Technical

Question 0

ENG 1(2) REV FAULT during start

Answer 0

The warning can be considered spurious if the fault disappears after MAX REV then FWD IDLE selected (Ground crew and equipment clear before selection)

Question 1

To conduct a FLX takeoff the crew must

Answer 1

Enter a Flex temperature that is higher than the TAT into the MCDU and then set the thrust levers to the FLX/MCT Detent

Question 2

Switching OFF then ON the APU Master SW

Answer 2

Resets the ECB

Question 3

The hydraulic reservoirs are normally pressurised from?

Answer 3

Engine 1 HP bleed air

Question 4

On the ground with one engine running

Answer 4

TATE probes are not heated and the pitot tubes are heated at low level

Question 5

A Hydraulic System Accumulator is fitted to each hydraulic system, this is

Answer 5

Helping to maintain a constant pressure by covering transient demands during normal operations

Question 6

The Yellow hydraulic system has an electric pump as well as an engine driven pump, this pump comes on automatically when?

Answer 6

Engine two fails and and the flap lever is not at zero or on the ground the cargo door open/close lever is selected

Question 7

Following an EPR malfunction in B-HYI the FADEC would revert to N1 Rated or N1 Unrated Mode. In either case

Answer 7

Autothrust control is lost. Alpha-floor protection is lost

Question 8

ENG 1(2) EIVMU FAULT (IN FLIGHT)

Answer 8

CATII Autoland is available

Question 9

Reverser deployment requires

Answer 9

That there is an on-ground signal from at least one LGCIU

Question 10

The engine can be manually dry cranked by:

Answer 10

Selecting the ENGINE START selector to CRANK and pushing the corresponding MAN START pushbutton to ON

Question 11

The hydraulic system on the A330 consists of?

Answer 11

Four engine driven pumps, three electric pumps and a RAT

Question 12

When thrust reversers are selected thrust is limited to revers idle:

Answer 12

Until the doors are deployed by more than 70%

Question 13

The Fadec system on the engines receives its power from

Answer 13

Powered by the aircraft electrical circuit below 8% N3 and is self powered above 8% N3

Question 14

Hydraulic Reservoir Quantity is available to the crew on:

Answer 14

The ECAM system display and indicating as a sliding scale

Question 15

If there is excessive pressure loss across the main oil scavenge filter

Answer 15

CLOG appears on the ENG page

Question 16

If electrical power supply to the engine anti-ice fails

Answer 16

The anti ice valves will automatically open regardless of switch position

Question 17

The outlet hydraulic pressure from the RAT is

Answer 17

2500 psi

Question 18

The thrust levers

Answer 18

Can only be moved manually

Question 19

The APU green AVAIL light comes on when

Answer 19

N reaches 95%

Question 20

Which statement is correct

Answer 20

In forward thrust, normally EPR controls the thrust: in reverse operations, thrust is controlled as a function of N1

Question 21

The hydraulic reservoirs are pressurised, this is to

Answer 21

Prevent the hydraulic pumps from cavitating

Question 22

The FADEC control has a function called Approach Idle. This comes into effect:

Answer 22

During approach when the flaps are extended to 2 or greater, or when the gear is down

Question 23

Flight Deck Window heating comes on:

Answer 23

Automatically when at least one engine is running, or the aircraft is in flight

Question 24

High ENG vibration in icing conditions :

Answer 24

If the ENG ANTI ICE is OFF, switch on at idle fan speed one ENG after the other with approx 30sec interval

Question 25

The Probe/Window Heat pushbutton when selected ON in flight:

Answer 25

Does nothing. ON is only used to supply power to the probes and window on the ground

Question 26

If N1 exceeds 99% during a flight, a red mark shows the highest N1 attained

Answer 26

It will disappear after a new start on the ground

Question 27

To shut down the APU in an emergency:

Answer 27

Push the cockpit APU FIRE switch or either the external APU SHUT OFF or APU EMER SHUT DOWN pushbuttons

Question 28

If the wing anti ice is selected on during taxi

Answer 28

The wing anti ice calve will open for 30 seconds and then close until airborne

Question 29

With an ECAM ENG 1(2) START FAULT

Answer 29

There is a MASTER CAUTION and a single chime

Question 30

The APU

Answer 30

Can be used to start the engines in flight