Learn this Flashcards

1
Q

Imperial gallon > US gallon

A

x1.205

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2
Q

Litres > Imperial gallons

A

x4.546

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3
Q

US gallons > Litres

A

x3.785

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4
Q

Litres > Kilograms

A

x Specific gravity

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5
Q

Imperial gallons > lbs.

A

x10
x Specific gravity

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6
Q

US gallons > lbs.

A

x8.33
x Specific gravity

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7
Q

1 meter > feet

A

x 3.28

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8
Q

Nautical mile > statute mile

A

x 1.15

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9
Q

kilogram > lbs

A

2.205

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10
Q

Class B
Take off
Performance factor
Paved Wet

A

x 1.0

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11
Q

Class B
Take off
Performance factor
Grass Wet

A

1.3

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12
Q

Class B
Take off
Performance factor
Grass dry

A

1.2

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13
Q

Class B
Take off
Performance factor
Slope

A

1.05 per 1%
(5% increase per 1% slope, negative affects only)

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14
Q

Class B
Take off
Regulation factor
Unbalanced field
cannot exceed ASDA

A

TOD x 1.3
cannot exceed ASDA

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15
Q

Class B
Take off
Regulation factor
Unbalanced field
cannot exceed TODA

A

TOD x 1.15
cannot exceed TODA

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16
Q

Class B
Take off
Regulation factor
Unbalanced field
cannot exceed TORA

A

TOD x 1.0
cannot exceed TORA

17
Q

Class B
Take off
Regulation factor
Balanced field
cannot exceed TORA

A

TOD x 1.25
cannot exceed TORA

18
Q

Class A
Take off
Regulation factor

The take-off distance required is the highest of:

A

TOD (all engine TOD) x 1.15

TOD N-1

19
Q

Landing
Performance factor
Wet:

20
Q

Landing
Performance factor
Grass:

A

Grass: 1.15

21
Q

Landing
Performance factor
Slope:

A

Slope: 1.05 per 1% (negative affects only)

22
Q

Landing
Regulation factor
All props:

A

All props: 1.43

23
Q

Landing
Regulation factor
All jets:

A

All Jets: 1.67

24
Q

Graphical distance
>Performance factors>
Actual distance
>Regulation factors>
Distance required

A

Graphical distance

x Performance factors

Actual distance

x Regulation factors

Distance required

25
Q

Graphical distance
<Performance factors<
Actual distance
<Regulation factors<
Distance required

A

Distance required

÷ Regulation factors

Actual distance

÷ Performance factors

Graphical distance

26
Q

Gross to Net conversion: Climb
2 Engines: xx%
3 Engines: xx%
4 Engines: xx%

A

2 Engines: 0.8%
3 Engines: 0.9%
4 Engines: 1.0%

27
Q

Gross to Net conversion: Descent
2 Engines: xx%
3 Engines: xx%
4 Engines: xx%

A

2 Engines: 1.1%
3 Engines: 1.4%
4 Engines : 1.6%

28
Q

Single Engine
VR must be ______ than VS

A

VR must be faster than VS

29
Q

Landing: VREF
Class A =
Class B =

A

Landing: VREF
Class A = 1.23VSRO
Class B = 1.3VSO

30
Q

Vspeeds

VMCA:

  • VR
  • V2 MIN
A
  • VR x1.05
  • V2 MIN x1.1
31
Q

Vspeeds

VS (R):

  • VR
  • V2 MIN
A

VR x1.1

V2 MIN
* Class B x1.2
* Class A x1.13
* 4engine turboprop x1.08