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General| Manufacturer | Comco Ikarus |
|---|---|
| Type | Light aircraft |
| Crew | 1 |
| Capacity | 1 passenger |
| Max Takeoff Weight | 600 kg |
| Powerplant | Rotax 912 |
| Engine | Rotax 912ULS |
| Service ceiling | 4, 000 m (13, 125 ft) |
| Stall Speed | 64 km/h (40 mph, 35 kn) |
Specifies never-exceed, turbulent air, and stall speeds for different models.
Details maximum take-off and minimum payload weights.
Defines positive and negative limit load factors.
Specifies reference datum and CG limits.
Describes the white, green, and yellow arcs on the airspeed indicator.
Outlines maximum engine and continuous rpm limits.
Specifies operating limits for Rotax 912 and 912S engines, including oil and fuel.
Procedures for initiating flight and ascending.
Explains stall characteristics and recovery procedures.
Procedures for approaching and landing the aircraft safely.
Emergency procedures for engine failure during takeoff or flight.
Actions for specific in-flight emergencies like tipping, sideslip, and spin.
Forms and calculations for determining aircraft weight and balance.
Provides take-off distances for different conditions and weights.
Checks for the engine section during pre-flight inspection.
Details on towing gliders with the aircraft.
Actions to take in emergencies while towing.
Procedures and equipment for banner towing.
Steps for performing the skydiver drop.
Masterplan electrical circuit diagram for the aircraft.
