1/30
Question ID: 111874

What are the effects of using a clearway on both the Allowed Take-Off Mass and the associated V1.

The Allowed Take-Off Mass?

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A

Decreases and V1 increases

B

And V1 decrease

C

And V1 increase

D

Increases and V1 decreases
2/30
Question ID: 107494

The speed VSR is defined as?

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A

As reference stall speed and may not be less than 1-g stall speed

B

Take-off safety speed for a contaminated runway

C

Design stress speed

D

Speed for best specific range
3/30
Question ID: 111890

Which statement is correct?

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A

VR must not be less than 1.05 VMCA and not less than V1

B

VR must not be less than 1.1 VMCA and not less than V1

C

VR must not be less than VMCA and not less than 1.05 V1

D

VR must not be less than 1.05 VMCA and not less than 1.1 V1
4/30
Question ID: 107431

What determines the maximum flight altitude in the Buffet Onset Boundary graph?

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A

Service ceiling

B

Theoretical ceiling

C

Economy

D

Aerodynamics
5/30
Question ID: 107625

Refer to the image:

A twin engine aeroplane with data provided in the annex is flying for Long Range Cruise LRC at FL340 and in ISA +20° C conditions.

Find the N1, Mach number and fuel consumption if the aeroplane mass is 71000 kg and the CG is at 33% MAC.

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A

88.9, M 0.775 and 166.7 NM/1000 kg

B

88.35, M 0.768 and 165.6 NM/1000 kg

C

88.35, M 0.768 and 2814 kg/h

D

88.9, M 0.775 and 2810 kg/h
6/30
Question ID: 111112

Given:

Still air gradient of climb: 5%

TAS: 250 kts

G/S: 200 kts


What is climb rate?

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A

1250 fpm

B

2000 fpm

C

500 fpm

D

1000 fpm
7/30
Question ID: 107376

On a segment of the take-off flight path an obstacle requires a minimum gradient of climb of 2.6% in order to provide an adequate margin of safe clearance at a mass of 110000 kg the gradient of climb is 2.8% 

For the same power and assuming that the sine of the angle of climb varies inversely with mass, at what maximum mass will the aeroplane be able to achieve the minimum gradient?

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A

106425 kg

B

102150 kg

C

124808 kg

D

118455 kg
8/30
Question ID: 111099

What is the minimum width of a clearway?

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A

250 feet

B

750 feet

C

1000 feet

D

500 feet
9/30
Question ID: 107428

Having all other conditions the same, taking off from an upward-sloping runway compared to a zero slope runway will result in?

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A

An increased take-off distance, and a decreased stopping distance in case of an aborted take-off

B

An increased take-off distance, and an increased stopping distance in case of an aborted take-off

C

A decreased take-off distance, and an increased stopping distance in case of an aborted take-off

D

A decreased take-off distance, and a decreased stopping distance in case of an aborted take-off
10/30
Question ID: 107593

Using Annex or CAP 698 Fig 4.7

Determine VMBE?

Given:

TOM 60000 kg

PA 6000 ft

OAT-10°C

Slope 2% down,

5 kts TW,

PMC OFF.

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A

154 kts

B

139 kts

C

170 kts

D

149 kts
11/30
Question ID: 110983

Which take-off condition is most likely resulting in the poorest climb performance?

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A

Sea level field elevation, ISA -20°, take-off flaps 10°

B

Sea level field elevation, ISA +5°, take-off flaps 10°

C

5000 ft field elevation, ISA +20°, take-off flaps 30°

D

5000 ft field elevation, ISA-5°, take-off flaps 10°
12/30
Question ID: 107337

A Class B light twin aeroplane is to take-off on a Commercial Air Transport flight from an airfield with data as given below. What is the de-factored take-off distance that should be used to determine the maximum take-off mass from the gross-take-off performance graph produced for a level, paved and dry runway?

TORA 1270 ft

Clearway 385 ft

Stop way 215 ft

Upslope 1.3% (5% extra distance required for every 1 % of upslope)

Runway surface paved and wet

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A

1073 ft

B

1175 ft

C

954 ft

D

933 ft
13/30
Question ID: 107645

A flight benefits from a strong tailwind which was not forecasted.

On arrival at the destination a straight-in approach and immediate landing clearance is given.

The Landing Mass will be higher than planned and?

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A

The landing distance required will be longer

B

The approach path will be steeper and threshold speed higher

C

The landing distance will be unaffected

D

The approach path will be steeper
14/30
Question ID: 111979

On a transatlantic flight, the captain asks the First Officer why a final step climb from FL340 to FL380 ten minutes before top of descent might not be an efficient use of the fuel. Select a possible explanation?

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A

Even in still air, cruising at the higher optimum level would decrease the specific range

B

There might be stronger tailwinds at FL380

C

A climb to FL380 might consume more fuel than would be saved by being at the higher altitude for a short period

D

The headwind present at FL 340 might be more favorable than the still air conditions at FL380
15/30
Question ID: 107944

An increase in ambient temperature causes the absolute ceiling to?

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A

Increase

B

Decrease

C

Increase subject to its relation to ISA

D

Remain unchanged
16/30
Question ID: 111880

A lower airspeed at constant mass and altitude requires?

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A

A higher coefficient of lift

B

More thrust and a lower coefficient of lift

C

Less thrust and a lower coefficient of lift

D

More thrust and a lower coefficient of drag
17/30
Question ID: 107601

Given Climb power

Full throttle / 2500 RPM,

Altitude 6,500 ft,

Temperature ISA +15°C

QNH 1,030 hPa

Weight 1,250 kg


Find the rate of climb?

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A

1,560 ft/min

B

1,620 ft/min

C

1,420 ft/min

D

1,450 ft/min
18/30
Question ID: 107363

For an instrument departure (SID). What is the procedure design gradient (PDG)?

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A

5%

B

2.5%

C

3.3%

D

3.5%
19/30
Question ID: 111116

When compared to a clean configuration, how does flap setting usually affect the Runway Length Limited Take-Off Mass and the Climb Limited Take-Off Mass? The Runway Length Limited Take-Off Mass?

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A

Increases, and the Climb Limited Take Off Mass increases

B

Decreases, and the Climb Limited Take Off Mass decreases

C

Decreases, and the Climb Limited Take Off Mass increases

D

Increases, and the Climb Limited Take Off Mass decreases
20/30
Question ID: 108127

Considering TAS for maximum range and maximum endurance, other factors remaining constant?

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A

TAS for maximum range will increase with increased altitude while TAS for maximum endurance will decrease with increased altitude

B

Both will stay constant regardless of altitude

C

Both will increase with increasing altitude

D

Both will decrease with increasing altitude
21/30
Question ID: 110120

What percentages of the headwind and tailwind components are taken into account when calculating the take-off field length required?

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A

100% headwind and 100% tailwind

B

50% headwind and 100% tailwind

C

50% headwind and 150% tailwind

D

150% headwind and 50% tailwind
22/30
Question ID: 107408

What is the consequence of using a dry V1 on a wet runway for the Accelerate Stop Distance ASD?

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A

Increases, and the runway remains balanced

B

Increases, and the runway becomes unbalanced

C

Decreases due to the greater friction drag on a wet runway

D

Remains the same if thrust reversers are used
23/30
Question ID: 107392

ON a contaminated runway, what happens to the CLTOM & FLTOM?

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A

Increase & Decrease

B

Unchanged & Decrease

C

Unchanged & Increase

D

Decrease & Decrease
24/30
Question ID: 107453

What is likely to happen during take-off if a pilot uses a 'dry V1' in wet runway conditions?

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A

In case of an aborted take-off procedure the airplane would not exceed the ASDA because V1 wet and V1 dry are always the same

B

In case of an aborted take-off procedure the airplane would not exceed the ASDA because V1 dry considers a safety margin for wet conditions

C

In case of an aborted take-off procedure the airplane would exceed the ASDA because the anti-skid system would be adjusted to dry conditions

D

In case of an aborted take-off procedure the airplane would exceed the ASDA because braking action would be lower
25/30
Question ID: 107519

Refer to the attached figure and choose a correct statement below?

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A

Point F: maximum rate of descent

B

The speed at point C would result in a greater angle of descent than at point B.

C

Point D: the aircraft would decelerate if it would fly straight and level

D

Point C: maximum angle of climb
26/30
Question ID: 107419

Required net climb gradients in the 1st segment for 3-engine aircraft with one engine out are?

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A

2.7%

B

0.1%

C

5.5%

D

0.3%
27/30
Question ID: 110116

For take-off performance calculations, what is taken into account?

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A

OAT, pressure altitude, wind, weight

B

Standard temperature, altitude, wind, weight

C

Standard temperature, pressure altitude, wind, weight

D

Standard altitude, standard temperature, wind, weight
28/30
Question ID: 111885

What is the effect of excess thrust on an aircraft climbing at a constant angle? It:

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A

Accelerates, and the climb gradient increases

B

Converts the excess thrust to increase the flight path angle

C

Accelerates, and the rate of climb increases

D

Accelerates, and the pitch angle increases
29/30
Question ID: 111914

Which of the following describes VLOF?

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A

Maximum landing gear operating and flaps extended speed

B

Landing gear operation failure speed

C

Take-off safety speed

D

Lift-off speed
30/30
Question ID: 107491

How is V2 affected if T/O flaps 20° is chosen instead of T/O flaps 10°?

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A

V2 has the same value in both cases

B

V2 decreases if not restricted by VMCA

C

V2 has no connection with T/O flap setting, as it is a function of runway length only

D

V2 increases in proportion to the angle at which the flaps are set
Finish Test
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