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Alpha Parameter Unit Comment -------------------------------------------------------------------------------
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 1 306 01 % Selected HPTC position engine #1
7C 2 306 10 % Selected HPTC position 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
LCIT 7A 1 110 01 DEGC APU Load compressor inlet temperature
LGDW 6D 1 021 01 LGCIU discrete word #2
6D 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
LPT 7C 1 307 01 % Selected LPTC position engine #1
7C 2 307 10 % Selected LPTC position engine #2
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)
R 1EFF : 001-049, 051-099, 101-105, 159-199, 1 31-37-00Page 22 1210-210, 1May 01/05 1 1 1CES 1
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Alpha Parameter Unit Comment -------------------------------------------------------------------------------
06 2 205 10 MACH MN3 26 1 205 11 MACH MW1 7C 1 350 01
7C 2 350 10 MW2 7C 1 351 01 7C 2 351 10 MW3 7C 1 352 01 7C 2 352 10 MW4 7C 1 353 01 7C 2 353 10 MW5 7C 1 354 01 7C 2 354 10 N1 7C 1 346 01 %RPM 7C 2 346 10 %RPM N1C 7C 1 341 01 %RPM 7C 2 341 10 %RPM N1F %RPM
%RPM
N1K N1K
N1L 7C 1 337 01 %RPM 7C 2 337 10 %RPM N1MX 7C 1 342 01 %RPM 7C 2 342 10 %RPM N1R %RPM %RPM N2 7C 1 344 01 %RPM 7C 2 344 10 %RPM N2F %RPM %RPM
N2K
NA 7A 1 176 01 %RPM NAI 50 2 061 10
50 2 061 10 NPA %RPM NRA 6E 1 336 01 DEG
6E 2 336 10 DEG NSVC 6E 1 335 01 MA 6E 2 335 10 MA NWSA 6E 1 334 01 DEG 6E 2 334 10 DEG
Mach (switched Parameter)Mach 3ECU Maintenance data word #1 engine #1ECU Maintenance data word #1 engine #2ECU Maintenance data word #2 engine #1ECU Maintenance data word #2 engine #2ECU Maintenance data word #3 engine #1ECU Maintenance data word #3 engine #2ECU Maintenance data word #4 engine #1ECU Maintenance data word #4 engine #2ECU Maintenance data word #5 engine #1ECU Maintenance data word #5 engine #2Actual (low rotor speed) engine #1Actual (low rotor speed) engine #2N1 command engine #1N1 command engine #2N1 Actual (low rotor speed) engine #1:Filtered ParameterN1 Actual (low rotor speed) engine #2:Filtered ParameterN1 corrected left (DMU computed) N1 corrected right (DMU computed)N1 limit engine #1N1 limit engine #2N1 maximun engine #1N1 maximun engine #2N1 left rateN1 right rateN2 Actual (high rotor speed) engine #1N2 Actual (high rotor speed) engine #2N2 Actual (high rotor speed) engine #1:FilteredN2 Actual (high rotor speed) engine #2:FilteredN2 corrected left (DMU computed) N2 corrected right (DMU computed)APU RPMNacelle anti-ice engine #1 openNacelle anti-ice engine #2 openAPU RPM at APU EGT peak during APU startNWS reference angleNWS reference anglecurrent servo valve NWScurrent servo valve NWSNWS angleNWS angle
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本文链接地址：A320飞机维护手册 AMM 指示/记录系统 4(44)
