FORCETALLY
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At a glance
Measured figures
Beechcraft 1900D · Length
Single source57 ft 8 in (17.62 m)[source]
Length
Single sourceConfiguration
| Specification | Beechcraft 1900 | Learjet 55 |
|---|---|---|
| Type | Regional airliner , cargo , and corporate aircraft[source] | Business jet[source] |
| Manufacturer | Beech Aircraft Corporation Raytheon Aircraft Company[source] | Learjet[source] |
| Status | In service[source] | In service[source] |
| Primary users | Ameriflight Alpine Air Express Central Mountain Air Propair[source] | — |
55 ft 1 in (16.80 m)[source]
Empty; Beechcraft 1900D · Empty weight
Single sourceGross; Beechcraft 1900D · Gross weight
Single sourceMaximum take-off; Beechcraft 1900D · Max takeoff weight
Single source10,874 lb (4,932 kg)[source]
17,227 lb (7,814 kg)[source]
17,120 lb (7,764 kg)[source]
Empty; Empty weight
Single sourceMaximum take-off; Max takeoff weight
Single sourceCruise; 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 · with 19 passenger payload
Single sourceFerry; Beechcraft 1900D · Ferry range
Single source382 nmi (439 mi, 707 km) with 19 passenger payload[source]
1,245 nmi (1,432 mi, 2,306 km)[source]
with four passengers and fuel reserves
Single source2,492 mi (4,010 km, 2,165 nmi) with four passengers and fuel reserves[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]
2 × Garrett TFE731-3A-2B turbofan aero-engine thrust each
Single source2 × Garrett TFE731-3A-2B turbofan aero-engine, 3,700 lbf (16 kN) thrust each[source]
Beechcraft 1900D · 2,615 ft/min (
Single source2,615 ft/min (13.28 m/s)[source]
Wing area
Single source264.5 sq ft (24.57 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 695[source] | 147[source] |
|---|
| Manufactured | 1982–2002[source] | 1979–1987[source] |
|---|
| Introduction date | February 1984[source] | 1981[source] |
|---|
| First flight | September 3, 1982[source] | 19 April 1979[source] |
|---|
| Developed from | Beechcraft Super King Air[source] | — |
|---|
| Capacity | 19 passengers and 6,356 lb (2,882 kg) useful load[source] | 10[source] |
|---|
| Fuel capacity | 4,458 lb (2,022 kg)[source] | — |
|---|
| Fuel type | Jet A recommended, others usable[source] | — |
|---|
| National origin | United States[source] | United States[source] |
|---|
| Developed into | — | Learjet 60[source] |
|---|