The speed is too low for an indication.

An IRS is an Inertial Reference System  which consists of accelerometers, gyroscopes (laser) and a position computer.

The computer calculates the aircrafts position by direction and velocity sensed by the accelerometers from the initial latitude and longitude input.

An IRS enables the aircraft to fly great circle tracks and to navigate accurately across vast expanses where no ground based navigation aids are available.

Induced drag and its wing tip vortices are a direct consequence of the creation of lift by the wing.

Since the Coefficient of Lift is large when the Angle of Attack is large, induced drag is inversely proportional to the square of the speed whereas all other drag is directly proportional to the square of the speed.

The effect of this is that induced drag is relatively unimportant at high speed in the cruise and descent where it probably represents less than 10% of total drag. In the climb, it is more important representing at least 20% of total drag. At slow speeds just after take off and in the initial climb, it is of maximum importance and may produce as much as 70% of total drag.

Finally, when looking at the potential strength of wing tip vortices, all this theory on induced drag must be moderated by the effect of aircraft weight. Induced drag will always increase with aircraft weight.

Battery power to the starter motors.

Tire creep is the tendency of the tire to rotate slowly around the wheel hub as a result of a millisecond landing friction on the tire before wheel spin occurs.

Yes, it is important because if there is too much creep the tire can tear out the inflation valve and cause the tire to burst.

Assuming I'm performing single pilot operations:

• power idle,

• max brakes (and reversers if available),

-maintain directional control using rudder input,

• After coming to a full stop set parking break.

• Inform ATC 'Stopping'.

• Initiate the appropriate process to diagnose the problem (ECAM, NITS DODAR, checklists....).

• When performing multi pilot operations the actions performed by me will depend with my current role: PF, PM and/or CM1 CM2.

Example answer for a candidate with previous Seneca experience:

Weights:

Max all up weight – take off 4570lbs Max all up weight – landing 4340lbs Empty weight - 2830lbs Usefull load - 1740lbs

Speeds:

Clean stall 66kts with flaps 60kts Vyse 89kts Cruise 140kts gear raising 107kts – lowering 129kts. Vne 195

The 6 cyclinder teledyne continental turbo- charged, fuel injected engines provide 200 hp at 2575.

Left engine rotated clockwise and right anti clockwise.

No critical engine, RayGay turbo’s 42” MAP, 40” limit at lower levels, cowl flaps provide cooling and has 3 positions, open mid and closed.

Avgas 100/130

Props 2 or 3 blade, constant speed, hydraulically actuated, fully feathering.

Oil keeps props at fine pitch, gas and air keep the rpm towards feather. Takes 6 seconds to feather and must happen before locks engage at 800 rpm.

Limit load factor 3.8G

Fuel 2 x 54 (64US) gallons tanks 8 quarts oil max 6 Min

Retractable gear – hydraulic pumps – electrically driven. 6-7 seconds transit

Nose gear has 27 degrees castor.

Main wheels 55psi, nose wheel 31psi

Cable operated controls, all moving stabilator with anti servo tab which acts as a trim.

Frise ailerons and differential ailerons, up more than down.

Manual flaps, 3 settings, 10, 25, 40 degrees.

4.5” – 5.2” hg suction – AH, DI.

Heated lift deflectors and stall warners, anti ice.

Downward inclination of a wing from the root to the tip.

No, there is no P-factor (asymmetric blade effect) as on a propeller-driven aircraft.

When rolling the aircraft the up-going wing will experience more drag than the down-going wing. This will result in a yawing moment that directly opposes the desired direction of turn. (i.e.: rolling left will cause a right yaw.)