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Performance - ATPL - Airline Transport Pilot license
Performance - ATPL - Airline Transport Pilot license
Test 10 domande Performance, tempo libero
Cambia Materia
Nuovo Test!
1 - What is the result of a large take off flap setting compared to a small take off flap setting on required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM)?
Increased TOD required and decreased field length limited TOM
Decreased TOD required and increased field length limited TOM
Decreased TOD required and decreased field length limited TOM
Increased TOD required and increased field length limited TOM
2 - Field length is balanced when:
Calculated V2 is less than 110% VMCA and V1
Take-off distance available equals accelerate stop distance available
One engine acceleration from V1 to VLOF plus flare distance between VLOF and 35 feet are equal
All engine acceleration to V1 and braking distance for rejected take-off are equal
3 - An aeroplane executes a steady glide at the speed for minimum glide angle. If the forward speed is kept constant, what is the effect of a lower mass? Rate of descent / Glide angle / CL / CD ratio
Increases / increases / decreases
Increases / constant / increases
Increases / increases / constant
Decreases / constant / decreases
4 - When compared to still air conditions, a constant headwind component:
Increases the best rate of climb
Decreases the angle of climb
Increases the angle of flight path during climb
Increases the maximum endurance
5 - The danger associated with low speed and/or high speed buffet
Can be reduced by increasing the load factor.
Limits the manoeuvring load factor at high altitudes.
Has to be considered at take-off and landing.
Exists only above MMO.
6 - The intersections of the thrust available and the drag curve are the operating points of the aeroplane
In accelerated level flight.
In descent with constant IAS.
In unaccelerated climb.
In unaccelerated level flight.
7 - To minimize the risk of hydroplaning during landing the pilot should:
Use maximum reverse thrust, and should start braking below the hydroplaning speed.
Use normal landing-, braking- and reverse technique.
Make a 'positive' landing and apply maximum reverse thrust and brakes as quickly as possible.
Postpone the landing until the risk of hydroplaning no longer exists.
8 - V1 has to be:
Equal to or higher than VMCG
Equal to or higher than V2
Higher than VR
Equal to or higher than VMCA
9 - The drift down procedure specifies requirements concerning the:
Engine power at the altitude at which engine failure occurs.
Climb gradient during the descent to the net level-off altitude.
Obstacle clearance after engine failure.
Weight during landing at the alternate.
10 - A higher pressure altitude at ISA temperature:
Increases the climb limited take-off mass
Decreases the take-off distance
Has no influence on the allowed take-off mass
Decreases the field length limited take-off mass
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