Two identical aeroplanes mass 1500 kg commence a 20◦ banked turn. Aeroplane A flies at 130 kt and aeroplane B flies at 200 kt. Which of the following statements is correct?

(d) The rate of turn for A is greater than the rate of turn for B.

(a) The load factor for A is greater than the load factor for B.

(b) The turn radius for A is greater than the turn radius for B.

(c) The Cl for A is smaller than the Cl for B.

(d) increases during a constant IAS descent

(a) is always greatest after a step climb

(b) decreases during a constant Mach number descent

(c) is always positive below Mmo

(b) the maximum speed at which maximum upelevator deflection is permitted

(a) the speed that should not be exceeded in a climb

(c) the maximum speed at which rolls are permitted

(d) the turbulence speed for transport aeroplanes

(d) should not be greater than Vc

(a) should be chosen between Vc and Vd

(b) is equal to the design speed for maximum gust intensity

(c) is the calibrated airspeed at which Mmo is reached at FL350

In a level, coordinated turn the load factor n (i) . . .. . ...and the stalling speed Vs (ii) . . .. . .. . . are:

(ii) higher than in straight and level flight

(a) (i) less than 1; (ii) lower than in straight and level flight

(b) (i) more than 1; (ii) lower than in straight and level flight

(c) (i) less than 1; (ii) higher than in straight and level flight (d) (i) more than 1;

Exceeding Va by a small amount may result in:

(a) permanent structural damage if the elevator is deflected fully up

(b) structural failure if the elevator is deflected fully up

(c) permanent structural damage because of excessive dynamic pressure

(d) structural failure if a turn is executed

At high altitude an aeroplane flies at a Mach number that ensures a 0.3g buffet margin. So that the buffet margin is increased to 0.4g at the same speed the pilot must:

(a) increase the angle of attack

(c) extend the flaps to the take-off setting

If there is only one fixed value of Va it is:

(a) the speed at which the aeroplane will stall at the manoeuvring load factor at the MTOM

(b) the maximum speed in smooth air

(c) the speed that ensures that the maximum manoeuvring load factor is not exceeded with unrestricted use of the elevators

(d) the speed to be used in rough air

Regarding the gust load of an aeroplane for every other factor remains constant, which of the following statements is correct: (i) the gust load increases when the mass decreases. (ii) the gust load increases when the altitude increases.

(c) (i) correct; (ii) incorrect

(a) (i) incorrect; (ii) incorrect

(b) (i) incorrect; (ii) correct

Regarding the gust load of an aeroplane if every other factor remains constant, which of the following statements is correct: (i) the gust load increases with increased aspect ratio of the wing. (ii) the gust load increases when the speed increases.

(b) (i) incorrect; (ii) correct

(c) (i) incorrect; (ii) incorrect

(d) (i) correct; (ii) incorrect

Is it permissible for a transport aeroplane to exceed the ‘buffet-onset Mach number?

(b) Yes, to fly faster at extremely high altitudes.

To maintain altitude and airspeed during a turn the pilot must:

(b) increase the angle of attack and increase the thrust

(a) increase the angle of attack

(c) a dorsal fin (c) increase the thrust

(d) decrease the radius of the turn

The effect that mass has on the radius of turn for the same bank angle is that:

(c) mass does not affect the radius of turn

(a) it increases proportionately as mass increases

(b) it decreases proportionately as mass increases

(d) it increases proportionately as mass decreases

To maintain a constant Mach number in a level turn the pilot has to increase:

(b) the angle of attack and increase the thrust

(a) the angle of attack and maintain the thrust setting

(c) the thrust and maintain the same angle of attack

(d) the thrust and decrease the angle of attack

The manner in which a pilot can increase the rate of turn and decrease the radius of turn simultaneously is to:

(d) increase the bank angle and decrease the airspeed

(a) increase the bank angle and increase the airspeed

(b) decrease the bank angle and increase the airspeed

(c) decrease the bank angle and decrease the airspeed

In a minimum radius turn if the flap is lowered:

(c) decrease the turn radius provided that there is sufficient excess thrust to maintain a safe speed and the Vfe is not a factor

(b) increase the turn radius provided that there is sufficient thrust to prevent the aeroplane from stalling and that Vle is not a factor

(d) increase the rate of turn but not affect the turn radius

Which of the following statements regarding Va is correct?

(c) Va = Vs1g × n2 (c) Full control deflection is possible without exceeding the limiting load factor up to Va.

(a) At speeds below Va stalling with full control deflection will damage the airframe.

(b) In normal operations Va should never be exceeded.

(d) Manoeuvring the aeroplane at speeds in excess of Va will permanently damage the airframe.

Va is the speed to be used as the maximum:

(c) speed at which maximum nose-up-elevator deflection is permitted

(a) turbulence speed for transport aeroplanes

(b) climbing speed for transport aeroplanes

(d) 2.5(d) descending speed for transport aeroplanes

If the maximum cruise altitude limited by the minimum load factor is exceeded:

(d) Mach buffet may be induced by turbulence

(a) 4.4(a) the load factor may be exceeded if turbulence is encountered

(b) the load factor may be exceeded if a sudden turn is made (

c) Mach buffet will be immediately experienced

JEREMY:)

Authored by Charlie Cajeta

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MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In steady horizontal flight the Cl of an aeroplane is 0.35. A one-degree increase in the AoA increases the Cl by 0.079. A vertical gust of air instantly changes the AoA by two degrees. The new load factor is:

1.9

1.45

0.9

0.45

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

In a gust, which combination of speeds is applicable for the structural strength of an aeroplane in the clean configuration at MSL?

28 fps and Vd

66 fps at all speeds

66 fps and Vb

56 fps and Vc

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The load factor that determines Va is the:

(a) gust load factor at 66 fps

(b) manoeuvring flap limit load factor

(d) manoeuvring ultimate load factor

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The data that may be obtained from a buffetonset boundary chart is:

(a) Mmo for various masses and altitudes

(b) Mcrit for various masses and altitudes

(d) the low-speed and the high-speed buffet Mach numbers for various masses and altitudes

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The manoeuvring load factor positive limit for a utility category light aeroplane in the clean configuration is:

(a) 6.0

(b) 4.4

(d) 3.8

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Two aeroplanes at different masses execute a 20◦ banked turn at 150 kt IAS. The heavier aeroplane will:

(a) have a greater rate of turn than the lighter aeroplane

(b) turn at the same radius as the lighter aeroplane

(d) have a smaller radius of turn than the lighter aeroplane

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

To maintain altitude and speed when an aeroplane is rolled into a turn the pilot must
(i) . . .. . .. . .. . .the thrust:
(ii) . . .. . .. . .. . .. . .the angle of attack.

(a) (i) maintain; (ii) increase

(b) (i) increase; (ii) increase

(d) (i) increase; (ii) decrease

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JEREMY:)

In steady horizontal flight the Cl of an aeroplane is 0.35. A one-degree increase in the AoA increases the Cl by 0.079. A vertical gust of air instantly changes the AoA by two degrees. The new load factor is:

In a gust, which combination of speeds is applicable for the structural strength of an aeroplane in the clean configuration at MSL?

The load factor that determines Va is the:

The data that may be obtained from a buffetonset boundary chart is:

The manoeuvring load factor positive limit for a utility category light aeroplane in the clean configuration is:

Two aeroplanes at different masses execute a 20◦ banked turn at 150 kt IAS. The heavier aeroplane will:

To maintain altitude and speed when an aeroplane is rolled into a turn the pilot must
(i) . . .. . .. . .. . .the thrust:
(ii) . . .. . .. . .. . .. . .the angle of attack.

The limiting load factor for a large transport aeroplane in the manoeuvring diagram is:

Two identical aeroplanes mass 1500 kg commence a 20◦ banked turn. Aeroplane A flies at 130 kt and aeroplane B flies at 200 kt. Which of the following statements is correct?

Given: TAS 300 kt; Bank angle 45◦; g = 10 m/s2. The turn radius is:

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JEREMY:)

In steady horizontal flight the Cl of an aeroplane is 0.35. A one-degree increase in the AoA increases the Cl by 0.079. A vertical gust of air instantly changes the AoA by two degrees. The new load factor is:

In a gust, which combination of speeds is applicable for the structural strength of an aeroplane in the clean configuration at MSL?

The load factor that determines Va is the:

The data that may be obtained from a buffetonset boundary chart is:

The manoeuvring load factor positive limit for a utility category light aeroplane in the clean configuration is:

Two aeroplanes at different masses execute a 20◦ banked turn at 150 kt IAS. The heavier aeroplane will:

To maintain altitude and speed when an aeroplane is rolled into a turn the pilot must (i) . . .. . .. . .. . .the thrust: (ii) . . .. . .. . .. . .. . .the angle of attack.

The limiting load factor for a large transport aeroplane in the manoeuvring diagram is:

Two identical aeroplanes mass 1500 kg commence a 20◦ banked turn. Aeroplane A flies at 130 kt and aeroplane B flies at 200 kt. Which of the following statements is correct?

Given: TAS 300 kt; Bank angle 45◦; g = 10 m/s2. The turn radius is:

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To maintain altitude and speed when an aeroplane is rolled into a turn the pilot must
(i) . . .. . .. . .. . .the thrust:
(ii) . . .. . .. . .. . .. . .the angle of attack.