54 Questions
The minimum theoretical pavement width for a 180 deg turn on the A320 is:
22.8 m
What is the max wheel brake temperature for take-off with brake fans off:
300 ̊C
What is the max wheel brake temperature for take-off with brake fans on:
150 ̊C
What is the normal hydraulic system operating pressure:
3,000 psi
What is the max operating altitude with slats or flaps extended:
20,000 ft
With an engine failure what is the time limit on TOGA power on the live engine:
Ten mins
Max speed for conf. full (A321) is:
186 kts
Under the provisions of the MEL, what does an (m) mean when it occurs beside an item?
Item requiring maintenance action
Under the provisions of the Minimum Equipment List (MEL), what does (v) mean when it occurs beside an item:
Item relating to RVSM operations
A cabin door is opened from the outside, but the escape slide is armed, what happens?
The escape slide is automatically disarmed
If door control handle is lifted and the white indicator illuminates - what does this mean?
The escape slide is armed, if you go on lifting the handle, door opens and slide will deploy
After landing, the red indicator on the door flashes red. It indicates that:
Escape slide is disarmed, and engines are stopped, but cabin is still pressurised
How many passenger portable oxygen bottles are fitted to the A21N?
12
How many first aid kits are fitted to the A21N?
3
The range and duration of the halon extinguisher fitted to the A21N is:
10ft / 10secs
The number of water extinguishers fitted to the A21N:
1
How many smokehoods are fitted to the A21N in total?
6
The range and duration of the water extinguisher fitted to the A21N?
15ft / 30secs
How many escape ropes are in the cockpit?
2 escape ropes which can be used through either window
The autoland red light is armed for failures on ILS approaches:
Below 200 ft radio
For a Cat III approach with a DH and an FMA capability of CAT 3 Dual, the minimum visual reference must contain:
1 centreline light
A Cat II or Cat III approach may be flown:
By the LHS only
When must you go-around for an amber caution on a Cat II/III approach?:
At any time below 1,000 ft
The maximum reduction in thrust (flex thrust) is:
25%
What is the maximum allowable flex temperature (A320 CEO)?
ISA+53
Reduced thrust is not permitted:
On a contaminated runway or in windshear conditions
A runway is contaminated when it is covered with a depth of water exceeding:
3 mm
Take off performance information for the A320/321 is contained in:
PER
The Airbus 320/321 limitations section is contained in:
LIM
On a runway covered with 10mm of dry snow (max recommended depth 100mm)
Flex T/O is not permitted
Off a dry runway, what height must the aircraft reach by the end of TODA?
35 ft
Engine limitations for the A320/321 are contained in:
LIM
Under CAT.OP.MPA.180, Aer Lingus is approved by the IAA to operate which type of fuel scheme?
Basic Fuel Scheme with variations
The normal max landing weight (A21N) is:
79,200 kg
The max ramp weight (A320) is:
73,900 kg
The structural MTOW (A21N) is:
97,000 kg
When drifting down using the obstacle strategy, the speed used is:
Green dot speed
The max T/O weight (A320) is:
73,500 kg
The final reserve fuel required to be carried by a jet A/C (A320/A321) is:
30 mins
The final reserve fuel on the A320 /321 for a ‘Mayday’ call is:
30 minutes
Regarding the determination of aerodrome operating minima, the A320 / A321 is:
Category C
The ICAO recommended minimum time spacing when departing after an aircraft in wake turbulence category ‘heavy’ is:
2 min
The maximum cross wind allowed for CAT II/III automatic approach landing and rollout on the A320 (two engines) is:
20 kt
FMA ‘CAT III single’ means:
Cat III minima with a DH must be used
Maximum allowed wing fuel imbalance (A21N) with heavier tank full, in flight and at landing is:
1,320 kg
The max zero fuel weight (A21N) is:
75,600 kg
For take-off the trimmable horizontal stabilizer (THS):
Must be set in accordance with the take-off % MAC from the load & trim sheet
Max landing weight (A320 CEO) is:
66,000 kg
When the cargo door switch for the yellow hydraulic pump is in use, the flight controls are:
Inhibited
The refueling control panel is located:
In the RH wing body fairing
When the aircraft has been parked for a long period the pressure in the brake accumulator may have to be topped up, this could be achieved by:
Operating the yellow electric pump
When refueling with passengers on board, the fasten seat belt sign should be:
Off
The anti-collision beacon should be switched off after shutting down the engines:
N1=10% and fuel flow zero on both engines
The maximum refueling pressure is:
50 psi (3.5 bars)
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