Performance Flashcards

(29 cards)

1
Q

Define take-off distance required (TODR)

A
  • The distance the aircraft requires to take-off from a standing start at maximum power, reaching a screen height above the runway at take-off safety speed.
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2
Q

Define take-off safety speed (TOSS)

A
  • The speed which gives a safe buffer above the stall speed on take-off.
  • Must not be less than 1.2 x Vs in the take of configuration.
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3
Q

Define screen height (or barrier)

A
  • Ensures the aircraft can not only lift off the ground but also attain a minimum safe altitude at the runways end to clear obstacles
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4
Q

Displaced threshold

A
  • Can’t land before it
  • Can take off before it
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5
Q

Define stopway

A
  • Rectangular area on ground at end of take-off run available.
  • Where an aircraft can be stopped in the case of a rejected take-off.
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6
Q

Define clearway

A
  • The area at the departure end of the runway selected or prepared as a suitable area over which an aeroplane may make a portion of its initial climb to a specified height.
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7
Q

Landing distance available

A
  • Length of runway that is declare by the aerodrome operator as available and suitable for the ground runway of an aeroplane.
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8
Q

Take-off run available (TORA)

A

The length of the runway declared by the aerodrome operator as available and suitable from the ground runway of an aeroplane taking off.

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9
Q

Accelerate-stop distance available (ASDA)

A
  • The effective length available for the use by an aircraft executing a rejected take off.
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10
Q

Take-off distance available (TODA)

A
  • The length of the take-off run available plus the length of any clearway.
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11
Q

Landing distance required (LDR)

A
  • Horizontal distance that an aircraft required to land and decelerate to a full stop using maximum breaking.
  • Calculated 50ft above the landing threshold at a speed not less than 1.3 x Vs.
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12
Q

Dry runway

A
  • Not wet or contaminated
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13
Q

Wet runway

A
  • Surface is covered with sufficient moisture
  • Less than contaminated runway or when there is sufficient moisture on the runway surface to cause it to appear reflective but without significant areas of standing water.
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14
Q

Contaminated runway

A
  • A runway of which more than 25% of the runway surface area within the required length and width being used is covered by more than 3mm in depth of surface water, slush, or loose snow
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15
Q

Gross flight path

A
  • Aircraft’s assumed flight path when flown in a given configuration in accordance with specific procedures.
  • The best performance that the aircraft can achieve under ideal conditions
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16
Q

Net flight path

A
  • Gross flight path reduced by specified margins.
  • MArgins determined by CAA
  • Provides a safety margin in a real emergency situation
17
Q

Drift down

A
  • Procedure used on multi-engine aircraft when one of the engines fails.
  • Involves a slow descent to a lower altitude at which the aircraft can comply with the one-engine inoperative enroute climb performance
18
Q

Gradient of climb

A
  • The ratio of height gained over the horizontal distance travelled, expressed as a percentage.
  • Measures the steepness of an aircraft’s climb path
19
Q

How to calculate gradient of climb

A
  1. Add tailwind or subtract headwind from IAS
  2. Divide rate of climb by the ANS
20
Q

Factors affecting take-off performance

A
  • Take -off run available
  • Weight of plane at commencement of take-off run
  • Pressure altitude
  • Ambient temperature
  • Type of surface
  • Surface condition
  • Runway slope
  • Not more than 50% of the reported headwind component or not less than 150% of the reported tail wing component is used
21
Q

Air density on take-off performance

A

More dense the air the better performance

22
Q

Weight on take-off performance

A

Higher weight reduces performance

23
Q

Wind on take-off performance

A

Headwind good, tailwind bad

24
Q

Runway slope of take-off distance

A
  • Down sloped runway will decrease the TODR
25
Runway surface/condition on take-off performance
Any other runway aside from paved with increase TODR.
26
Factors affecting landing performance
- Aerodrome elevation - Ambient temperature - Type of runway surface and condition - Runway slope - Not more than 50% of the reported head wing or not less than 150% of the reported tailwind component
27
Pressure altitude
Height above a given datum
28
What s a ‘single engine en-route’ chart?
- Used to work out the maximum pressure altitude at which you can operate with one engine inoperative.
29
Conditions on single engine en-route charts
- Engine and propeller reference - 1% climb gradient - Best rate of climb speed 88kts IAS