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Imperial gallon > US gallon
x1.205
Litres > Imperial gallons
x4.546
US gallons > Litres
x3.785
Litres > Kilograms
x Specific gravity
Imperial gallons > lbs.
x10
x Specific gravity
US gallons > lbs.
x8.33
x Specific gravity
1 meter > feet
x 3.28
Nautical mile > statute mile
x 1.15
kilogram > lbs
2.205
Class B
Take off
Performance factor
Paved Wet
x 1.0
Class B
Take off
Performance factor
Grass Wet
1.3
Class B
Take off
Performance factor
Grass dry
1.2
Class B
Take off
Performance factor
Slope
1.05 per 1%
(5% increase per 1% slope, negative affects only)
Class B
Take off
Regulation factor
Unbalanced field
cannot exceed ASDA
TOD x 1.3
cannot exceed ASDA
Class B
Take off
Regulation factor
Unbalanced field
cannot exceed TODA
TOD x 1.15
cannot exceed TODA
Class B
Take off
Regulation factor
Unbalanced field
cannot exceed TORA
TOD x 1.0
cannot exceed TORA
Class B
Take off
Regulation factor
Balanced field
cannot exceed TORA
TOD x 1.25
cannot exceed TORA
Class A
Take off
Regulation factor
The take-off distance required is the highest of:
TOD (all engine TOD) x 1.15
TOD N-1
Landing
Performance factor
Wet:
Wet: 1.15
Landing
Performance factor
Grass:
Grass: 1.15
Landing
Performance factor
Slope:
Slope: 1.05 per 1% (negative affects only)
Landing
Regulation factor
All props:
All props: 1.43
Landing
Regulation factor
All jets:
All Jets: 1.67
Graphical distance
>Performance factors>
Actual distance
>Regulation factors>
Distance required
Graphical distance
x Performance factors
Actual distance
x Regulation factors
Distance required
Graphical distance
<Performance factors<
Actual distance
<Regulation factors<
Distance required
Distance required
÷ Regulation factors
Actual distance
÷ Performance factors
Graphical distance
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%
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%
Single Engine
VR must be ______ than VS
VR must be faster than VS
Landing: VREF
Class A =
Class B =
Landing: VREF
Class A = 1.23VSRO
Class B = 1.3VSO
Vspeeds
VMCA:
- VR
- V2 MIN
- VR x1.05
- V2 MIN x1.1
Vspeeds
VS (R):
- VR
- V2 MIN
VR x1.1
V2 MIN
* Class B x1.2
* Class A x1.13
* 4engine turboprop x1.08