TYPE: Single-seat ultralight kitbuilt.
PROGRAMME: Derived from Pioneer Flightstar II. Can conform to FAR Pt 103.
CURRENT VERSIONS: Spyder: Standard version, as described.
Formula: High-performance upgraded model with wider windscreen and cockpit doors for cold weather flying; now discontinued.
CUSTOMERS: Total of 112 kits sold, and 110 flying, by mid-2001.
COSTS: Spyder US$10,995 without engine (2003).
DESIGN FEATURES: Flightstar FS-I-2 aerofoil. Wings fold for storage and transportation. Optional BRS parachute recovery system.
FLYING CONTROLS: As Flightstar II SL.
STRUCTURE: As Flightstar II SL.
LANDING GEAR: As Flightstar II SL.
POWER PLANT: One 31.0 kW (41.6 hp) Rotax 447 UL-2V driving Tennessee two-blade or three-blade propeller. Options include 37.0 kW (49.6 hp) Rotax 503 UL-2V and 47.8 kW (64.1 hp) Rotax 582 UL. Standard fuel capacity 18.9 litres (5.0 US gallons; 4.2 Imp gallons); optionally 37.9 litres (10.0 US gallons; 8.3 Imp gallons).
DIMENSIONS, EXTERNAL:
- Wing span: 9.14 m (30 ft 0 in)
- Length overall: 5.03 m (16 ft 6 in)
- Height overall: 2.39 m (7 ft 10 in)
AREAS:
- Wings, gross: 13.38 m² (144.0 sq ft)
WEIGHTS AND LOADINGS:
- Weight empty: 127 kg (280 lb)
- Max T-O weight: 294 kg (650 lb)
PERFORMANCE:
- Never-exceed speed (VNE): 83 kt (154 km/h; 96 mph)
- Max operating speed: 74 kt (137 km/h; 85 mph)
- Normal cruising speed: 48 kt (89 km/h; 55 mph)
- Stalling speed: 28 kt (52 km/h; 32 mph)
- Max rate of climb at S/L: 201 m (660 ft)/min
- T-O run: 62 m (205 ft)
- Landing run: 61 m (200 ft)
- Range with standard fuel: 86 n miles (161 km; 100 miles)
The article appears in the following publication:
Jane's All the World's Aircraft 2004-2005. Jane's Information Group Ltd. 2004. ISBN: 0-7106-2614-2
