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At a glance
Measured figures
Li-2P · Length
Single source19.65 m (64 ft 6 in)[source]
Length
Single sourceConfiguration
| Specification | Lisunov Li-2 | Pilatus PC-24 |
|---|---|---|
| Type | Cargo/passenger utility aircraft and light bomber[source] | Light business jet[source] |
| National origin | Soviet Union[source] | Switzerland[source] |
| Manufacturer | State Aircraft Plant No. 84[source] | Pilatus Aircraft[source] |
| Status | Out of production; in limited service[source] | In production |
16.85 m (55 ft 3 in)[source]
Li-2P · 2 × Shvetsov M-62 9-cylinder air-cooled radial piston engines each
Single source2 × Shvetsov M-62 9-cylinder air-cooled radial piston engines, 670 kW (900 hp) each[source]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
(3,960 ft/min) MTOW, at Sea level
Single source20.1 m/s (3,960 ft/min) MTOW, at Sea level[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Soviet Air Force Aeroflot[source] | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Number built | 6,157 (per later research 4,937)[source] | 212 (Q1 2024)[source] |
|---|
| Manufactured | 1939–1952[source] | 2015–present[source] |
|---|
| Introduction date | 1939[source] | 1 April 2018[source] |
|---|
| Developed from | Douglas DC-3[source] | — |
|---|
| Capacity | 24 passengers / (20 troops Li-2T )[source] | 10 passengers[source] |
|---|
| Guns | * 3× 7.62 mm (.30 in) ShKAS machine guns Li-2T / Li-2VV[source] | — |
|---|
| Airfoil | root: NACA 2215 ; tip: NACA 2206[source] | — |
|---|
| Propellers | 3-bladed variable-pitch propellers[source] | — |
|---|
| Bombs | * 1,000 kg bombs (normal load) Li-2VV[source] | — |
|---|
| First flight | — | 11 May 2015[source] |
|---|
| Aspect ratio | — | 9.35[source] |
|---|
| Fuel capacity | — | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Cabin | — | 7.01 m × 1.69 m × 1.55 m long × wide × high ( 23 ft 0 in × 5 ft 7 in × 5 ft 1 in)[source] |
|---|
| Cabin altitude | — | 2,438 m at 13,716 m (8,000 ft at 45,000 ft), 8.78 psi (0.605 bar)[source] |
|---|
| Stall speed | — | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Time to altitude | — | 45,000 ft (14,000 m) 27.1 mins[source] |
|---|
| Wing loading | — | 259 kg/m 2 (53 lb/sq ft)[source] |
|---|
| Fuel consumption | — | 0.58 kg/km (2.1 lb/mi) Mach 0.72/416 kn (770 km/h) cruise, 15,375 lb (6,974 kg) weight, FL 450, ISA+3C[source] |
|---|
| Thrust/weight | — | 0.36[source] |
|---|
| Take-off | — | 942 m; 3,091 ft (MTOW, ISA, sea level, dry paved runway)[source] |
|---|
| Landing | — | 734 m; 2,408 ft (Over 50 ft obstacle, MLW, ISA, sea level, dry paved runway)[source] |
|---|
Maximum take-off; Max takeoff weight
Single source