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Manufacturer | ICP |
---|---|
Model | Savannah VG |
Seats | 2 |
Engine | Rotax 912 ULS |
Category | Light-sport aircraft |
Wingspan | 9.00 m (29 ft 6 in) |
Max Takeoff Weight | 450 kg |
Power | 100 hp |
Cruise Speed | 180 km/h |
Stall Speed | 65 km/h |
Range | 800 km |
Rate of Climb | 5.0 m/s (980 ft/min) |
Aircraft dimensions, weight, and powerplant details.
Details on wings, airframe, and stabilizer construction.
Covers landing gear, engine options, and control mechanisms.
Details propeller, fuel storage, delivery, and electrical setup.
Describes cabin features, instruments, and environmental controls.
Explains flight controls, flaps, pitot-static system, and baggage.
Specifies Vso, Vne, and other critical flight speeds.
Details maximum load factors and engine operational parameters.
Covers weight limitations, center of gravity, and flying weather.
Procedures for engine failure and various fire scenarios.
Addresses unintentional spins and cabin fires.
Outlines procedures for engine failure during ground roll and flight.
Covers pre-flight checks, exterior checks, and engine start-up.
Details taxiing techniques and normal/short take-off procedures.
Outlines procedures for cruise, descent, approach, and landing.
Covers crosswind landing, go-around, engine shutdown, and parking.
Details stall speeds with and without flaps, and take-off ground roll.
Provides landing distances and rate of climb data.
Explains CG range, loading, and modifications.
Outlines the procedure for determining the aircraft's basic empty weight.
Presents charts and tables for pilot computing of weight and balance.