No because it is warmer, according to ISA temperature should be -55°C

They are aerodynamically efficient surfaces located at the wing tips, designed to reduce induced drag and increase fuel efficiency.

They increase efficiency by reducing the size of the wingtip vortices, which are created by the difference between the pressure on the upper surface of the wing and that on the lower surface.

SOP's are Standard Operating Procedures, they provide safety, uniformity and work ethics.

A turbofan is a type of jet engine, similar to a turbojet.

It essentially consists of a ducted fan with a smaller diameter turbojet engine mounted behind it that powers the fan.

Part of the airstream from the ducted fan passes through the turbojet where it is burnt to power the fan, but the majority of the flow bypasses it, and produces most of the thrust. They are mainly used commercially because they are highly efficient and relatively quiet in operation.

Contingency fuel is carried to account for additional enroute fuel consumption caused by wind, routing changes or ATM: ATM/CNS restrictions.

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.

The airspeed indicator uses part of the aircraft's pitot-static system to measure and compare the dynamic air pressure between air moving into the pitot tube and static air pressure measured in the case. 

The ASI is calibrated to ISA at MSL and represents the dynamic pressure as indicated airspeed in knots per hour.

ASI errors can originate and vary from:

Instrument Pressure Density Compressibility Maneuver Blocked pitot static system

Precision Approach Path Indicator