Class b aircraft take off – Air – DGCA Question Bank For Politics

#1. For a single engine Class B aeroplane, how does runway slope affect allowable take-off mass, assuming other factors remain constant and not limiting?

An uphill slope decreases take-off mass.

Allowable take-off mass is not affected by runway slope

A downhill slope decreases allowable take-off mass

A downhill slope increases allowable take-off mass

#2. For this question use Performance Manual CAP 698 SEP 1 Figure 2.1. With regard to the take-off performance chart for the single engine aeroplane, determine the take-off speed for (1) rotation and (2) at a height of 50ft. Given:- O.A.T : ISA + 10 Pressure Altitude: 5,000 ft, Aeroplane mass: 3,400 IBS, Headwind component: 5 kt, Flaps: up, Runway: Tarred and Dry

73 and 84 kt

68 and 78 kt

65 and 75 kt

71 and 82 kt

#3. For this question use Performance Manual CAP 698 SEP 1 Figure 2.2. With regard to the take-off performance chart for the single engine aeroplane determine the take-off distance over a 50ft obstacle height. Given:- O.A.T : 30°C, Pressure Altitude: 1,000ft, Aeroplane Mass: 2,950 IBS, Tailwind component: 5kt, Flaps: Approach setting, Runway: Short, wet grass, firm subsoil, Correction factor: 1.25 for the current runway conditions.

1,700ft

2,500ft

2,200ft

1,900ft

#4. For this question use Performance Manual CAP 698 SEP 1 Figure 2.1. With regard to the take off performance chart for the single engine aeroplane determine the maximum allowable take off mass. Given:- O.A.T : ISA, Pressure Altitude : 4,000ft, Headwind component : 5kt, Flaps : up, Runway : Tarred and Dry, Factored runway length : 2,000ft, Obstacle height : 50ft

3,000 IBS

2,900 IBS

3,650 IBS

3,200 IBS

#5. For this question use Performance Manual CAP 698 SEP 1 Figure 2.1. With regard to the take-off performance chart for the single engine aeroplane determine the take-off distance to a height of 50ft. Given:- O.A.T: 30°C, Pressure Altitude: 1,000ft, Aeroplane Mass: 3,450 IBS, Tailwind component: 2.5 kt, Flaps: up, Runway: Tarred and Dry.

approximately: 2,200 feet

approximately: 2,400 feet

approximately: 1,400 feet

approximately: 2,800 feet

#6. For this question use Performance Manual CAP 698 SEP 1 Figure 2.2. With regard to the take-off performance chart for the single engine aeroplane determine the take-off distance to a height of 50ft. Given:- O.A.T:- 7°C, Pressure Altitude: 7,000ft, Aeroplane Mass: 2,950 Ibs, Headwind component: 5kt, Flaps: Approach setting, Runway: Tarred and Dry.

approximately: 1,150 ft

approximately: 2,450 ft

approximately: 1,500 ft

approximately: 2,100 ft

#7. For this question use Performance Manual CAP 698 SEP 1 Figure 2.1. With regard to the take-off performance chart for the single engine aeroplane determine the take-off distance to a height of 50ft. Given:- Airport characteristics: hard, dry and zero slope runway, Pressure altitude: 1,500ft, Outside air temperature: +18°C, wind component: 4 knots tailwind, Take-off mass: 1,270 kg.

520m

415m

440m

615m

#8. For this question use Performance Manual CAP 698 SEP 1 Figure 2.2. With regard to the take-off performance chart for the single engine aeroplane determine the take-off distance to a height of 50 ft. Given:- O.A.T: 38°C, Pressure Altitude: 4,000 ft, Aeroplane Mass: 3,400 Ibs, Tailwind component: 5 kt, Flaps: Approach setting, Runway: Dry Grass, Correction factor: 1.2

approximately: 3,250 ft

approximately: 4,200 ft

approximately: 5,040 ft

approximately: 3,900 ft

#9. For a Class B aircraft at an aerodrome with no stopway or clearway, the minimum length of Take-off Run that must be available to satisfy the take-off requirements:

Must not be less than the gross take off distance to 50ft.

Must not be less than 1.15 times the gross take off distance to 50ft.

Must not be less than 1.25 times the gross take off distance to 50ft.

Must not be less than 1.3 times the gross take off distance to 50ft

#10. For a single engine Class B aircraft, the rotation speed VR:

Must not be less than 1.1 VS1

Must not be less than VS1

Must not be less than 1.2 VMC

Must not be less than VMC

#11. For a single engine Class B aircraft at an aerodrome with stopway:

The TOD x 1.3 must not exceed the ASDA.

The TOD must not exceed the ASDA x 1.3.

The TOD x 1.25 must not exceed the ASDA.

The TOD must not exceed the ASDA x 1.25.

Dgca Question Bank For Pilots

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#1. For a single engine Class B aeroplane, how does runway slope affect allowable take-off mass, assuming other factors remain constant and not limiting?

#9. For a Class B aircraft at an aerodrome with no stopway or clearway, the minimum length of Take-off Run that must be available to satisfy the take-off requirements:

#10. For a single engine Class B aircraft, the rotation speed VR:

#11. For a single engine Class B aircraft at an aerodrome with stopway: