Section 2 - Limitations
Speed Limitations
Airspeed Indicator Markings
Powerplant Limitations
Following table reports the operating limitations for both engines installed:
Engine Manufacturer: Bombardier Rotax GmbH.
Engine Model: 912 S3
Maximum Power:
Temperatures:
Max CHT: 135°C
Max CT:120°C
Min/Max Oil: 50°C / 130°C
Oil normal operating range (approx.): 90°C / 110°C
Oil Pressure (below 1400 rpm prop):
Minimum: 0.8 Bar / 12 psi
Normal: 2-5 Bar / 29-73 psi
Maximum: 7 Bar / 102 psi
Fuel pressure:
Minimum: 0.15 Bar / 2.2 psi
Maximum 0.40 Bar / 5.8 psi
Maximum Operating Altitude
Maximum operating altitude is 14000 ft (4260 m) MSL.
Ambient Temperature
Ambient temperature: from -25°C to +50°C. Flight in expected and/or known icing conditions is forbidden.
Powerplant Instruments Markings
"0" Indication
Shows the unusable fuel quantity (2,8 litres for each fuel tank).
Other Instruments Markings
Warnings, Cautions and Advisories Lights
Weights
Approved Maneuvers
The aircraft is certified in normal category in accordance with EASA CS-23 regulation.
Non aerobatic operations include:
Any manoeuvre pertaining to “normal” flight
Stalls (except whip stalls)
Lazy eights
Turns in which the angle of bank is not more than 60°
Chandelle
Maneuvers Load Factor Limits
Flight Crew
Minimum crew: 1 pilot
Maximum number of occupants: 4 people (including the pilot)
Flight Conditions
The aircraft can be equipped for following flight operations:
VFR Day and Night
IFR Day and Night including IMC
Flight in expected and/or known icing conditions, in proximity of storms or severe turbulence is forbidden.
Fuel
2 Tanks: 100 litres each one (26.42 US gallons)
Maximum Capacity: 200 litres (52.8 US gallons)
Maximum Usable Fuel: 194.4 litres (51.35 US gallons)
Approved Fuel: MOGAS / AVGAS