Q&A Forum
1118 questions found
When in reverse pitch, CTM will tend to move the propeller blades towards
- a positive pitch.
- a position depending on rpm.
- a negative pitch.
i dont understand it.
Auto feathering is disarmed
- during landing.
- during take off.
- in the cruise.
why is it disarmed during cruise?Wouldnt be right to have it auto while crusing in case of engine failure?
In what position is the constant-speed propeller control placed to check the magnetos?
- Full decrease, low propeller blade pitch angle.
- Full increase, low propeller blade pitch angle.
- Full increase, high propeller blade pitch angle.
what are magnetos?
A rotating propeller imparts rearwards motion to a
- small mass of air at high velocity.
- large mass of air at low velocity.
- small mass of air at low velocity.
i dont understand
The purpose of using reverse pitch propellers is to
- provide aerodynamic breaking.
- allow aircraft to taxi backwards.
- reverse the direction of rotation of the propeller.
isnt the B also right?