A swept wing makes the velocity vector normal to the leading edge a shorter distance than the chordwise resultant.

A wing stalls because the airflow over the wing’s upper surface separates when the critical angle of attack is reached or exceeded. This causes a reduction in the lift generated by the aerofoil

To monitor the flight management and aircraft control actions of the Pilot Flying and carry out support duties such as communications and check-list reading.

Drag is the component of the total aerodynamic force parallel to the relative airflow.

Drag is generated by any body placed in a flow and it's composed of friction, form, and pressure drag.

The Center of pressure position is dependent of the angle of attack. As the angle of attack increases the center of pressure moves closer to the leading edge.

GPWS is a central computer system that receives various data inputs on configuration, (radio altimeter) height/altitude and instrument landing system glide slope deviation and is able to alert the pilot when a dangerous situation is about to occur.

To notify the crew of the aircraft of a particular position on the IAP.

Locators have been largely replaced with Distance Measuring Equipment (DME), but they can sometimes be found associated with Outer or Middle Markers where they are referred to as Locator Outer Marker (LOM) or Locator Middle Marker (LMM).

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.

It's vertical velocity of the aircraft usually expressed in feet per minute.

Vref = 1.3 x Vs0 (stall speed in the landing configuration).