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Performance - ATPL - Airline Transport Pilot license
Performance - ATPL - Airline Transport Pilot license
Test 10 domande Performance, tempo libero
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Nuovo Test!
1 - Considering VR, which statement is correct?
VR is the lowest climb speed after engine failure
In case of engine failure below VR the take-off should be aborted
VR is the speed at which rotation should be initiated
VR is the lowest speed for directional control in case of engine failure
2 - Which statement about reduced thrust is correct?
Reduced thrust is primarily a noise abatement procedure
Reduced thrust can be used when the actual take-off mass is less than the field length limited take-off mass
In case of reduced thrust V1 should be decreased
Reduced thrust is used in order to save fuel
3 - During a descent at constant Mach number, the margin to low speed buffet will:
Remain constant, because the Mach number remains constant.
Increase, because the lift coefficient increases.
Increase, because the lift coefficient decreases.
Decrease, because the lift coefficient decreases.
4 - During take-off the third segment begins:
When landing gear is fully retracted
When acceleration to flap retraction speed is started
When flap retraction is completed
When acceleration starts from VLOF to V2
5 - Refer to CAP698 Section 3 - MEP1 Figure 3.1 Normal Procedure Given:OAT -15 °CPressure Altitude: 4000' RWY 12RWind· 080/12 KTTake-off Mass: 4000 lbs Runway Surface: tarred and dryWhat is the minimum runway length? No stopway or clearway is available.
1250 ft
1750 ft
1950 ft
1550 ft
6 - The optimum altitude:
Decreases as mass decreases
Increases as mass decreases and is the altitude at which the specific range reaches its maximum
Is the altitude up to which cabin pressure of 8 000 ft can be maintained
Is the altitude at which the specific range reaches its minimum
7 - The force exactly opposing and balance lift in a glide descent is:
Thrust x sin(angle of descent)
Weight x sin(angle of descent)
Weight x cos(angle of descent)
Thrust x cos(angle of descent)
8 - The angle of climb with flaps extended, compared to that with flaps retracted, will normally be:
Larger
Smaller
Increase at moderate flap setting, decrease at large flap setting
Not change
9 - A twin engine aeroplane in cruise flight with one engine inoperative has to fly over high ground. In order to maintain the highest possible altitude the pilot should choose:
The long range speed
The speed corresponding to the minimum value of (lift / drag)^3/2
The speed corresponding to the maximum value of the lift / drag ratio
The speed at the maximum lift
10 - Given that the characteristics of a three engine turbojet aeroplane are as follows:Thrust = 50000 Newton / Engine g = 10 m/s2Drag = 72569 NMinimum steady gradient of climb (2nd segment) = 2.7% SIN (Angle of climb) = (Thrust - Drag) / WeightThe maximum take-off mass under 2nd segment conditions with 1 engine out is:
101596 kg
209064 kg
74064 kg
286781 kg
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