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At a glance
Measured figures
Cruise; Beechcraft 1900D · at 20,000 ft (6,100 m)
Single source280 kn (322 mph, 518 km/h) at 20,000 ft (6,100 m)[source]
Beechcraft 1900D · 2 × Pratt & Whitney Canada PT6A-67D turboprops , 1,279 shp ( ) each
Single source2 × Pratt & Whitney Canada PT6A-67D turboprops , 1,279 shp (955 kW) each[source]
Alto TG European ultralight · 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 hp)[source]
Beechcraft 1900D · Service ceiling
Single source25,000 ft (7,620 m)[source]
Alto TG European ultralight · Wing area
Single source10.14 m 2 (109.1 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Beechcraft 1900 | Direct Fly Alto |
|---|---|---|
| Type | Regional airliner , cargo , and corporate aircraft[source] | Light sport aircraft[source] |
| Manufacturer | Beech Aircraft Corporation Raytheon Aircraft Company[source] | Direct Fly s.r.o.[source] |
| Status | In service[source] | In production[source] |
| Primary users | Ameriflight Alpine Air Express Central Mountain Air Propair[source] | — |
| Number built | 695[source] | 41 (2015)[source] |
| Manufactured | 1982–2002[source] | — |
| Introduction date | February 1984[source] | 2008[source] |
| First flight | September 3, 1982[source] | — |
| Developed from | Beechcraft Super King Air[source] | — |
| Capacity | 19 passengers and 6,356 lb (2,882 kg) useful load[source] | one passenger[source] |
| Fuel capacity | 4,458 lb (2,022 kg)[source] | 118 litres (26 imp gal; 31 US gal)[source] |
| Fuel type | Jet A recommended, others usable[source] | — |
| National origin | United States[source] | Czech Republic[source] |
| Primary user | — | Ukrainian Air Force[source] |
| Stall speed | — | 65 km/h (40 mph, 35 kn)[source] |
| Never exceed speed | — | 270 km/h (170 mph, 150 kn)[source] |
| g limits | — | +4/-2[source] |
| Wing loading | — | 46.6 kg/m 2 (9.5 lb/sq ft)[source] |