Credit
Michal šenki · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
L-59E · Length
Single source12.20 m (40 ft 0 in)[source]
Beechcraft 1900D · Length
Single sourceConfiguration
| Specification | Aero L-59 Super Albatros | Beechcraft 1900 |
|---|---|---|
| Type | Military trainer aircraft COIN[source] | Regional airliner , cargo , and corporate aircraft[source] |
| Manufacturer | Aero Vodochody[source] | Beech Aircraft Corporation Raytheon Aircraft Company[source] |
| Status | Out of production, in service[source] | In service[source] |
| Primary users | Czech Air Force Egyptian Air Force Tunisian Air Force[source] |
57 ft 8 in (17.62 m)[source]
Empty; L-59E · includes gun
Single sourceMaximum take-off; L-59E · Max takeoff weight
Single source4,030 kg (8,885 lb) (includes gun)[source]
7,000 kg (15,432 lb)[source]
Empty; Beechcraft 1900D · Empty weight
Single sourceGross; Beechcraft 1900D · Gross weight
Single sourceL-59E · at 7,000 m (23,000 ft) (with maximum internal and external fuel)
Single source2,000 km (1,200 mi, 1,100 nmi) at 7,000 m (23,000 ft) (with maximum internal and external fuel)[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]
L-59E · 1 × Lotarev DV-2 turbofan thrust
Single source1 × Lotarev DV-2 turbofan , 21.57 kN (4,850 lbf) thrust[source]
L-59E · Wing area
Single source18.80 m 2 (202.4 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Ameriflight Alpine Air Express Central Mountain Air Propair[source] |
| Number built | 80[source] | 695[source] |
|---|
| Manufactured | 1986–1996[source] | 1982–2002[source] |
|---|
| First flight | 30 September 1986[source] | September 3, 1982[source] |
|---|
| Developed from | Aero L-39 Albatros[source] | Beechcraft Super King Air[source] |
|---|
| Variant | Aero L-159 ALCA[source] | — |
|---|
| Fuel capacity | 1,537 L (406 US gal; 338 imp gal) including tip tanks[source] | 4,458 lb (2,022 kg)[source] |
|---|
| Stall speed | 185 km/h (115 mph, 100 kn) (flaps down)[source] | — |
|---|
| Guns | one GSh-23L cannon in under-fuselage pod[source] | — |
|---|
| Hardpoints | four underwing hardpoints with a capacity of inner hardpoints 500 kg (1,100 lb)capacity, outer hardpoints 250 kg (550 lb)[source] | — |
|---|
| Country of origin | Czechoslovakia[source]Inventory Origin column; table 1, row 26, cell 2; revision 1374778711; retrieved 2026-10-01 | — |
|---|
| Introduction date | — | February 1984[source] |
|---|
| Capacity | — | 19 passengers and 6,356 lb (2,882 kg) useful load[source] |
|---|
| Fuel type | — | Jet A recommended, others usable[source] |
|---|
| National origin | — | United States[source] |
|---|
Maximum take-off; Beechcraft 1900D · Max takeoff weight
Single source