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A318/A319/A320/A321 FLEET DSC-34-PLP-TOC P 4/4
FCOM 19 AUG 10
DSC-34-70-30 EGPWS FUNCTIONS
TERRAIN AWARENESS AND DISPLAY............................................................................................................. 1/8
TERRAIN CAUTION AND WARNING ENVELOPE............................................................................................. 4/8
TERRAIN CLEARANCE FLOOR..........................................................................................................................5/8
RUNWAY FIELD CLEARANCE FLOOR.............................................................................................................. 6/8
DSC-34-70-40 CONTROLS AND INDICATORS
OVERHEAD PANEL........................................................................................................................................... 1/4
INSTRUMENT PANELS......................................................................................................................................2/4
DSC-34-70-50 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-34-70-60 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
DSC-34-80 TCAS
DSC-34-80-10 DESCRIPTION
GENERAL............................................................................................................................................................1/6
MAIN COMPONENTS.........................................................................................................................................1/6
PRINCIPLE..........................................................................................................................................................4/6
INTRUDER CLASSIFICATION........................................................................................................................... 4/6
TA/RA THRESHOLDS........................................................................................................................................ 5/6
TCAS MODES.....................................................................................................................................................6/6
ADVISORY INHIBITION......................................................................................................................................6/6
DSC-34-80-20 CONTROLS AND INDICATORS
ATC/TCAS PANEL............................................................................................................................................1/14
ND INDICATIONS.............................................................................................................................................4/14
TCAS MESSAGES............................................................................................................................................7/14
PFD INDICATIONS...........................................................................................................................................8/14
AURAL MESSAGES....................................................................................................................................... 12/14
DSC-34-80-30 WARNINGS AND CAUTIONS
WARNINGS AND CAUTIONS............................................................................................................................ 1/2
DSC-34-80-40 ELECTRICAL SUPPLY
BUS EQUIPMENT LIST......................................................................................................................................1/2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
NAVIGATION
ADIRS - DESCRIPTION
A318/A319/A320/A321 FLEET DSC-34-10-10 P 1/8
FCOM 19 AUG 10
GENERAL
Applicable to:
The Air Data and Inertial Reference System (ADIRS) supplies temperature, anemometric, barometric
and inertial parameters to the EFIS system (PFD and ND) and to other user systems (FMGC,
FADEC, ELAC, SEC, FAC, FWC, SFCC, ATC, GPWS, CFDIU, CPC).
The system includes :
three identical ADIRU’s (Air ‐ Data and Inertial Reference Units).
Each ADIRU is divided in two parts, either of which can work separately in case of failure in the
other :
• the ADR part (Air Data Reference) which supplies barometric altitude, airspeed, mach, angle of
attack, temperature and overspeed warnings.
• the IR part (Inertial Reference) which supplies attitude, flight path vector, track, heading,
accelerations, angular rates, ground speed and aircraft position.
Note: The ADIRU gives true heading instead of magnetic heading :
　
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