Section 5 - Performance
This section provides all necessary data for an accurate and comprehensive planning of flight activity from takeoff to landing.
Last updated
This section provides all necessary data for an accurate and comprehensive planning of flight activity from takeoff to landing.
Last updated
Maximum demonstrated crosswind is 24 Kts.
The actual crosswind component can be calculated using a variety of tools such as AeroToolbox.
Associated conditions:
Power ........................................................................ max continuous
Propellers .......................................................................... 2575 RPM
Surfaces .......................................... as reported in the relevant table
Take-off speed ........................................................ IAS, as tabulated
Static take-off âĻâĻâĻâĻâĻâĻâĻ.âĻâĻâĻâĻ full power, before brakes release
Headwind: subtract 6% and 4% respectively from the ground and total distances for each 5 knots headwind.
Tailwind: add 20% and 15% respectively to the ground and total distances for each 5 knots tailwind.
Sloped runway: increase table distances by 8% of the ground distance at Sea Level, 12% of the ground distance at 5000 ft, 16% of the ground distance at 10000 ft for each 1% of upslope. Decrease table distances by 7% of the ground distance at Sea Level, 9% of the ground distance at 5000 ft, and 12% of the ground distance at 10000 ft for each 1% of downslope.
Refer to figures below. Associated conditions:
Flaps ......................................................................................... LAND
Surface ............................................. as reported in the relevant table
Maximum effective braking
Power ......................................................................................... IDLE
Landing speed ........................................................ IAS, as tabulated
Landing distances on grass surface have been determined for the following airfield surfaces:
firm bare soil
grass up to 5 cm (2 inches) long
wheel impression up to 1 cm (0.4 in) Different runway conditions may result in improved or degraded performance.
Headwind: subtract 12% and 6% respectively from the ground and total distances for each 5 knots headwind.
Tailwind: add 13% and 7% respectively to the ground and total distances for each 5 knots tailwind.
Sloped runway: increase table distances by 6% of the ground distance at Sea Level, 7% of the ground distance at 5000 ft, 8% of the ground distance at 10000 ft for each 1% of downslope. Decrease table distances by 5% of the ground distance at Sea Level, 6% of the ground distance at 5000 ft, and 7% of the ground distance at 10000 ft for each 1% of upslope.
Consider about 10 m (33 ft) of ground distance reduction for each 100 kg (220 lb) of weight reduction.
Consider about 10 m (33 ft) of ground distance reduction for each 100 kg (220 lb) of weight reduction.
| Weight (Kg / lbs) | VR (KIAS) | V50ft (KIAS) |
|---|---|---|
| Weight (Kg / lbs) | VREF (KIAS) | VTD (KIAS) |
|---|---|---|
3600 / 7937
75
83
3400 / 7496
73
81
3200 / 7055
72
78
3000 / 6614
72
75
3600 / 7937
88
76
3400 / 7496
85
74
3200 / 7055
82
71
3000 / 6614
79
66