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moodle-efpn.portail.smartschool.defense.gouv.fr
032 Performance Aircraft

032 Performance Aircraft

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Which of the following statements are correct, concerning the determination of VMCG, the minimum control speed on the ground?

1. V_MC_G must be determined using rudder control alone.

2. During the V_MCG determination, the CG should be on the forward limit.

3. Reduced thrust may be used during the V_MCG determination.

4. The aircraft may NOT deviate more than 9.1 m (30 ft) laterally from the centre line

2 and 4

2 and з

1 and 4

1 and 3

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Aircraft-type-specific procedures for take-off and landing on contaminated runways can be found in the Operations Manual __ under Normal procedures.

Part A

Part C

Part D

Part B

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The one engine out take-off run is the distance between the brake release point and:

the lift-off point.

the point where V1 is reached.

50%

the middle of the segment between V_LOF point and 35 ft point.

the point half way between V1 and V2

50%

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Refer to figure.

Airport elevation: 3000 ft

Temperature: ISA +10°C

QNH: 1030 hPa

Landing mass: 8400 lb

Find the available Rate Of Climb of a twin piston engine aeroplane in case of Balked Landing, for the

given conditions:

2030 ft/min

1430 ft/min

1630 ft/min

100%

1760 ft/min

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A commercial air transport flight is to be conducted in a single-engined piston aircraft. At the most

critical point during the flight, the distance to be travelled to a safe landing place is 10 NM. Given the

following information, what is the lowest altitude the aircraft should fly over this critical point?

Terrain elevation: 0 ft

Gross glide gradient: 10%

TAS: 110 kt

Expected tailwind component: 20 kt

1 NM = 6080 ft

Still air distance = (height difference / net gradient) × 100

Ground distance = Still Air Distance × (GS / TAS)

5800 ft

6200 ft

5400 ft

5100 ft

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Refer to figure.

Determine the landing climb limit for the MRJT, given:

Icing conditions occur during the flight.

61 800 kg

58 100 kg

62 250 kg

59 500 kg

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How does the thrust of a propeller vary during take-off run, assuming unstalled flow conditions at the

propeller blades? The thrust...

has no change during take-off and climb.

decreases while the aeroplane speed builds up

increases while the aeroplane speed builds up

100%

varies with mass changes only.

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A pilot is flying to a destination close to the aeroplane maximum range, flying at maximum range cruise speed, with NOsignificant forecast winds. However, during the flight the pilot experienced a headwind. To achieve maximum range overthe ground, the pilot should…

Decrease the airspeed compared to the speed for maximum cruise with NO wind.

Fly at an airspeed equal to the maximum endurance speed.

Increase the airspeed compared to the speed for maximum cruise with NO wind.

Continue to fly at an airspeed equal to speed for maximum cruise with NO wind.

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Refer to figure.

Which of the following graphs illustrate the power change with decreasing altitude?