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Section 5 - Performance
This section provides all necessary data for an accurate and comprehensive planning of flight activity from takeoff to landing.
Maximum demonstrated crosswind is 24 Kts.
Associated conditions:
- 1.Power ........................................................................ max continuous
- 2.Propellers .......................................................................... 2575 RPM
- 3.Surfaces .......................................... as reported in the relevant table
- 4.Take-off speed ........................................................ IAS, as tabulated
- 5.Static take-off ………………….………… full power, before brakes release
Weight (Kg / lbs) | VR (KIAS) | V50ft (KIAS) |
|---|---|---|
3600 / 7937 | 75 | 83 |
3400 / 7496 | 73 | 81 |
3200 / 7055 | 72 | 78 |
3000 / 6614 | 72 | 75 |
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:
- 1.Flaps ......................................................................................... LAND
- 2.Surface ............................................. as reported in the relevant table
- 3.Maximum effective braking
- 4.Power ......................................................................................... IDLE
- 5.Landing speed ........................................................ IAS, as tabulated
Weight (Kg / lbs) | VREF (KIAS) | VTD (KIAS) |
|---|---|---|
3600 / 7937 | 88 | 76 |
3400 / 7496 | 85 | 74 |
3200 / 7055 | 82 | 71 |
3000 / 6614 | 79 | 66 |
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.