Definitions Flashcards

1
Q

Critical speed

A

The speed, beneath which, after engine failure, control of the aircraft is lost- no rudder controllability

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2
Q

Vyse

A

Single engine best rate of climb speed- blue line

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3
Q

Basic weight

A

The weight of the aircraft structure including engines, unusable fuel and oil

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4
Q

Service ceiling

A

The maximum altitude where the aircraft can maintain a climb rate of 50ft per minute

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5
Q

Vmca

A

The minimum control speed relating to sudden engine failure - at takeoff configuration. A certification, theoretical speed.

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6
Q

Absolute ceiling

A

The maximum altitude whereby rate of climb falls to zero at full power conditions

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7
Q

TORA

A

The length of the runway available for the ground run of an aircraft at takeoff

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8
Q

Counter rotating propellers

A

Propellers which rotate in opposite directions to each other

Be76

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9
Q

Contra-rotating propellers

A

Problems which rotate in same direction as each other

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10
Q

ASDA

A

Accelerate Stop Distance Available

The length of the take off run available plus the stopway (if available) if takeoff is aborted and aircraft brought to a stop

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11
Q

Take off Safety Speed Vtoss

A

Nominal speed to give a safety margin between minimum control speed and stall speed.

Greater of 1.1 x Vmca and 1.2 x stalling speed

The speed above which the aircraft is safely controllable

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12
Q

Vso

A

The stall speed in landing configuration

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13
Q

Vs1

A

Stall speed in clean configuration

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14
Q

Vfe

A

Maximum flap extension speed

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15
Q

Vlo

A

Maximum landing gear operating speed

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16
Q

Vle

A

Maximum gear extension speed

17
Q

Vsse

A

Single engine safety speed above stall speed and minimum control speed - provide a greater margin of safety for deliberate asymmetric operations and training

18
Q

Red line speed

A

Signifies Vmca and Vne

19
Q

Critical engine

A

The engine which creates the largest yawing moment when failed in any given set of conditions

20
Q

Asymmetric blade effect

A

At reduced power and resulting high angle of attack, the downgoing blade produces more thrust than the upgoing one creating an offset thrust line.

21
Q

Vxse

A

The single engine speed for best angle of climb

22
Q

Define ‘drift down’

A

Is the maximum thrust/ minimum rate of descent necessitated by engine failure in a multi engine aeroplane in climb or cruise whereby the aircraft cannot maintain current altitude and maintain terrain clearance

23
Q

What is zero thrust setting?

A

To simulate feathered prop- typically 13” MAP with aircraft to stay in selected trims

24
Q

ICAO wake turbulence minima - light twin engine aircraft

A

Light twin following a heavy aircraft- 6NM / 3 mins

25
Q

Define load factor

A

The ratio of lift to weight