Stoddard-Hamilton Glasair I
The Glasair I, originally built as the prototype Glasair TD taildragger, is a high-performance homebuilt aircraft built of fiberglass. Created by Tom Hamilton as a fast, two-seat kitplane, the Glasair TD was derived from the earlier Tom Hamilton Glasair and first flew in 1979. Hamilton formed Stoddard-Hamilton Aircraft that year to produce and market the kit, which was the first pre-molded composite aircraft available to builders.
| Glasair I | |
|---|---|
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| Role | amateur-built kit airplane | 
| Manufacturer | Stoddard-Hamilton Aircraft Glasair Aviation  | 
| First flight | 1979 | 
| Introduction | 1980 | 
| Number built | 807[1] | 
| Developed into | Stoddard-Hamilton Glasair II | 

Glasair I TD (modified with non-standard dorsal fin)
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Glasair I. EAA AirVenture 2011
Specifications (Glasair 1 )
    
Data from Pilot Friend[2]
General characteristics
- Crew: one
 - Capacity: one passenger
 - Length: 19 ft 6 in (5.94 m)
 - Wingspan: 24 ft 4 in (7.42 m)
 - Height: 6 ft 2 in (1.88 m)
 - Wing area: 81.3 sq ft (7.55 m2)
 - Empty weight: 1,368 lb (621 kg)
 - Gross weight: 2,200 lb (998 kg)
 - Fuel capacity: 61.4 US gallons (232 litres)
 - Powerplant: 1 × Lycoming IO-360 A1B four cylinder, horizontally opposed, four stroke aircraft engine, 200 hp (150 kW)
 - Propellers: 3-bladed Hoffmann VP with wood blades
 
Performance
- Maximum speed: 260 mph (420 km/h, 230 kn)
 - Cruise speed: 201 mph (324 km/h, 175 kn)
 - Stall speed: 65 mph (105 km/h, 56 kn)
 - Never exceed speed: 260 mph (420 km/h, 230 kn)
 - Range: 1,177 mi (1,894 km, 1,023 nmi)
 - Service ceiling: 19,000 ft (5,800 m)
 - Rate of climb: 1,500 ft/min (7.6 m/s)
 - Wing loading: 27.06 lb/sq ft (132.1 kg/m2)
 
References
    
 Media related to Stoddard-Hamilton Glasair at Wikimedia Commons
- Bud Daviddson (May 2014). "35 Years of Fast Glas". Sport Aviation: 53.
 - Pilot Friend - Glasair 1
 
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