This speed is defined to be equal to the greater of stall speed (Vso) multiplied by 1.3, or stall speed (Vs1g) multiplied by 1.23.

The landing configuration that is to be taken into consideration can be defined by either the operator or by the aeroplane manufacturer but is most commonly assigned by the manufacturer.

Swept wings are:

Better for high speed flight as they have minimal camber and thickness reduce drag and delay Mcrit More stable in turbulence as they produce less lift and as a result they are less responsive to updraughts

662 kts

Local speed of sound = 39 x √(Temperature in Kelvin)

15°C in Kelvin is (15 + 273) = 288

So the local speed of sound = 39 x √288 = 662 kts

a line extending from the leading edge to the trailing edge equidistent from the upper and lower surface of the aerofoil.

+2.5G / -1.0G

Advection fog occurs when moist air passes over a cool surface by advection (wind) and is cooled.

It is common as a warm front passes over an area with significant snowpack, but it is most common at sea when tropical air encounters cooler waters, including areas of cold water upwelling, such as along the coast of California.

The angle between the chordline and the incoming airflow.

To varify the nose gear position (up or down).

Dihedral is the upward inclinitation of the wing from the root to the tip.

By using the formula: Range (nm) = 1.23(√H1 + √H2)

H1=height of transmitter (feet)

H2=height of receiver (feet)