Phase 2

What transmits the temperature data to CIDS?. ACSC. ECS. Temperatures sensor directly.

What is the purpose of the SELCAL system?. o receive signals from satellites. To alert the flight crew of a call from a ground based radio station. To send signals to satellites.

Which VHF System transmits usually and receives data?. HF 1 only. F 3 only. HF 2and VHF 3.

Where is the EVAC aural warning (analogue signal) generated?. They are integrated into the DEU A units with the overhead speakers. In each type A DEU and broadcast with the cabin speakers. By individual speakers in the overhead lockers.

Where can you initiate a Test of the Conkpit Voice Recorder (CVR)?. On the Center Pedestal. on the Overhead Panel. central fault Display System (CFDS).

Which VDR data radio connects to the ATSU?. VDR 2. VDR 3. VDR 1.

What does DEU B control?. cabin crew functions. Lighting, signs, calls and cabin sounds. Emergency Lighting.

How is a SELCAL call indicated in the Cockpit?. By an indication on all the Audio control Panels (ACPs). By an indication on all the Audio Control Panels (ACPs) with an aural alert. By an indication on one Audio Control Panel (ACP).

What conditions will allow you to erase the CVR?. use the special function of an MCDU. Parking brake On and landing Gears down and compressed. The two Engines shut down and Landing Gears compressed.

hat is the purpose of the Landing Gear Control and Interface Unit (LGCIU) input to the VHF transceivers?. To Swich from low to high frequency transmission when the landing gear is selected down. For automatic data transfer via the ATSU when the landing gear is selected down. For the FLIGHT/GROUND status to the VHF System Bite.

How is the FCU usually used?. Long term order selection. Short term order selection. For order selection, if guidance is managed.

When is windshear detection active?. Anytime the aircraft is in flight. when selected on the FCU. From 1300 ft RA to 50 ft RA in approach.

when can the two autopilot be engaged at the same time?. Only when and track mode is active, below 400 ft. On ground, if engines are stopped without any other condition. When approach has been selected on the FCU.

What happens when alpha Floor Protection is initiated?. Autothrust is forced to TO/GA thrust. Autothrust is forced to TO/GA thrust only if AP is engaged. Engines are commanded to full thrust via the EEC.

How can the MCDUs be reset?. By the brightness ON/OFF knob. by the FMGEC reset CB on the overhead. by the FM reset CB on the overhead.

What is managed speed?. the speed reference can only be selected. If the speed reference is computed by the FMGEC. When the speed is set on the FCU and the knob is pulled.

What abnormal flight condition does the Flight Envelope protection function within the FMGEC detect?. Excessive Terrain Closure. Aircraft Cargo Position. Wind Shear protection.

What happens when autothrust is disengaged by the P/B switches on the FCU ?. the engine thrust will gradually adapt to the current thrust lever position. the engine thrust immediately adapts to the current thrust lever position. the engine thrust will gradually go to IDLE 0.

How can autopilot be disengaged ?. side stick pushbutton or force application on a side stick. Applying a Force on a side stick. priority pushbutton on the side stick.

How is autothrust manually engaged?. by pressing the A/THR P/B on the FCU. the auto throttle cannot be manually engaged. By setting the throttle levers in any position between IDLE and CL.

What are the possible autothrust modes?. Alphafloor, SPEED,TOGA. SPEED, MACH,THRUST. TOGA, T/OFF, IDLE.

where do WINDSHEAR warnings show?. ECAM. PFD. ND.

What shows if there is a GPS failure?. GPS 1 (2) FAIL message Shows. NAV GPS 1 (2) FAULT message shows on. V GPS 1(2) FAULT message shows in the lower part of the EWD.

What unit is used for the barometric reference adjustment?. display management Computer. Flight Management Guidance and Envelope computer. Flight control unit.

what is the source of radio altitude data for the TAWS/EGPWS. Radio altimeter 1 or 2. Radio altimeter 1. Radio altimeter 2.

Which MCDU page lets present position data be entered?. POS INIT. RAD NAV. PERF INIT.

What guidance does a resolution advisory give?. Actions of threat. location of threat. vertical correction.

How is VOR 2 receiver auto-tuned if FMGEC 2 has failed?. From VOR 1 synchronising the tune data. from FMGEC 1after FM switching. the VOR 2 cannot be auto-tuned.

why does the ON BAT light come on when a selector is set to NAV?. indicates that the present position needs to be inserted. indicates a test of the switching to the IRU batteries. indicates a test of the switching to the aircraft batteries.

Where are radio altimeter transceivers?. in the aft cargo compartmnet door area. in the unpressurized tail area. Avionic bay, aft rack.

How is an ADF receiver usually tuned?. Manually through onside RMP. Automatically by the onside FMGEC through the onside RMP. Automatically by the onside MCDU Through any RMP.

Which ND mode(s) show WXR returns?. PLAN mode. ARC mode only. ARC or ROSE mode.

what data can show on the DDRMI?. VOR, DME, ADF and Heading. DME, ADF and Marker Beacon. VOR, DME and Heading.

What information does DME provide?. Slant range distance. Range and bearing. Ground distance.

Which RMP can tune ADF 1 in the backup tuning mode?. RMP 3. RMP 1. RMP 1 or RMP 2.

Which cockpit display shows the necessary Vertical Speed (V/S) to reach sufficient vertical separation in case of a resolution advisory?. Primary Flight Display (PFD). System Display (SD). Navigational Display (ND).

How is a fast realignment made?. By using the MCDU to insert the LAT/LONG of the current position. By using the auto alignment by the GPS. Selecting from NAV to OFF and back to NAV within 5 seconds.

Which alerts/warnings have priority over EGPWS alerts?. Predictive windshear. ake off warning. TCAS advisory.

In normal operation where is Radio Altimeter 1 (Rad Alt 1) information displayed?. First officers' PFD. Captains' PFD. System Display Memo area.

What are the pressure sources for the Air Data Modules (ADM)?. The pitot probes only. the captain and first officer pilot probes and static port only. 3 pilot tubes, 4 static ports and one standby static line.