PHASE 2

WHEN AUTOTHRUST IS DISENGAGED BY THE DISCONNECT SWITCHES ON THE THROTTLES THE. ENGINE THRUST IMMEDIATELY ADAPTS TO THE CURRENT THRUST LEVER POSITION. .

THE FCU IS USUALLY USED. SHORT TERM ORDER SELECTION. .

AN AUTOPILOT BE ENGAGED. 5 SECONDS AFTER LIFT OFF. .

THE FUNCTION COMPUTES THE LIMIT AND MANOEUVRING SPEEDS THAT SHOW ON THE PFD IS. FE. .

WINDSHEAR WARNINGS SHOW ON. PFD. .

THE FUNCTION OF THE FMGEC RELATES TO THE DETECTION OF UNUSUAL FLIGHT CONDITIONS. IS FLIGHT ENVELOPE. .

THE POSSIBLE AUTOTHRUST MODES ARE. SPEED, MACH, THRUST. .

THE CIDS CAUTION ANNUNCIATION ON THE FAP. SHOW THAT A CIDS FAILURE HAS OCCURRED. .

RECEPTION ANTENNAS IN A RADIO ALTIMETER SYSTEM ARE. ONE. .

THE POWER SUPPLY TO THE SATCOM SUB-SYSTEMS IS. 115 VAC BUS 2. .

TO MAKE SURE THAT THE QUICK-DISCONNECT COUPLING ON THE ADMS ARE CORRECTLY INSTALLED. THE BLUE RING IS VISIBLE. .

THE PROCEDURE TO ALIGN THE ADIRU IF THE GPS POSITION IS NOT AVAILABLE IS. ENTER THE FROM/TO CITY PAIR ON THE INIT PAGE OF THE MCDU. .

THE ADIRU PROVIDE HEADING DATA TO THE DIGITAL DISTANCE AND RADIO MAGNETIC INDICATOR (DDRMI) IS. ADIRU 1 AND 3. .

THE TIME TO IRS ALIGNMENT IS SHOW. ON THE ECAM MEMO PAGE OR MCDU. .

THE NAVIGATION RECEIVERS USUALLY TUNED. AUTOMATICALLY BY THE FMGEC. .

THE RMP CAN TUNE ADF 1 IN THE BACKUP TUNING MODE IS. RMP 1. .

THE ILS 1 DATA SHOW ON. CAPT PFD AND F/O ND. .

ILS RECEIVER USUALLY IS TUNED. BY THE ONSIDE FMGEC THROUGH THE ONSIDE RMP. .

ND MODE(S) SHOW WXR RETURNS ARE. ARC OR ROSE MODE. .

RADIO ALTIMETER TRANSCEIVERS ARE. IN THE AFT CARGO COMPARTMENT DOOR AREA. .

THE SOURCE OF RADIO ALTITUDE DATA FOR THE TAWS/EGPWS. RADIO ALTIMETER 1 OR 2. .

THE ALERTS/WARNINGS HAVE PRIORITY OVER EGPWS ALERTS ARE. PREDICTIVE WINDSHEAR. .

THE INFORMATION DOES DME PROVIDE. SLANT RANGE DISTANCE. .

DME DATA SHOW. PFD, ND AND DDRMI. .

THE DATA CAN SHOW ON THE. DDRMI ARE VOR, DME, ADF AND HEADING. .

THE BAROMETRIC ALTITUDE SOURCE FOR ATC ARE. 1 ADIRU 1 OR 3. .

THE ADF ANTENNA PRE-AMPLIFIER IS. IN THE ADF ANTENNA. .

THE FMGEC USE VOR AND DME DATA. AIRCRAFT POSITION AND RADIO DISTANCE COMPUTATION. .

IF THERE IS A GPS FAILURE SHOWS. NAVGPS 1(2) FAULT MESSAGE SHOWS IN THE LOWER PART OF THE. .

THE FOLLOWING IS NOT A DME FUNCTION. PREPARE DME BEARING DATA FOR FLIGHT DECK INDICATION. .

THE TYPE OF STATIONS CAN THE ADF RECEIVE ARE. NDB. .

THE FUNCTION COMPUTES THE LIMIT AND MANOEUVRING SPEEDS THAT SHOW ON THE PFD IS. FE. .