Technical Flashcards
ENG 1(2) REV FAULT during start
The warning can be considered spurious if the fault disappears after MAX REV then FWD IDLE selected (Ground crew and equipment clear before selection)
To conduct a FLX takeoff the crew must
Enter a Flex temperature that is higher than the TAT into the MCDU and then set the thrust levers to the FLX/MCT Detent
Switching OFF then ON the APU Master SW
Resets the ECB
The hydraulic reservoirs are normally pressurised from?
Engine 1 HP bleed air
On the ground with one engine running
TATE probes are not heated and the pitot tubes are heated at low level
A Hydraulic System Accumulator is fitted to each hydraulic system, this is
Helping to maintain a constant pressure by covering transient demands during normal operations
The Yellow hydraulic system has an electric pump as well as an engine driven pump, this pump comes on automatically when?
Engine two fails and and the flap lever is not at zero or on the ground the cargo door open/close lever is selected
Following an EPR malfunction in B-HYI the FADEC would revert to N1 Rated or N1 Unrated Mode. In either case
Autothrust control is lost. Alpha-floor protection is lost
ENG 1(2) EIVMU FAULT (IN FLIGHT)
CATII Autoland is available
Reverser deployment requires
That there is an on-ground signal from at least one LGCIU
The engine can be manually dry cranked by:
Selecting the ENGINE START selector to CRANK and pushing the corresponding MAN START pushbutton to ON
The hydraulic system on the A330 consists of?
Four engine driven pumps, three electric pumps and a RAT
When thrust reversers are selected thrust is limited to revers idle:
Until the doors are deployed by more than 70%
The Fadec system on the engines receives its power from
Powered by the aircraft electrical circuit below 8% N3 and is self powered above 8% N3
Hydraulic Reservoir Quantity is available to the crew on:
The ECAM system display and indicating as a sliding scale
If there is excessive pressure loss across the main oil scavenge filter
CLOG appears on the ENG page
If electrical power supply to the engine anti-ice fails
The anti ice valves will automatically open regardless of switch position
The outlet hydraulic pressure from the RAT is
2500 psi
The thrust levers
Can only be moved manually
The APU green AVAIL light comes on when
N reaches 95%
Which statement is correct
In forward thrust, normally EPR controls the thrust: in reverse operations, thrust is controlled as a function of N1
The hydraulic reservoirs are pressurised, this is to
Prevent the hydraulic pumps from cavitating
The FADEC control has a function called Approach Idle. This comes into effect:
During approach when the flaps are extended to 2 or greater, or when the gear is down
Flight Deck Window heating comes on:
Automatically when at least one engine is running, or the aircraft is in flight
High ENG vibration in icing conditions :
If the ENG ANTI ICE is OFF, switch on at idle fan speed one ENG after the other with approx 30sec interval
The Probe/Window Heat pushbutton when selected ON in flight:
Does nothing. ON is only used to supply power to the probes and window on the ground
If N1 exceeds 99% during a flight, a red mark shows the highest N1 attained
It will disappear after a new start on the ground
To shut down the APU in an emergency:
Push the cockpit APU FIRE switch or either the external APU SHUT OFF or APU EMER SHUT DOWN pushbuttons
If the wing anti ice is selected on during taxi
The wing anti ice calve will open for 30 seconds and then close until airborne
With an ECAM ENG 1(2) START FAULT
There is a MASTER CAUTION and a single chime
The APU
Can be used to start the engines in flight
