1/30
Question ID: 109767

When Take-off Mass is limited by VMBE, an increase in the uphill slope will?

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A

Require a decrease in the mass

B

Decrease the TODR

C

Allow An increase in the mass

D

Have no effect
2/30
Question ID: 107522

Which of the following images correctly shows the movement of the power required curve with increasing altitude?

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A

Figure A

B

Figure D

C

Figure C

D

Figure B
3/30
Question ID: 111121

The optimum cruise altitude is?

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A

The pressure altitude at which the best specific range can be achieved

B

The pressure altitude up to which a cabin altitude of 8000 ft can be maintained

C

The pressure altitude at which the fuel flow is a maximum

D

The pressure altitude at which the speed for high speed buffet as TAS is a maximum
4/30
Question ID: 111878

For a given V1, an inoperative aeroplane antiskid on one wheel will result in an increased?

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A

Ground roll distance

B

Take off distance

C

Accelerate stop distance

D

Take-off run distance
5/30
Question ID: 111866

Runway 02 has a threshold elevation of 230 ft and runway 20 has a threshold elevation of 260ft. 

If the TORA is 1200m calculate the slope of runway 02?

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A

1.56% down

B

1.56% up

C

0.76% up

D

0.76% down
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

1000 fpm

C

2000 fpm

D

500 fpm
7/30
Question ID: 110422

What is the advantage of using the increased V2 (improved climb) procedure on take-off?

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A

The obstacle-limited take-off mass is increased

B

The time to reach the optimum altitude is reduced

C

The associated higher V2 allows for an increased take-off mass

D

The safety margin of the field-length limited mass is increased
8/30
Question ID: 111904

Which condition is least favorable handling-wise during take-off for a twin engine aircraft with the engines wing mounted, both being right hand props?

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A

A left engine failure, with a left quartering wind

B

A right engine failure, with a right quartering wind

C

A right engine failure, with a left quartering wind

D

A left engine failure, with a right quartering wind
9/30
Question ID: 110402

The maximum mass for landing could be limited by?

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A

The climb requirements with one engine inoperative in the landing configuration

B

The climb requirements with one engine inoperative in the approach configuration

C

The climb requirements with all engines in the approach configuration

D

The climb requirements with all engines in the landing configuration but with gear up
10/30
Question ID: 107557

Given:

OAT 10° C

Pressure Altitude 2000 ft

Gross Mass 3750 lbs

Mixture full rich


Other conditions as associated in the header of the graph What is the two engine rate of climb for the conditions given?

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A

1770 ft/min

B

1970 ft/min

C

1570 ft/min

D

430 ft/min
11/30
Question ID: 107446

Compared with balanced-field calculations for an aerodrome with no stopway or clearway, the use of a clearway in the take-off calculations will?

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A

Not affect the value of V1

B

Increase the field-length-limited take-off mass

C

Increase the value of V1

D

Not affect the value of the field-length-limited take-off mass
12/30
Question ID: 110393

The lift coefficient decreases during a glide with constant Mach number, mainly because the?

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A

Aircraft mass decreases

B

Glide angle increases

C

TAS decreases

D

IAS increases
13/30
Question ID: 107538

With regard to the landing chart for the single engine aeroplane determine the approximate landing distance from a height of 50 ft?

Given:

OAT 27°C

Pressure Altitude 3000 ft

Aeroplane Mass 2900 lbs

Tailwind component 5 kts

Flaps Landing position (down)

Runway Tarred and Dry

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A

1120 feet

B

1850 feet

C

1370 feet

D

1700 feet
14/30
Question ID: 109854

During a take-off from a runway contaminated by slush the drag caused by the slush will?

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A

Increase then remain constant

B

Increase with increasing speed

C

Increase up to VP then increase at a greater rate

D

Increase then decrease
15/30
Question ID: 110460

Which of the following factors leads to the maximum flight time of a glide?

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A

High mass

B

Tailwind

C

Low mass

D

Headwind
16/30
Question ID: 110965

The conditions most likely to produce the highest engine power are?

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A

Warm and dry air at high pressure

B

Warm air at low pressure with high relative humidity

C

Cold air at high pressure with high relative humidity

D

Cold and dry air at high pressure
17/30
Question ID: 109852

For take-off obstacle clearance calculations, obstacles in the first segment may be avoided?

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A

Only by using standard turns

B

By standard turns - but only after passing 1500 ft

C

By banking not more than 15° between 50 ft and 400 ft above the runway elevation

D

By banking as much as needed if aeroplane is more than 50 ft above runway elevation
18/30
Question ID: 107331

Consider a performance class B aeroplane which is used for commercial transports and a runway where a clearway or a stop way is available. The take-off mass shall not exceed the maximum take-off mass specified in the AFM for the pressure altitude and the ambient temperature at the aerodrome of departure. The un-factored take-off distance, specified in the AFM, shall not exceed the take-off distance available (TODA), when multiplied by a factor of?

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A

1.3

B

1.15

C

1.25

D

1.5
19/30
Question ID: 107321

For a multi engined aircraft not certified under EASA CS 25 and in Performance Class B, service ceiling is defined as?

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A

The altitude which at maximum power the rate of climb of an aircraft has fallen to 500 ft per minute

B

The altitude which at maximum power the rate of climb of an aircraft has fallen to 0 ft per minute

C

The altitude which at maximum power the rate of climb of an aircraft has fallen to 100 ft per minute

D

The altitude which at maximum power the rate of climb of an aircraft has fallen to 100 ft per minute for a piston engine and 500 ft per minute for a jet aircraft
20/30
Question ID: 111030

A decrease in atmospheric pressure has, among other things, the following consequences on take-off performance?

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A

An increased take-off distance and degraded initial climb performance

B

A reduced take-off distance and degraded initial climb performance

C

A reduced take-off distance and improved initial climb performance

D

An increased take-off distance and improved initial climb performance
21/30
Question ID: 107602

Given the following data calculate the obstacle limited TOM Using MRJT1 4.21?

Obstacle Height: 310 ft,

Distance: 22000 ft,

OAT: 35°C,

PA: 2140 ft,

HW: 20 kts, 

PMC OFF, 

Flaps 15°.

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A

49350 kgs

B

46980 kgs

C

51500 kgs

D

46680 kgs
22/30
Question ID: 107433

The Accelerate Stop Distance on a dry runway considers both the all engine case and the engine failure case. The latter is calculated by adding the sum of the distance necessary to accelerate to VEF, the distance to accelerate to the highest speed reached during the rejected take-off?

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A

The distance to come to a full stop, and a distance equivalent to 2 seconds at V1 all multiplied by 1.15

B

150% of the distance to come to a full stop, and a distance equivalent to 2 seconds at VEF

C

The distance to come to a full stop, and a distance equivalent to 2 seconds at V1

D

The distance to come to a full stop multiplied by 1.15, and a distance equivalent to 2 seconds at VEF
23/30
Question ID: 107653

Deployment of flaps ____________ CL / CD?

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A

Only slightly increases

B

Reduces

C

Increases

D

Does not affect
24/30
Question ID: 109876

The speed for best rate of climb is called?

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A

VCL

B

V2

C

VY

D

VX
25/30
Question ID: 110343

If the level-off altitude is below the obstacle clearance altitude during a drift down procedure?

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A

Fuel jettisoning should be started when the obstacle clearance altitude is reached

B

Fuel jettisoning should be started at the beginning of drift down

C

The recommended drift down speed should be disregarded and it should be flown at the stall speed plus 10 kts

D

The drift down should be flown with flaps in the approach configuration
26/30
Question ID: 108081

In straight and level flight the lift is opposed by the?

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A

Drag

B

Drag and weight

C

Thrust

D

Weight
27/30
Question ID: 110979

Which of the following statements, concerning tires, is the major consideration when establishing the tyre speed limit?

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A

Tyre pressure and brake temperature

B

Rotation rate of the tyre and temperature

C

Tyre pressure and temperature

D

Rotation rate of the tyre and VMBE
28/30
Question ID: 107359

The Landing Distance for a Performance Class B aeroplane is the horizontal distance necessary to land and come to a complete stop from what height above the landing surface?

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A

35 ft

B

50 ft

C

11 ft

D

15 ft
29/30
Question ID: 107548

Using Figure 4.5

Given:

Climb Limited Take-Off mass (CLTOM) 48020 kg

Airport pressure altitude 6000 ft

Flaps 15"

Packs OFF

Anti-Ice OFF

PMC ON


What is the maximum airport Outside Air Temperature (OAT) at which the take-off can be performed under those conditions?

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A

39°C

B

34°C

C

44°C

D

30°C
30/30
Question ID: 111014

The annex shows take off rejected take off distance for an aeroplane in given conditions. 

The balanced field is shown at distance?

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A

D

B

C

C

A

D

B
Finish Test
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