The tailplane of a Seneca has an elevator and a trim tab, what does a Boeing 737 have?

The tailplane of a Seneca has an elevator and a trim tab, what does a Boeing 737 have?

The Boeing 737 has an all moving horizontal stabilizer.

What is the range of a VOR at 32000ft?

What is the range of a VOR at 32000ft?

Range = 1.23(√H1 + √H2)

= 1.23 * √32000

= 220 nm

On a tapered wing, where would the stall occur first?

On a tapered wing, where would the stall occur first?

At the tip as downwash and spanwise flow effect the angle of attack at each section, but because of the tapered wing the effective angle of attack near the tips is greater than that near the center.

If you are outside the range of any VOR’s/NDB's, how does the aircraft know where it is?

If you are outside the range of any VOR’s/NDB's, how does the aircraft know where it is?

Via INS/IRS/GPS

What are the advantages of swept wings?

What are the advantages of swept wings?

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

Why does a swept wing increase Mcrit?

Why does a swept wing increase Mcrit?

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

Which flight will take the shortest time, from London to New York or New York to London?

Which flight will take the shortest time, from London to New York or New York to London?

New York to London (flying east) would take less time because of the Polar front westerly jet stream.

At high altitudes, what speed do aircrafts climb on?

At high altitudes, what speed do aircrafts climb on?

Mach number

What are the benefits of a free turbine?

What are the benefits of a free turbine?

A free turbine is a turbine that is not directly connected to the compressor. This allows the compressor to rotate at a different speed than the turbine. Since the turbine speed is coupled with the propeller, this allows for the propeller to be maintained at a constant ideal speed.

Another advantage is that free turbine engines can be designed to be more compact than their single shaft counterparts

Describe the take off segments.

Describe the take off segments.

1st segment starts at screen height and finishes at gear retracted.

2nd segment starts when the gear is retracted and finishes when acceleration alt is reached (min. 400ft max 1000ft) speed V2.

3rd segment starts at acceleration alt, minimum 400ft, and finishes when the flaps are retracted.

4th segment starts when the flaps are retracted, MCT is set and finishes at the 1500ft.

You have reached the end of the test!Share LinkFinish