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032 Performance Aircraft

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Where are the procedures associated with take-off and landing on contaminated runways found?

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Refer to figure.

NOTE: For this question do NOT interpolate, Choose the most conservative figures at ALL times.

The annex shows a regulated take-off mass (RTOM) table for runway 23L from take-off position VB. In each RTOM chart

box, the following information is provided for a given wind component / outside air temperature combination: MTOM /

limitation code / V,/VR/V2 (+100 kt). Given the following information, determine the RTOM for departure.

W/V: 140°/14 kt

OAT: +10°C

QNH: 1008 hPa

Runway: WET

Engine anti-ice: ON

Packs: OFF

Quick line-up

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What is the result of an increase in air density?

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The crew of a Medium-Range Jet Transport aeroplane are planning for a Commercial Air Transport flight departing from Mykonos (LGMK) Runway 16, which is 1902 m long with a take-off path over the sea. The aeroplane has three take-off flap settings, which give the following maximum take-off masses:

T/0 1: 1 stage of slats and 1 stage of flaps - 78.1 tonnes.

T/0 2: 2 stages of slats and 2 stages of flaps - 81.1 tonnes.

T/0 3: 2 stages of slats and 3 stages of flaps - 82.9 tonnes.

These maximum take-off masses are limited by the...

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Refer to figure.

You are taking-off with a single-engined aeroplane, and a field-lenght-limited take-off mass, from

runway 18, in Vmc, for a straight-out departure. Given the following information, what will be the

expected obstacle clearance over the trees on the extended centre line?

Climb gradient: 9%

TAS: 124 kt

Wind component: 10 kt headwind

1 NM = 6080 ft

Height Difference = ((GD × TAS)/GS) × Gradient/100

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Refer to figure or CAP 698 file 4.20.

Given the following information for a medium range jet transport aeroplane, determine the regulated take-off mass for

the new runway:

OAT: +15°C

Airfield pressure altitude: 0 ft

Nil Wind

Flap setting: 5°

TORA: 7000 ft

The normal Take-off mass limits relevant for this flight are:

Maximum Structural Limit: 62 800 kg

Field Length Limit: 60 500 kg

Climb Limit: 64 000 kg

Tyre Speed Limit: greater than 84 000 kg

Due to wind direction change, ATC changes the runway in use, which will have the same conditions described previously,

except for the following:

Wind: 10 kt headwind

Obstacle height: 360 ft

Obstacle distance from the break release point: 21 000 ft

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Refer to figure or CAP698 file 3.1.

TORA: 2250 ft

Runway surface: grass

Runway condition: dry

No clearway and no stopway available

Airfield pressure altitude: 2000 ft

Airfield temperature: +11°C

Headwind component: 5 kt

Given the following information, what is the Field Length Limited Take-Off Mass?

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Which of the following options correctly describes the effects on aircraft performance of landing on

wet or contaminated runways? 

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The following runways are available: 07/25 and 01/19. The wind is coming from 350°25 degrees.

Which runway should the pilot choose? 

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Refer to figure. (For this question use CAP 698 Figure 4.7).

Planned take-off mass is 64000 kg, pressure altitude 4000 ft, OAT +10°C, V, 151, 155, 161. Runway slope is -1% and

tailwind 5 kt. What is the maximum permitted take-off mass?

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