A high wing location like the BAE and the Fokker give a natural stable contribution.

This is because the Center of Gravity is underneath the wing, therefore when disturbed the C.G. provides a positive momentum opposite to the distortion.

Decreasing speed, by reducing engine power or pitching up.

For every 1kg of air passing through the combustion chamber, 11kg of air pass bypass the combustion chamber.

Mcrit

NDB’s are stations emitting a signal. There is nothing for them to be accurate about. ADF's on the other hand, when tuned to an NDB need to be accurate within +/- 5 degrees.

Enhanced Ground Proximity Warning System, provides a greater level of detection than GPWS.

EGPWS is capable of ‘looking ahead’ to identify potential risks on the aircraft flight path as it includes a terrain and obstacle database.

Wing loading is the loaded weight of the aircraft divided by the area of the wing.

The faster an aircraft flies, the more lift is produced by each unit area of the wing. Correspondingly, the landing and take-off speeds will be higher and the high wing loading also decreases maneuverability.

A variable pitch propeller provides an optimum angle of attack for the propeller blades for a longer range which reduces fuel usage. Fixed pitch propellers are easier to produce and maintain, but reach maximum efficient at only one specific airspeed.

Depends on the engine.

In the case of the 737-800 CFM56, 27,300lbs total thrust at a ratio of 5.5:1

Jet streams are narrow bands of high-speed upper thermal winds at very high altitudes.