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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 takeoff 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 takeoff mass is less than the field length limited takeoff 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 takeoff 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 KTTakeoff 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 takeoff mass under 2nd segment conditions with 1 engine out is:
101596 kg
209064 kg
74064 kg
286781 kg
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