Principles of Flight - ATPL - Airline Transport Pilot license Page 2

ATPL - Airline Transport Pilot license Page 2

The pitch up effect of an aeroplane with swept wing in a stall is due to the	4 risposte
With increasing altitude and constant IAS the static lateral stability ( 1) and the dynamic lateral/directional stability ( 2) of an aeroplane with swept-back wing will:	4 risposte
During the take-off roll with a strong crosswind from the left, a four engine jet aeroplane with wing mounted engines experiences an engine failure above V1. Which engine causes the greatest control problem?	4 risposte
Differential aileron deflection:	4 risposte
If the elevator trim tab is deflected up, the cockpit trim indicator presents:	4 risposte
How can wing flutter be prevented?	4 risposte
Load factor is:	4 risposte
The positive manoeuvring limit load factor for a light aeroplane in the utility category in the clean configuration is:	4 risposte
The positive manoeuvring limit load factor for a large jet transport aeroplane with flaps extended is:	4 risposte
The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.42. An increase in angle of attack of 1 degree increases CL by 0.1. A vertical up gust instantly changes the angle of attack by 3 degrees. The load factor will be:	4 risposte

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