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2.10 Manoeuvres
This aircraft has been certified in normal category.
Permissible manoeuvres and manoeuvre entry speeds are given below.
Turn, bank of 60° ............................................... 124 km/h
Side slip ............................................................ 124 km/h
WARNING
Aerobatics, intentional stalls and spins are prohibited.
2.11 Maximum wind component limitations
Maximum permitted wind speed components for take-off and landing:
aligned with runway axis ................................... 10 m/s
perpendicular to runway ..................................... 4 m/s
tail wind .............................................................. 3 m/s
2.12 Crew
Number of seats ................................................ 2
Minimum crew weight ......................................... 55 kg
Max. crew weight ............................................... 175 kg
Maximum permissible cockpit load ..................... 180 kg
2.13 Kinds of Operation
Only VFR day flights (by permanent visual ground contact.)
WARNING
IFR flights and flying in clouds are prohibited.
2.14 Fuel system
Fuel tank capacity wing tanks ............................ 2 x 30 l
Link tank ............................................................. 6 l
Max. fuel quantity ............................................... 66 l
Usable fuel quantity ............................................ 60 l
Unusable fuel quantity on ground ....................... 6 l
Unusable fuel quantity in the air with engine on...2 l
Fuel specification unleaded Minimum ............. RON 95
in accordance with DIN 51607
CAUTION
! The fuel tanks (wings+center tank) contains 6 litres of fuel after complete
defueling on the ground. This amount is the unusable fuel quantity on ground. In the air with
operating engine the unusable fuel is 2 litres. The engine can completely empty the center
link tank.
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