Phase 1

what is the main procedure for leveling the aircraft?. Level indicator. Spirit leveler. ADIRS.

What zone relates to the upper fuselage?. 100. 200. 800.

Wha will occur when the annunciator lights switch is set to TEST?. The ECAM displays a test pattern. AII LEDs show a test pattern. the cockpit lighting systems dims.

When will the emergency lights be supplied from EPSU batteries?. The EMER push-button on the forward attendant, panel is depressed and the EMER Lt switch isON. The EMER Lt switch isARM, usual AC power and DC essential bus fails. The EMER Lt switch isON and the DC essential bus is supplied.

What has to be done to recover the failed ND?. ND image must be switched over to upper ECAM display. Nothing. ND image is recovered automatically by it's associated DMC. Manually pressing PFD/ND transfer p/b.

What isthe reconfiguration ifthe EWD fails?. EWD is automatically transferred to lower ECAM display. No reconfiguration possible. EWD can be manually transferred to lower ECAM display.

When will the STAT INV operate in flight?. AC buses and CSM/G not available. CSM/G available and RAT extended. CSM/G suppliesAC ESS at slat extension.

What are the Main Electrical power sources?. Integrated Drive Generators (IDGs), APU Generator and External Power. Integrated Drive Generators (IDGs), Back Up Generators (BUGs), Primary and Secondary External Power. Integrated Drive Generators (IDGs), APU generator, Back Up Generators (BUGs).

What type are batteries?. Lead-acid. Nickel cadmium. Lithium-ion.

What is the effect if TR2 fail son ground with EXT PWR A connected and the MAINT BUS switch in ON position?. DC BAT BUS is not available. DC SERVICE BUS is not available. TR1will supply DC SERVICE BUS.

What supplies the AC BUS 1 and 2 if Engine 2 fails inflight and APU is operating?. GEN 1 supplies AC BUS 1 and 2. GEN 1 supplies AC Bus 1, APU GEN supplies AC BUS 2. AC BUS 2 will not be powered.

What is the effect if the BUS TIE P/BSW (13XU on 235VU) is set to OFF?. BTC 1, BTC 2 and SIC opens. BTC 1 and 2 opens, SIC closes. BTC 1 and 2 closes, SIC opens.

What is the purpose of the Inadvertent Paralleling Trip function on an AC BUS?. Prevents two different sources to be connected in parallel for more than 130 ms. Allows two different sources to be connected in parallel after 130 ms. Prevents two different sources to be connected in parallel for more than 80 ms.

How are the main and APU batteries ventilated?. Dedicated fan below each battery. Equipment cooling and ventilation system. Differential pressure between cabin and the outside.

What is the supply priority for AC Bus1 XP?. IDG 1/APU GEN/EXT PWR B/EXT PWR A/IDG2. APU GEN/IDG 1/EXT PWR A/EXT PWR B/IDG2. IDG 2/APU GEN/EXT PWR B/EXT PWR A/IDG1.

What are the characteristics of type 3 systems?. They can be downloaded in flight and on ground. They can be uploaded in flight. They do not generate failure messages.

What are the type 1 system computers in CMS?. System that can remember last 64 flight memories. System that can remember only last flight memory. System that do not have any memory.

Where are the ACARS functions In ATIMS?. ATC menu. AOC menu. Communication menu.

What types of communication does ATIMS use for data-link communication?. Radio Communication, Internet, and Satellite Communication. GPS, Cellular Data, and Radar. VHF Data Link, HF Data Radio, and Satellite Communication.

How do class 2 aircraft system failures show on ECAM?. By a box on the failed system at lower part of the EWD. By system failures with underline in the EWD. On the ECAM status page.

When isthe DFDRS usually powered?. If one engine is started until 5 minutes after last engine shutdown. No.1 engine start until 5 minutes after first engine stop. At electrical power-up until 5 minutes after power down.

How many ECAM modes of operation let aircraft system operation and status data show on the SD?. 2 manual and 2 automatic. 3 manual and 1 automatic. 1 manual and 3 automatic.

What is the maximum number of aircraft parameters that can be viewed on MCDU by the alpha call up function?: 3000. 300. 30.

When a PFD fails where will the PFD data show?. The off-side inboard display. The related in board display. The lower center display.

When does the EFIS SINGLE SOURCE 2 message on both PFDs comes on?. When DMC 1, 2 and 3 have failed. When DMC 2 is driving all 6 DUs. When EFIS is in Single Mode.

How can a system page show on the EWD when ECAM is in single-display mode?. Not able to see any system page. Press and hold any system page button on ECAM Control Panel. Press any system page button on ECAM Control Panel.

How many points on the structure are designated for the purpose of lifting the aircraft?. 2. 4. 3.

What is the purpose o fATA 10-00 ?. Parking and mooring. Parking only. Mooring only.