2.1.Introduction
The chapter 2 contents are operational limits necessary for a save operation of the aircraft
2.2. Air Speeds |
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Never exceed speed |
| vNE | ….. | 286 km/h | ….. | 154 kt | ||
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| Do not exceed this speed in any case |
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Design manoeuvre speed |
| vA | …… | 187 km/h | ….. | 101 kt | ||
Do not use full deflection of the rudders and sudden control operations. Overload of the
aircraft may occur
Maximum design cruising speed |
| vC | …… | 238 km/h | ….. | 128 kt |
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| Operation over this speed must be conducted with caution in smooth air only |
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Maximum speed at flaps deflection | 10° | vFI | …… | 140 km/h | ….. | 75 kt |
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Maximum speed at flaps deflection | 20° | vFII | ....... | 130 km/h | ...... | 70 kt |
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Maximum speed at full deflection | 35° | vFE | …… | 120 km/h | ….. | 65 kt |
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Maximum recommended speed at def. 35° | vFIII | …… | 100 km/h | ….. | 55 kt |
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| Do not exceed this speed by flaps deflected |
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Stalling speed flaps retracted |
| vS1 | …… | 76,4 km/h | ….. | 41 kt |
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| The loss of uplift and fall of aircraft with flaps retracted happens by this speed |
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Stalling speed in landing configuration |
| vSO | …... | 64,2 km/h | ….. | 35 kt |
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The loss of uplift and fall of aircraft with flaps position III deflected happens by this
speed
2.3. Weights |
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Empty weight …………………………………. | kg |
Maximum | 300 315 kg |
Useful load …………………………………. | kg |
Never exceed the maximum take-off weight of the aeroplane
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