1.24.2010

A320 CH 34



34

ADIRU

1. RMP1(2) CAN TUNE NAV UNITS 1(2) ( VOR1 (2), ILS1 (2), ADF1 (2)…)
2. ADIRU CONSIST OF ADC AND IRS CAN OFF SEPERATELY
3. ONLY STBY PITOT STATIC L/H CONNECTED TO R/H AND AVRAGE GOES TO STBY ASI AND ALTEMETER BUT VIA ADM(AIR DATA MODULE) TO ADIRU
4. THERE ARE 3 ALFA PROBE CONNECTED TO 3 ADIRU, 6 PORT AND 5 ADM (FOR COVERTING ANALOGE TO ARINC)
5. L/H AND R/H HAVE SEPERATED ADM
6. TAT1 HAS 2 ELEMENT GOES TO ADIRU1 AND 3 (SECOND ELEMENT IN TAT2 NOT USED)
7. ONLY STBY P/S PROBE NEED WATER DRAIN(OTHERS ARE ABOVE PROBE LEVEL SO DO NOT NEED DRAIN)
8. ADIRU#3 OUTPUT GOES TO BOTH FAC’S AND ATC’S ALSO W/R ‘S AND ALL 3 DMC
9. BOTH FAC RECEIVE DATA FROM ALL 3 ADIRU
10. AIR DATA AND ATT CAN SW SEPERATEDLY TO #3 ADIRU
11. ALL ADIRU SEND SAT AND TAT TO DMC FOR ECAM SYSTEM DISPLAY
12. DDRMI (DIGITAL DISTANCE AND RADIO MAG IND) RECIEVES HDG FROM ADIRU1 ONLY
13. ADIRU CAN ALIGN FROM MCDU BY GIVING: COMPANY ROUTE, FROM/TO OR LAT AND LONG
14. AOA TEST CAN DONE ONLY ON GND
15. DICREPANCY OF ADIRU DATA DONE BY FWC (5 DEG, 500FT IN STD AND 250FT IN QNH)
16. ADIRU3 FAULTS ARE INHIBITED IN EMER CONFIG
17. OVERSPEED WARN DISPLAYED IN VMO/MMO, VFE, VLE MORE THAN THEIR VALUE + 4KTS
18. STBY COMPASS RADIO RECEIVER SW MUST ON FOR CALIBRATION





MMR

1. MMR(MULTI MODE RX) IS CONSIST OF ILS AND GPS
2. LOC FRQ IS 108.1 TO 111.95MHZ
3. G/S FRQ IS 329.15 TO 335MHZ
4. GPS FRQ :
          L1: 1575.42 MHZ
          L2: 1227.6 IS USED TO CORRECT ERROR OF L1
5. GPS RANGE IS 55 DEG TO EQUATOR
6. WHEN GPS USED NO RADIO NAV USED
7. ILS1(2) SHOWN ON PFD1(2) AND ND2(1)
8. GPS MONITORED IN MCDU AND FAULT( GPS PRIMARY WHITE) ON ND
9. GPS CON SEGMENT ARE 4 MONITOR STATION AND 1 MASTER CONT STATION
10. GPS HAS 2 ANT BUT LOC AND G/S ARE 1 ANT
11. G/S AND LOC ANT ARE FOLDED HALF LOOP DRIVEN BY CAPACITANCE COUPLING AND 2 RF CONNECTOR FOR BOTH MMR
12. GPS ANT HAS A PRE AMP AND FILTER POWERED FROM MMR
13. FMGC POS IS MIX OF GPS AND IRS POS
14. MMR TEST ONLY AVAIL IN GND
15. MMR1 SENDS DATA TO GPWS (FOR G/S MODE)
16. BELOW 700FT FMGC INHIBITES ANY FRQ CHANGE IN MMR IF LAND ARM
17. PRIMARY SOURCE FOR ADIRU3 IS GPS1
18. WRPWS IS W/R AND PWS(PREDICTIVE WIND SHEAR) SEPERATEDLY CAN OFF
19. ALL W/R INFO(FAULT, TILT,GAIN) SHOWN ON ALL ND MODE EXCEPT PLAN
20. IN PLAN W/R TR IS DE-ENER
21. A RED MSG W/S AHEAD SHOWN ON PFD
22. PWS ACTIVED BELOW 2300FT WITH ATC AUTO OR ENG RUN(OIL PRESS)
23. ONE W/R TR AND ONE CONT PNL
24. ONE WAVE GUIDE NEEDED FOR DUAL TR INSTALL
25. TR FRQ IS 9345MHZ
26. W/R TR TEST AVAIL ON GND ONLY
27. PWS HAS PRIORITY OVER GPWS AND TCAS
28. ANT MOVEMENT DONE BY 2 DC MOTOR


RA

1. RA IND ON PFD:
ALT BELOW 2500FT
GND LINE BELOW 300FT
RED RIBBON BELOW 500FT
2. RA DIGIT IS GREEN AND WILL AMBER 100FT BEFOR DH BUT IF NO DH SEL CHANGED FROM 400FT
3. RA FRQ IS 4200 TO 4400 MHZ
4. ANT RANGE IS 30 DEG FOR PITCH/ROLL
5. A CAPASITOR ON FAN CASE FOR SUPPRESS NOISE
6. DMC AUTO SW IF ONE RA FAIL
7. EIU SEND SIG FOR INHIB TEST RA IF ENG RUN IN GND (N2)
8. RA1 ONLY SENDS ALT TO EGPWS
9. ONE R/A OR ILS FAIL CAT3 INOP

TCAS

1. TCAS TX AT 1030 AND RX AT 1090MHZ AND ATC IS VICE VERSA
2. TCAS TEST AVAIL ON GND
3. TCAS TR IS IN 80VU HAS INTERFACE FOR TEST
4. CONT PNL CONT THE TCAS VIA ATC
5. TCAS RX HDG, PITCH AND ROLL FROM ADIRU1
6. TCAS HAS 2 ANT ONE UP AND ONE BOTTOM

ATC

1. 2 ATC TRANSPONDER IN 80VU, EACH HAS 2 ANT ONE TOP AND ONE TOP
2. IF ADIRU FAIL PILOT OR F/O MUST SW TO ADIRU3
3. TEST AVAIL ON GND ONLY
4. ANT IS BLADE TYPE

DME

1. DME HAS 2 INTEROGATORS IN 80VU AND 2 ANT
2. FMGC1(2) TUNE DME1(2) IN NORMAL VIA RMP BUT IF FMGC1(2) OR RMP1(2) FAIL FMGC2(1) CAN TUNE DME1(2) DIRECTLY
3. DME FRQ FOR REPLY IS FROM 962 TO 1213MHZ BUT ONLY 1025 TO 1150MHZ FOR INTROGATION
4. A SUPPRESSION LINE(ANALOG) PREVENT ATC OR DME TX AT SAME TIME TO PREVENT INTERFERENCE
5. DME TONE CAN HEARD BY VOR OR ILS KNOB ON ACP
6. LGCIU SENT SIGNAL TO DME TO FLT LEG COUNT AND ENABLE TEST ON GND ONLY
7. DME RANGE SHOWN ON CAPT PFD ANF F/O ND AND DDRMI
8. DME AND ATC ARE THE SAME TYPE

GPWS

1. TERRAIN AUTO OR BY P/B SHOW ON ND IF DET IN PLACE WITH RADAR
2. G/S P/B USE TO CANCEL G/S WARN AND TEST ON GND AND 2000FT AGL
3. UNIT IS IN 80VU




ADF

1. FRQ IS FROM 190 TO 1750KHZ
2. ADF RX IS IN 80VU NO2 IS OPTION
3. ADF BEARING SHOWN ON ND’S AND DDRMI
4. 2 ADF ANT EACH BOTH ON TOP,EACH ANT HAS 2 LOOP AND 1 SENSE AND 1 AMP SUPP BY 12VDC FROM RX

VOR

1. VOR AND MARKER IS IN SAME UNIT
2. 2 VOR RX IN 80VU BUT MKR IS ONE
3. VOR ANT IS ON TOP OF VERTICAL FIN
4. MKR ANT IS IN BOTTOM NEAR FWD CARGO






















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