Learn this Flashcards

(31 cards)

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:

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
Graphical distance
Distance required ÷ Regulation factors Actual distance ÷ Performance factors Graphical distance
26
Gross to Net conversion: Climb 2 Engines: xx% 3 Engines: xx% 4 Engines: xx%
2 Engines: 0.8% 3 Engines: 0.9% 4 Engines: 1.0%
27
Gross to Net conversion: Descent 2 Engines: xx% 3 Engines: xx% 4 Engines: xx%
2 Engines: 1.1% 3 Engines: 1.4% 4 Engines : 1.6%
28
Single Engine VR must be ______ than VS
VR must be faster than VS
29
Landing: VREF Class A = Class B =
Landing: VREF Class A = 1.23VSRO Class B = 1.3VSO
30
Vspeeds VMCA: * VR * V2 MIN
* VR x1.05 * V2 MIN x1.1
31
Vspeeds VS (R): * VR * V2 MIN
VR x1.1 V2 MIN * Class B x1.2 * Class A x1.13 * 4engine turboprop x1.08