral acceleration 29 2 332 01 G Lateral acceleration LATG 04 1 332 01 G body lateral acceleration 04 2 332 10 G body lateral acceleration LATP 04 1 310 Present position latitude system 1 04 2 310 Present position latitude system 2 LCDT 7A 1 074 01 DEGC APU Bleed air temperature



31-37-00

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------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------LCIT 7A 1 110 01 DEGC APU Load compressor inlet temperature LGDW 60 1 021 01 LGCIU discrete word #2 60 2 021 10 LGCIU discrete word #2 LOC 25 1 173 01 DDM ILS1 localizer deviation 25 1 173 10 DDM ILS2 localizer deviation LONA 29 1 331 01 G Longitudinal acceleration 29 2 331 01 G Longitudinal acceleration LONG 04 1 331 01 G body longitudinal acceleration 04 2 331 10 G body longitudinal acceleration LONP 04 1 311 DEG Present position longitude System 1 04 2 311 DEG Present position longitude system 2 LOPP 6E 1 331 01 DEG Left brake pedal angle 6E 2 331 10 DEG Left brake pedal angle MFDI 17 1 350 00 FDIU maintenance word MH 04 1 320 01 DEG Magnetic heading 04 2 320 10 DEG Magnetic heading MN 06 1 205 01 MACH Mach (switched parameter) 06 2 205 10 MACH Mach (switched Parameter) MN3 26 1 205 11 MACH Mach 3 MW1 7C 1 350 01 ECU Maintenance data word #1 engine #1 7C 2 350 10 ECU Maintenance data word #1 engine #2 MW2 7C 1 351 01 ECU Maintenance data word #2 engine #1 7C 2 351 10 ECU Maintenance data word #2 engine #2 MW3 7C 1 352 01 ECU Maintenance data word #3 engine #1 7C 2 352 10 ECU Maintenance data word #3 engine #2 MW4 7C 1 353 01 ECU Maintenance data word #4 engine #1 7C 2 353 10 ECU Maintenance data word #4 engine #2 MW5 7C 1 354 01 ECU Maintenance data word #5 engine #1 7C 2 354 10 ECU Maintenance data word #5 engine #2 MW6 7C 1 155 01 ECU Maintenance data word #6 engine #1 7C 2 155 10 ECU Maintenance data word #6 engine #2 MW7 7C 1 156 01 ECU Maintenance data word #7 engine #1 7C 2 156 10 ECU Maintenance data word #7 engine #2 MW8 7C 1 157 01 ECU Maintenance data word #8 engine #1 7C 2 157 10 ECU Maintenance data word #8 engine #2 N1 7C 1 346 01 %RPM Actual (low rotor speed) engine #1 7C 2 346 10 %RPM Actual (low rotor speed) engine #2 N1K N1K N1 corrected left (DMU computed) N1 corrected right (DMU computed) N2 7C 1 344 01 %RPM N2 Actual (high rotor speed) engine #1 7C 2 344 10 %RPM N2 Actual (high rotor speed) engine #2 N2F %RPM N2 Actual (high rotor speed) engine #1:Filtered %RPM N2 Actual (high rotor speed) engine #2:Filtered N2K N2 corrected left (DMU computed)

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31-37-00

------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------N2 corrected right (DMU computed) NA 7A 1 176 01 %RPM APU RPM NAI 50 2 061 10 Nacelle anti-ice engine #1 open 50 2 061 10 Nacelle anti-ice engine #2 open NPA %RPM APU RPM at APU EGT peak during APU start NRA 6E 1 334 01 DEG NWS angle 6E 2 334 10 DEG NWS angle NSVC 6E 1 335 01 MA current servo valve NWS 6E 2 335 10 MA current servo valve NWS NWSA 6E 1 334 01 DEG NWS angle 6E 2 334 10 DEG NWS angle OIP 26 1 317 01 PSI OIL pressure engine #1 26 1 317 10 PSI OIL pressure engine #2 OIQ 26 1 073 01 QUART OIL quantity engine #1 26 1 073 10 QUART OIL quantity engine #2 OIQH QTS/H OIL consumption from the previous flight Eng.#1 QTS/H OIL consumption from the previous flight Eng.#2 OIT 26 1 316 01 DEGC OIL temperature engine #1 26 1 316 10 DEGC OIL temperature engine #2 OTA 7A 1 247 01 DEGC APU OIL sum temperature OVP 5C 1 153 01 % Outflow valve position 5C 2 153 10 % Outflow valve position P125 7C 1 257 01 PSIA P12.5 (FAN exit pressure) engine #1 7C 2 257 10 PSIA P12.5 (FAN exit pressure) engine #2 P2 7C 1 131 01 PSIA PT2 (FAN inlet pressure) engine #1 7C 2 131 10 PSIA PT2 (FAN inlet pressure) engine #2 P25 7C 1 262 01 PSIA P2.5 (Low Pressure Compressor exit pressure) #1 7C 2 262 10 PSIA P2.5 (Low Pressure Compressor exit pressure) #2 P2A 7A 1 112 01 BAR APU inlet pressure P3 7C 1 264 01 PSIA Pb burner pressure engine #1 7C 2 264 10 PSIA Pb burner pressure engine #2 P49 7C 1 132 01 PSIA Low Pressure Turbine exit pressure engine #1 7C 2 132 10 PSIA Low Pressure Turbine exit pressure engine #2 PB 7C 1 264 01 PSIA Pb burner pressure engine #1 7C 2 264 10 PSIA Pb burner pressure engine #2 PB10 7C 1 162 01 PSIA P10 engine #1 7C 2 162 10 PSIA P10 engine #2 PBV 8E 1 112 11 % Pack bypass valve position system #1 8E 2 112 00 % Pack bypass valve position system #2 PCSW 5C 1 057 01 Press control bus:Status + Fault info 5C 2 057 10 Press control bus:Status + Fault info PD 6F 1 143 01 PSI Precooler inlet pressure engine #1 6F 1 142 01 PSI Precooler inlet pressure engine #2 PDC 5C 1 144 01 PSI Cabin differential pressure



31-37-00

------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------5C 2 144 10 PSI Cabin differential pressure PF 8E 1 126 11 KG/S Pack flow system #1 8E 2 126 00 KG/S Pack flow system #2 PFAD 7A 1 004 01 APU:Performance adjustments PH Flight phase to display (DMU computed) PHA 3D 1 226 01 DEG N1 phase unbalance brg1 engine #1 3D 1 226 10 DEG N1 phase unbalance brg1 engine #2 PHT 3D 1 226 11 DEG N1 phase unbalance TRF engine #1 3D 1 226 00 DEG N1 phase unbalance TRF engine #2 PSB 26 1 320 01 PSIA No4 bearing pressure engine #1 26 1 320 10 PSIA No4 bearing pressure engine #2 PSW1 8E 1 062 11 Discrete data word (Label 062) of pack control bus system #1 8E 2 062 00 Discrete data word (Label 062) of pack control bus system #2 PT 7A 1 166 01 BAR Bleed air pressure PTCH 04 1 324 01 DEG Pitch angle 04 2 324 10 DEG Pitch angle PTCR 04 1 326 01 DEG/S Body axis pitch rate 04 2 326 10 DEG/S Body axis pitch rate RALT 25 1 164 01 FEET Radio height (R/A1) 25 1 164 10 FEET Radio height (R/A2) RI 8E 1 130 11 % Pack ram inlet position LH 8E 2 130 00 % Pack ram inlet position RH RO 8E 1 124 11 % Pack ram outlet position LH 8E 2 124 00 % Pack ram outlet position RH ROLL 04 1 325 01 DEG ROLL angle 04 2 325 10 DEG ROLL angle ROLR 04 1 327 01 DEG/S Body axis roll rate 04 2 327 10 DEG/S Body axis roll rate ROPP 6E 1 330 01 DEG Right brake pedal angle 6E 2 330 10 DEG Right brake pedal angle RSCC 6E 1 332 01 KTS reference speed command channel 6E 2 332 10 KTS reference speed command channel RSP2 6C 1 362 01 DEG LH spoiler #2 position 6C 1 372 01 DEG RH spoiler #2 position RSP3 6C 1 363 01 DEG LH spoiler #3 position 6C 1 373 01 DEG RH spoiler #3 position RSP4 6C 1 364 01 DEG LH spoiler #4 position 6C 1 374 01 DEG RH spoiler #4 position RSP5 6C 1 365 01 DEG LH spoiler #5 position 6C 1 375 01 DEG RH spoiler #5 position RUDD 29 1 312 00 DEG Rudder position 29 2 312 00 DEG Rudder position



------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------RUDT 0A 1 313 00 DEG Rudder trim 0A 2 313 00 DEG Rudder trim SAT 06 1 213 01 DEGC Static air temperature (BNR) 06 2 213 10 DEGC Static air temperature (BNR) SC1 29 1 242 01 DEGC/F Selected ckpt compt temp SC1 29 2 242 01 DEGC/F Selected ckpt compt temp SC2 29 1 244 01 DEGC/F Sel fwd cab compt temp SC2 29 2 244 01 DEGC/F Sel fwd cab compt temp SC3 29 1 244 01 DEGC/F Sel aft cab compt temp SC3 29 2 244 01 DEGC/F Sel aft cab compt temp SCC 6E 1 340 01 DEG steering command captain 6E 2 340 10 DEG steering command captain SCFD 6E 1 341 01 DEG steering command F/0 6E 2 341 10 DE steering command F/0 SDS1 29 1 001 01 SDAC discrete word #1 29 2 001 01 SDAC discrete word #1 SDS2 29 1 001 10 SDAC discrete word #2 29 2 001 10 SDAC discrete word #2 SLAT 1B 1 127 01 DEG SLAT actual position system #1 1B 2 127 10 DEG SLAT actual position system #2 SLP 0A 1 226 00 DEG Estimd sideslip (side slip angle) system #1 0A 2 226 00 DEG Estimd sideslip (side slip angle) system #2 SM 7C 1 276 01 Autostart mode active engine #1 7C 2 276 10 Autostart mode active engine #2 STA SEC APU start time STAB 6C 1 315 01 DEG Stabilizer position #1 STVC 26 1 032 01 Scavenge valve stuck closed engine #1 26 1 032 10 Scavenge valve stuck closed engine #2 STVO 26 1 032 01 Scavenge valve stuck open engine #1 26 1 032 10 Scavenge valve stuck open engine #2 SV 7C 1 270 01 Starter air valve open (local switch) engine #1 7C 2 270 10 Starter air valve open (local switch) engine #2 SVA 7C 1 325 01 % SVA (stator vane actuator feedback) engine #1 7C 2 325 10 % SVA (stator vane actuator feedback) engine #2 SW1 7C 1 270 01 ECU Discrete status word #1 engine #1 7C 2 270 10 ECU Discrete status word #1 engine #2 SW2 7C 1 271 01 ECU Discrete status word #2 engine #1 7C 2 271 10 ECU Discrete status word #2 engine #2 SW3 7C 1 272 01 ECU Discrete status word #3 engine #1 7C 2 272 10 ECU Discrete status word #3 engine #2 SW4 7C 1 273 01 ECU Discrete status word #4 engine #1 7C 2 273 10 ECU Discrete status word #4 engine #2 SW5 7C 1 274 01 ECU Discrete status word #5 engine #1 7C 2 274 10 ECU Discrete status word #5 engine #2



------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------SW6 7C 1 275 01 ECU Discrete status word #6 engine #1 7C 2 275 10 ECU Discrete status word #6 engine #2 SW7 7C 1 276 01 ECU Discrete status word #7 engine #1 7C 2 276 10 ECU Discrete status word #7 engine #2 SW8 7C 1 145 01 ECU Discrete status word #8 engine #1 7C 2 145 10 ECU Discrete status word #8 engine #2 SW9 7C 1 146 01 ECU Discrete status word #9 engine #1 7C 2 146 10 ECU Discrete status word #9 engine #2 T2 7C 1 130 01 DEGC T2 (FAN inlet temp) engine #1 7C 2 130 10 DEGC T2 (FAN inlet temp) engine #2 T25 7C 1 263 01 DEGC T2.5 (Low Pressure Compressor exit temperature) engine #1 7C 2 263 10 DEGC T2.5 (Low Pressure Compressure exit temperature) engine #2 T3 7C 1 265 01 DEGC T3 (High Pressure Compressor exit temperature) engine #1 7C 2 265 10 DEGC T3 (High Pressure Compressor exit temperature) engine #2 TAIL1 A/C ident word #1 (DMU computed) TAIL2 A/C ident word #2 (DMU computed) TAT 06 1 211 01 DEGC Total air temperature (BNR) (switched param.) THDG 04 1 044 01 DEG TRUE HEADING system #1 04 2 044 10 DEG TRUE HEADING system #2 TN 26 1 322 01 DEGC Nacelle temperature engine #1 26 1 322 10 DEGC Nacelle temperature engine #2 TNR DEG delta TN reference value in climb DEG delta TN reference value in cruise TO Destination (DMU COMPUTED) TP 8E 1 121 11 DEGC Pack outlet temperature LH 8E 2 121 00 DEGC Pack outlet temperature RH TPO 6F 1 141 01 DEGC Precooler eng #1 outlet temperature 6F 1 140 01 DEGC Precooler eng #2 outlet temperature TRA 7C 1 133 01 TRA (Throttle resolver angle) engine #1 7C 2 133 10 TRA (Throttle resolver angle) engine #2 TRP 7C 1 137 01 Thrust reserver pos. engine #1 7C 2 137 10 Thrust reserver pos. engine #2 TW 8E 1 111 11 DGEC Pack water extr. temperature LH 8E 2 111 00 DGEC Pack water extr. temperature RH UTC 17 1 150 00 UTC UTC (Universal time coordinated BNR) V3 0A 1 263 00 KTS V3 (min speed flaps retracted ) 0A 2 263 00 KTS V3 (min speed flaps retracted ) V4 0A 1 264 00 KTS V4 (min speed siats retracted ) 0A 2 264 00 KTS V4 (min speed slats retracted ) VA 5D 2 220 10 % CAB temp reg vlv pos group 3

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------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------VACC 04 1 364 01 G Vertical acceleration 04 2 364 10 G Vertical acceleration VB1 3D 1 135 01 UNITS N1 vibration eng #1 3D 1 135 10 UNITS N1 vibration eng #2 VB2 3D 1 136 01 UNITS N2 vibration eng #1 3D 1 136 10 UNITS N2 vibration eng #2 VC 3D 1 227 11 MILS Displace unbalance TRF (LPT) engine 1 3D 1 227 00 MILS Displace unbaiance TRF (LPT) engine 2 VF 5D 2 206 10 % CAB temp reg vlv pos group 1 VH 3D 1 230 11 IPS N2 veloc unbalance BRG1 (HPC)engine #1 3D 1 230 00 IPS N2 veloc unbalance BRG1 (HPC) engine #2 VLS 0A 1 245 00 KTS VLS (Min. airspeed) 0A 2 245 00 KTS VLS (Min. airspeed) VMAN 0A 1 265 00 KTS Vman (maneuvering speed ) 0A 2 265 00 KTS Vman (maneuvering speed ) VMAX 0A 1 207 00 KTS V Max (Max. allowable airspeed) 0A 2 207 00 KTS V Max (Max. allowable airspeed) VN 3D 1 227 01 MILS Displace unbalance BRG1 or TRF engine 1 3D 1 227 10 MILS Displace unbalance BRG1 or TRF engine 2 VORF 25 1 034 01 MHz VOR 1 frequency 25 1 034 10 MHz VOR 2 frequency VRTA 29 1 333 01 G Normal acceleration 29 2 333 01 G Normal acceleration VRTG 04 1 333 01 G body normal acceleration 04 2 333 10 G body normal acceleration VSCB 5C 1 150 01 FT/MIN Cabin v/s 5C 2 150 10 FT/MIN Cabin v/s VW 5D 2 207 10 % CAB temp reg viv pos group 2 WAI 29 1 001 11 WAI LH wing anti ice valve closed system #1 29 1 001 00 WAI RH wing anti ice valve closed system #2 WARN 26 1 126 00 FWC Discrete status word (Label=1 26 SDI=00) WB 7A 1 123 01 KG/S APU bleed air flow WD 04 1 316 01 DEG WIND DIRECTION true system #1 04 2 316 10 DEG WIND DIRECTION true system #2 WFQ 5A 2 257 10 KG/LBS Fuel quantity LH inner cell system #1 5A 2 261 10 KG/LBS Fuel quantity LH inner cell system #2 WS 04 1 315 01 KTS WIND SPEED system #1 04 2 315 10 KTS WIND SPEED system #2 WS1 6E 1 320 01 M/S wheel 1 speed 6E 2 320 10 M/S wheel 1 speed WS2 6E 1 321 01 M/S wheel 2 speed 6E 2 321 10 M/S wheel 2 speed WS3 6E 1 322 01 M/S wheel 3 speed 6E 2 322 10 M/S wheel 3 speed

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------------------------------------------------------------------------------Alpha Parameter Unit Comment ------------------------------------------------------------------------------WS4 6E 1 323 01 M/S wheel 4 speed 6E 2 323 10 M/S wheel 4 speed YAW 04 1 330 01 DEG/S Body axis YAW rate 04 2 330 10 DEG/S Body axis YAW rate ZCB 5C 1 151 01 FEET Cabin altitude 5C 2 151 10 FEET Cabin altitude ZDW1 50 2 060 10 Discrete data word(Label 060) Zone Controller bus2 ZLD 5C 1 163 01 FEET Landing elevation 5C 2 163 10 FEET Landing elevation

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