During climb with all engines the altitude where the rate of climb reduces to ? [ Attainment AIM ]

Question 82-1 : Service ceiling absolute ceiling thrust ceiling aerodynamic ceiling

The maximum rate of climb that can be maintained at the absolute ceiling is ?

Question 82-2 : 0 ft/min 125 ft/min 500 ft/min 100 ft/min

A twin engine aeroplane is flying at the minimum control speed with take off ?

Question 82-3 : Straight flight straight flight and altitude heading altitude and a positive rate of climb of 100 ft/min altitude

The speed v2 is ?

Question 82-4 : The take off safety speed that speed at which the pic should decide to continue or not the take off in the case of an engine failure the lowest airspeed required to retract flaps without stall problems the lowest safety airspeed at which the aeroplane is under control with aerodynamic surfaces in the case of an engine failure

Which take off speed is affected by the presence or absence of stopway and/or ?

Question 82-5 : V1 v2 vmcg vmca

Maximum and minimum values of v1 are limited by ?

Question 82-6 : Vr and vmcg v2 and vmca vr and vmca v2 and vmcg

Take off run is defined as the ?

Question 82-7 : Horizontal distance along the take off path from the start of the take off to a point equidistant between the point at which vlof is reached and the point at which the aeroplane is 35 ft above the take off surface distance to v1 and stop assuming an engine failure at v1 distance to 35 feet with an engine failure at v1 or 115% all engine distance to 35 feet distance from brake release to v2

The minimum value of v2 must exceed vmc by ?

Question 82-8 : 10% 15% 20% 30%

Which of the following is true according to the relevant regulations for turbo ?

Question 82-9 : Maximum landing distance at the destination aerodrome and at any alternate aerodrome is 0 7 x lda landing distance available maximum landing distance at destination is 0 95 x lda landing distance available maximum take off run is 0 5 x runway maximum use of clearway is 1 5 x runway

For take off obstacle clearance calculations obstacles may be avoided ?

Question 82-10 : By banking not more than 15° between 50 ft and 400 ft above the runway elevation by banking as much as needed if aeroplane is more than 50 ft above runway elevation only by using standard turns by standard turns but only after passing 1500 ft

The speed vr ?

Question 82-11 : Is the speed at which rotation to the lift off angle of attack is initiated must be higher than v2 must be higher than vlof must be equal to or lower than v1

If the take off mass of an aeroplane is brake energy limited a higher uphill ?

Question 82-12 : Increase the maximum mass for take off decrease the maximum mass for take off have no effect on the maximum mass for take off decrease the required take off distance

If the take off mass of an aeroplane is tyre speed limited downhill slope would ?

Question 82-13 : Have no effect on the maximum mass for take off decrease the maximum mass for take off increase the maximum mass for take off increase the required take off distance

The take off mass could be limited by ?

Question 82-14 : The take off distance available toda the maximum brake energy and the climb gradient with one engine inoperative the take off distance available toda only the maximum brake energy only the climb gradient with one engine inoperative only

The climb limited take off mass can be increased by ?

Question 82-15 : A lower flap setting for take off and selecting a higher v2 selecting a lower v1 selecting a lower v2 selecting a lower vr

In the event that the take off mass is obstacle limited and the take off flight ?

Question 82-16 : 15 degrees up to height of 400 ft 10 degrees up to a height of 400 ft 20 degrees up to a height of 400 ft 25 degrees up to a height of 400 ft

Which speed provides maximum obstacle clearance during climb ?

Question 82-17 : The speed for which the ratio between rate of climb and forward speed is maximum v2 + 10 kt the speed for maximum rate of climb v2

The take off mass of an aeroplane is restricted by the climb limit what would ?

Question 82-18 : None the effect would vary depending upon the height of any obstacle within the net take off flight path the climb limited take off mass would increase the climb limited take off mass would decrease

If other factors are unchanged the fuel mileage nautical miles per kg is ?

Question 82-19 : Lower with a forward centre of gravity position independent from the centre of gravity position lower with an aft centre of gravity position higher with a forward centre of gravity position

Considering a rate of climb diagram rate of climb versus tas for an aeroplane ?

Question 82-20 : Diagram a diagram b diagram c diagramd

What is the effect of increased mass on the performance of a gliding aeroplane ?

Question 82-21 : The speed for best angle of descent increases there is no effect the gliding angle decreases the lift/drag ratio decreases

Which force compensates the weight in unaccelerated straight and level flight ?

Question 82-22 : The lift the thrust the drag the resultant from lift and drag

In which of the flight conditions listed below is the thrust required equal to ?

Question 82-23 : In level flight with constant ias in accelerated level flight in a climb with constant ias in a descent with constant tas

The load factor in a turn in level flight with constant tas depends on ?

Question 82-24 : The bank angle only the radius of the turn and the bank angle the true airspeed and the bank angle the radius of the turn and the weight of the aeroplane

The induced drag of an aeroplane ?

Question 82-25 : Decreases with increasing airspeed decreases with increasing gross weight is independent of the airspeed increases with increasing airspeed

The induced drag of an aeroplane at constant mass in un accelerated level ?

Question 82-26 : The lowest achievable speed in a given configuration vs1 vmo va

The point where drag coefficient/lift coefficient is a minimum is ?

Question 82-27 : The lowest point of the drag curve the point where a tangent from the origin touches the drag curve at stalling speed vs on the 'back side' of the drag curve

On the power versus tas graph for level flight the point at which a tangent ?

Question 82-28 : Is the point where the lift to drag ratio is a maximum is the point where drag coefficient is a minimum is the point where the lift to drag ratio is a minimum is the maximum drag speed

Assuming the gross mass altitude and airspeed remain unchanged moving the ?

Question 82-29 : Decreases the induced drag and reduces the power required increases the power required affects neither drag nor power required increases the induced drag

Compared to a more forward position a centre of gravity close to but not beyond ?

Question 82-30 : Improves the maximum range increases the stalling speed improves the longitudinal stability decreases the maximum range

The intersections of the thrust available and the drag curve are the operating ?

Question 82-31 : In unaccelerated level flight in descent with constant ias in accelerated level flight in unaccelerated climb

In straight horizontal steady flight at speeds below that for minimum drag ?

Question 82-32 : A lower speed requires a higher thrust the aeroplane can be controlled only in level flight a higher speed requires a higher thrust the aeroplane can not be controlled manually

A lower airspeed at constant mass and altitude requires ?

Question 82-33 : A higher coefficient of lift less thrust and a lower coefficient of lift more thrust and a lower coefficient of lift more thrust and a lower coefficient of drag

The coefficient of lift can be increased either by flap extension or by ?

Question 82-34 : Increasing the angle of attack increasing the tas decreasing the 'nose up' elevator trim setting increasing the cas

When flying the 'backside of thrust curve' means ?

Question 82-35 : A lower airspeed requires more thrust the thrust required is independent of the airspeed a thrust reduction results in an acceleration of the aeroplane a lower airspeed requires less thrust because drag is decreased

'maximum endurance' ?

Question 82-36 : Is achieved in unaccelerated level flight with minimum fuel flow is the same as maximum specific range with wind correction can be flown in a steady climb only can be reached with the 'best rate of climb' speed in level flight

The speed for maximum endurance ?

Question 82-37 : Is always lower than the speed for maximum specific range is the speed at which the aeroplane achieves 99% of maximum specific range can be either higher or lower than the speed for maximum specific range is always higher than the speed for maximum specific range

Which of the equations below defines specific range sr ?

Question 82-38 : Sr = true airspeed/total fuel flow sr = indicated airspeed/total fuel flow sr = mach number/total fuel flow sr = groundspeed/total fuel flow

To achieve the maximum range over ground with headwind the airspeed should be ?

Question 82-39 : Higher compared to the speed for maximum range cruise with no wind equal to the speed for maximum range cruise with no wind lower compared to the speed for maximum range cruise with no wind reduced to the gust penetration speed

Can the length of a stopway be added to the runway length to determine the take ?

Question 82-40 : No no unless its centreline is on the extended centreline of the runway but the stopway must be able to carry the weight of the aeroplane but the stopway must have the same width as the runway