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General| Manufacturer | Alpi Aviation |
|---|---|
| Model | Pioneer 200 |
| Seats | 2 |
| Engine | Rotax 912ULS |
| Power | 100 hp |
| Length | 6.40 m (21 ft 0 in) |
| Empty Weight | 280 kg (617 lb) |
| Category | Aircraft |
| Engine Type | 4-cylinder, 4-stroke |
| Stall Speed | 65 km/h |
Speed limit that may not be exceeded at any time.
Stall speed in landing configuration.
Stall speed in landing config at most forward CG.
Extreme CG locations for operation.
Max weight for takeoff run start.
Lists aircraft specifications like engine, propeller, fuel, oil, and tyre pressures.
Lists critical airspeeds like Vne, Vno, Va, Vfe, Vso.
Maximum takeoff and landing weights for the aircraft.
Defines forward and aft CG limits for safe operation.
Operating limits and instrument ranges for the engine.
Specifies permitted and prohibited aircraft maneuvers.
The limiting demonstrated crosswind speed.
Critical airspeeds recommended for various emergency scenarios.
Procedures for engine failure during takeoff, after takeoff, and in flight.
Procedure for restarting the engine in flight if it stops.
Steps to take for fires during start, in flight, electrical, and cabin fires.
Procedures for emergency landings with or without engine power.
Specific procedure for landing with a deflated tyre.
Actions to take when electrical system fails.
Recommended airspeeds for minimum sink rate and maximum distance.
Steps to recover the aircraft from an unintended spin.
Detailed checklist for pre-flight walk-around and systems check.
Final checks and procedures before commencing takeoff.
Procedures for normal and short field takeoffs.
Procedures for normal, short field, and baulked landings.
Information on stall speeds and stall warning characteristics.
Details required distances for takeoff and landing.
Defines operational CG limits and includes a CG diagram.
