Flight and Operations Manual of ATEC 321 Faeta ultralight aircraft with Rotax 912 iS Sport
ATEC v.o.s. Libice nad Cidlinou, Czech Republic Page 20 of 56
3.7. Safety Landing
Carried out in case of orientation loss, fuel exhaustion or any other reason when the aircraft is fully
controllable.
1. Determine the wind direction
2. Choose any suitable landing surface
3. Make a low pass headwind along the right-hand side of the landing surface and inspect the
terrain thoroughly
4. Make a pattern flight
5. Calculate the landing plan
6. Land in the first third of the landing area by using flaps in landing position
3.8. Aborted Landing
Carried out in case of wrong calculation of landing manoeuvre or bounce during landing and when the
pilot considers aborted landing manoeuvre as more safe and decides to proceed the flight.
1. Set the engine run up to maximum power
2. Fluently set up flaps to take-off position – I
3. Reach the horizontal speed of 110 km/h (59 kt)
4. Pull the control stick slowly to make the aircraft climbing by speed 110 – 120 km/h (59 – 65 kt)
5. Retract flaps
Maintain the aircraft in take-off axis by using rudder control throughout the flight.
3.9. Vibrations
In case of unusual vibrations occurance, it is necessary to:
1. Set the engine run up to appropriate RPM on which the vibrations are the lowest
2. Carry out safety landing, eventually find the nearest airfield to land
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