GsPilot

1/30

Question ID: 107388

With a positive rate of climb, the difference between the climb angle and the climb gradient is that the gradient?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Is stated in degrees, the angle in percentage

B

Represents the angle variation

C

Depends on the mass, while the angle is independent of the mass

D

Value is always higher than the angle value

2/30

Question ID: 107326

An airline operator shall make sure that if the aircraft planned for the flight is a performance class B aeroplane, it will be able, throughout its flight route or its alternate route scheduled from this initial route, to reach a climb rate of at least?

This question has been flagged as being in an exam by multiple students, give it more attention

A

500 ft/min with all engines operating at maximum cruise power

B

500 ft/min with one engine inoperative and all the others operating at maximum continuous power

C

300 ft/min with one engine inoperative and all the others operating at maximum continuous power

D

300 ft/min with all engines operating at maximum continuous power

3/30

Question ID: 107462

In accordance to EASA CS-25 which of the following listed speeds are used for determination of V2 MIN?

This question has been flagged as being in an exam by multiple students, give it more attention

A

V1, VR

B

VSO, VMCA

C

VMCG, V2

D

VSR, VMCA

4/30

Question ID: 107318

What happens to Specific Range (SR) for a heavier aircraft?

This question has been flagged as being in an exam by multiple students, give it more attention

A

SR stays constant

B

SR increases

C

SR improves above Maximum Zero Fuel Mass

D

SR reduces

5/30

Question ID: 109880

On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kts and the holding speed (minimum fuel burn per hour) is 95 kts

The best rate of climb speed will be obtained for a speed?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Between 95 and 125kts

B

Equal to 95 kts

C

< 95 kts

D

Equal to 125kts

6/30

Question ID: 109762

If the maximum Take-off Mass is limited by tire speed, what affect would a down sloping runway have?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Always increase the mass

B

No effect

C

Only increase the mass if not limited by any other limitation

D

Decrease the mass

7/30

Question ID: 111080

What is the climb requirement in the 3rd take off segment?

This question has been flagged as being in an exam by multiple students, give it more attention

A

200FT per minute

B

400FT per minute

C

There is no climb requirements

D

1500FT per minute

8/30

Question ID: 107572

With regard to the drift down performance of the twin jet aeroplane,\
Why does the curve representing 35 000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Because at this mass it takes about 4 minutes to decelerate to the optimum speed for drift down at the original cruising level

B

Because at this mass the engines slow down at a slower rate after failure, there is still some thrust left during three minutes

C

All the curves start at the same point, which is situated outside the chart

D

Due to higher TAS at this mass it takes more time to develop the optimal rate of descent, because of the inertia involved

9/30

Question ID: 107578

SEP 1 Figure 2.4
With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50 ft?
Given O.A.T ISA
Pressure Altitude 1000 ft
Aeroplane Mass 3500 lb
Tailwind component 5 kt
Flaps Landing position (down)
Runway Tarred and Dry

This question has been flagged as being in an exam by multiple students, give it more attention

A

Approximately: 1700 feet

B

Approximately: 1500 feet

C

Approximately: 920 feet

D

Approximately: 1150 feet

10/30

Question ID: 107499

On take-off from an un-balanced field you have an available range of V1s. If a higher V1 is selected from the range then?

This question has been flagged as being in an exam by multiple students, give it more attention

A

The all engine take-off distance will be unaffected

B

The ASDR will decrease

C

Both TOD and ASD will increase

D

Both TOD and ASD will decrease

11/30

Question ID: 110414

According to EASA AIR OPS, for turbo-prop aeroplanes, the required runway length at a destination airport is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Less then that required at an alternate airport

B

More than that required at an alternate airport

C

The same as that required at an alternate airport

D

60% greater than that required at an alternate airport

12/30

Question ID: 107573

What is the minimum field length required for the worst wind situation, landing a twin jet aeroplane with the anti-skid inoperative?
Given:
Elevation 2000 ft
QNH 1013 hPa
Landing Mass 50000 kg
Flaps as required for minimum landing distance
Runway condition dry
Maximum allowable tailwind 15kts
Maximum allowable headwind 50 kts

This question has been flagged as being in an exam by multiple students, give it more attention

A

2700 m

B

2900 m

C

2600 m

D

3100 m

13/30

Question ID: 110177

With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Lower than the angle of attack corresponding to maximum endurance

B

Equal to the angle of attack corresponding to maximum endurance

C

Equal to the angle of attack corresponding to maximum lift to drag ratio

D

Equal to the angle of attack corresponding to zero induced drag

14/30

Question ID: 110159

For a jet transport aeroplane, which of the following is the reason for the use of 'maximum range speed'?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Minimum drag

B

Minimum fuel flow

C

Minimum specific fuel consumption

D

Longest flight duration

15/30

Question ID: 111039

What is the maximum semi-width of the obstacle domain for an aircraft of wingspan 52m that can maintain navigational accuracy and is not required to turn more than 15° degrees after take-off. The obstacle is 2200m from the end of TODA?

This question has been flagged as being in an exam by multiple students, give it more attention

A

300m

B

600m

C

361m

D

365m

16/30

Question ID: 110969

Regarding the obstacle limited take-off mass, which of the following statements is correct?

This question has been flagged as being in an exam by multiple students, give it more attention

A

The obstacle limited mass can never be lower than the climb limited take-off mass

B

Wind speed plays no role when calculating this particular mass

C

A take-off in the direction of an obstacle is also permitted in tail wind condition

D

The maximum bank angle which can be used is 10°

17/30

Question ID: 108972

Gross performance is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

65 percent of net performance

B

The maximum performance which a fleet of aeroplanes should achieve if satisfactorily maintained and flown in accordance with the techniques described in the manual

C

The average performance which a fleet of aeroplanes should achieve if satisfactorily maintained and flown in accordance with the techniques described in the manual

D

The minimum performance which a fleet of aeroplanes should achieve if satisfactorily maintained and flown in accordance with the techniques described in the manual

18/30

Question ID: 110946

Which of the following will affect the level-off altitude during a drift-down?
1) Outside air temperature
2) Wind
3) Distance to alternate airport
4) Engine thrust

This question has been flagged as being in an exam by multiple students, give it more attention

A

1,4

B

2,4

C

1,2,4

D

1,2,3,4

19/30

Question ID: 111021

The result of a higher flap setting up to the optimum at take-off is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

A higher V1

B

A longer take off run

C

A shorter ground roll

D

An increased acceleration

20/30

Question ID: 107533

CAP 698 Figure 2.3
Using the climb performance chart, for the single-engine aeroplane, determine the ground distance to reach a height of 1 500 ft above the reference zero in the following conditions, given?

OAT at Take-off ISA
Airport pressure altitude 5000 ft
Aeroplane mass 3200 lbs
Speed 100 KIAS
Wind component 5 kts tailwind

This question has been flagged as being in an exam by multiple students, give it more attention

A

13900 ft

B

14900 ft

C

16900 ft

D

20200 ft

21/30

Question ID: 111943

Reduced take-off thrust should normally not be used when?

This question has been flagged as being in an exam by multiple students, give it more attention

A

The runway is wet

B

Windshear is reported on the take-off path

C

The runway is dry

D

It is dark

22/30

Question ID: 110152

A jet aeroplane is climbing at constant Mach number below the tropopause.
Which of the following statements is correct?

This question has been flagged as being in an exam by multiple students, give it more attention

A

IAS increases and TAS decreases

B

IAS increases and TAS increases

C

IAS decreases and TAS increases

D

IAS decreases and TAS decreases

23/30

Question ID: 107914

A clearway?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Provides an area over which an aeroplane can safely transit from lift off to the required height

B

Need not have the same weight bearing qualities as the runway with which it is associated

C

May be water

D

All of the above

24/30

Question ID: 107382

Given:

Still Air climb gradient 7.5%

TAS 140 kts

Wind component 25 kts head

What is the effective wind climb gradient?

This question has been flagged as being in an exam by multiple students, give it more attention

A

8.5%

B

5.8%

C

9.1%

D

6.1%

25/30

Question ID: 107650

The TODA is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Declared runway length only

B

Declared runway length plus clearway and stop way

C

Declared runway length plus clearway

D

Declared runway length plus stop way

26/30

Question ID: 110992

The take-off distance required increases?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Due to slush on the runway

B

Due to head wind because of the drag augmentation

C

Due to downhill slope because of the smaller angle of attack

D

Due to lower gross mass at take-off

27/30

Question ID: 107905

ASDA is defined as?

This question has been flagged as being in an exam by multiple students, give it more attention

A

TORA plus clearway

B

The same as TODA

C

TORA plus stopway

D

TODA plus stopway

28/30

Question ID: 107656

The rate of climb?

This question has been flagged as being in an exam by multiple students, give it more attention

A

The angle of climb multiplied by the TAS

B

The angle of climb divided by the TAS

C

The still-air gradient multiplied by the TAS

D

The still-air gradient divided by the TAS

29/30

Question ID: 111037

The effect of increasing the flap setting, from zero to the recommended take-off setting, on the length of the Take-off Distance required (TODR) and the Field-Length-Limited Take-off mass (TOM) is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Decreased TOD required and decreased field length limited TOM

B

Increased TOD required and decreased field length limited TOM

C

Decreased TOD required and increased field length limited TOM

D

Increased TOD required and increased field length limited TOM

30/30

Question ID: 107610

Using CAP 698 Figure 2.4
Pressure altitude: 10000 ft
Mass: 2860 lb
Temperature: -2°C
Runway LDA: 2000 ft

Given the following information, determine the minimum or maximum wind component for the SEP aircraft to land?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Maximum 6 kt tailwind

B

Maximum 4 kt tailwind

C

Minimum 19 kt headwind

D

Minimum 38 kt headwind

Question ID: 107388

With a positive rate of climb, the difference between the climb angle and the climb gradient is that the gradient?

A

B

C

D

Question ID: 107326

An airline operator shall make sure that if the aircraft planned for the flight is a performance class B aeroplane, it will be able, throughout its flight route or its alternate route scheduled from this initial route, to reach a climb rate of at least?

A

B

C

D

Question ID: 107462

In accordance to EASA CS-25 which of the following listed speeds are used for determination of V2 MIN?

A

B

C

D

Question ID: 107318

What happens to Specific Range (SR) for a heavier aircraft?

A

B

C

D

Question ID: 109880

On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kts and the holding speed (minimum fuel burn per hour) is 95 kts The best rate of climb speed will be obtained for a speed?

A

B

C

D

Question ID: 109762

If the maximum Take-off Mass is limited by tire speed, what affect would a down sloping runway have?

A

B

C

D

Question ID: 111080

What is the climb requirement in the 3rd take off segment?

A

B

C

D

Question ID: 107572

With regard to the drift down performance of the twin jet aeroplane,\Why does the curve representing 35 000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370?

A

B

C

D

Question ID: 107578

SEP 1 Figure 2.4With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50 ft?Given O.A.T ISAPressure Altitude 1000 ftAeroplane Mass 3500 lbTailwind component 5 ktFlaps Landing position (down)Runway Tarred and Dry

A

B

C

D

Question ID: 107499

On take-off from an un-balanced field you have an available range of V1s. If a higher V1 is selected from the range then?

A

B

C

D

Question ID: 110414

According to EASA AIR OPS, for turbo-prop aeroplanes, the required runway length at a destination airport is?

A

B

C

D

Question ID: 107573

A

B

C

D

Question ID: 110177

With zero wind, the angle of attack for maximum range for an aeroplane with turbojet engines is?

A

B

C

D

Question ID: 110159

For a jet transport aeroplane, which of the following is the reason for the use of 'maximum range speed'?

A

On a twin engined piston aircraft with variable pitch propellers, for a given mass and altitude, the minimum drag speed is 125 kts and the holding speed (minimum fuel burn per hour) is 95 kts

The best rate of climb speed will be obtained for a speed?

With regard to the drift down performance of the twin jet aeroplane,\
Why does the curve representing 35 000 kg gross mass in the chart for drift down net profiles start at approximately 4 minutes at FL370?

SEP 1 Figure 2.4
With regard to the landing chart for the single engine aeroplane determine the landing distance from a height of 50 ft?
Given O.A.T ISA
Pressure Altitude 1000 ft
Aeroplane Mass 3500 lb
Tailwind component 5 kt
Flaps Landing position (down)
Runway Tarred and Dry

Which of the following will affect the level-off altitude during a drift-down?
1) Outside air temperature
2) Wind
3) Distance to alternate airport
4) Engine thrust

A jet aeroplane is climbing at constant Mach number below the tropopause.
Which of the following statements is correct?