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At a glance
Measured figures
L 410NG · Length
Single source15.074 m (49 ft 5 in)[source]
C-47B-DK · Length
Configuration
| Specification | Aircraft Industries L 410 NG | Douglas C-47 Skytrain |
|---|---|---|
| Type | Regional airliner , cargo aircraft[source] | Military transport aircraft[source] |
| Manufacturer | Aircraft Industries (Let Kunovice)[source] | Douglas Aircraft Company[source] |
| Status | In service[source] | In service[source] |
| Manufactured | 2018–present[source] |
63 ft 9 in (19.43 m)[source]
Maximum take-off; L 410NG · Max takeoff weight
Single source7,000 kg (15,432 lb)[source]
L 410NG · at FL140 with reserve fuel
Single source2,750 km (1,710 mi, 1,480 nmi) at FL140 with reserve fuel[source]
C-47B-DK · 2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines takeoff rating
Single sourceC-47B-DK · normal rating at 14,500 ft (4,400 m)
Single source2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines 1,200 hp (890 kW) takeoff rating 1,000 hp (750 kW) normal rating at 14,500 ft (4,400 m)[source]
L 410NG · Endurance
Single source10 hours 30 minutes[source]
L 410NG · 1,670 ft/min
Single source8.5 m/s (1,670 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| First flight | 29 July 2015[source] | 23 December 1941 ( 1941-12-23 )[source] |
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| Developed from | Let L-410 Turbolet[source] | Douglas DC-3[source] |
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| Capacity | 19 passengers / 2,300 kg (5,071 lb) load[source] | 28 troops or 6,000 lb (2,700 kg) of cargo[source] |
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| Airfoil | root: NACA 63A418 ; tip: NACA 63A412[source] | root: NACA 2215 ; tip: NACA 2206[source] |
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| Cabin volume for passengers | 17.9 m 3 (632 cu ft)[source] | — |
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| Passenger doors | 0.8 m × 1.46 m (2 ft 7 in × 4 ft 9 in)[source] | — |
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| Cargo door | 1.25 m × 1.46 m (4 ft 1 in × 4 ft 9 in)[source] | — |
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| Seat pitch at max. Capacity | 0.76 m (2 ft 6 in)[source] | — |
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| Luggage compartment volume | 2.31 m 3 (82 cu ft)[source] | — |
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| Maximum landing weight | 6,800 kg (14,991 lb)[source] | — |
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| Fuel capacity | 2,244 kg (4,947 lb)[source] | — |
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| Powerplant | 2 × General Electric H85-200 turboprop engines[source] | — |
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| Propellers | 5-bladed Avia -725 constant-speed propellers[source] | 3-bladed constant-speed propellers[source] |
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| Service ceiling on one engine | 3,900 m (12,800 ft) (ISA, 95% MTOW, 15 m/min (50 ft/min) climb rate )[source] | — |
|---|
| Absolute ceiling | 8,230 m (27,000 ft)[source] | — |
|---|
| Take-off run | 600 m (2,000 ft)[source] | — |
|---|
| Landing run | 590 m (1,940 ft)[source] | — |
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| Source measurement | With these improvements, the L 410 NG has doubled the maximum distance it can fly and can carry 500 kilograms in increased payload than the previous model. Like its predecessor L 410 UVP-E20, it will be sold in all variations. It is intended for commercial airlines, government agencies, non-governmental organizations, and armed forces. In addition to the passenger version , it can also be configured as a cargo plane . It can be used especially in island states where there is a problem of refueling in remote islands.[source]Aircraft Industries L 410 NG · Design; only the objects and conditions stated in this passage Capacity: 19 passengers / 2,300 kg (5,071 lb) load[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Length: 15.074 m (49 ft 5 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Wingspan: 19.478 m (63 ft 11 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Height: 5.969 m (19 ft 7 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Wing area: 34.86 m 2 (375.2 sq ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Cabin volume for passengers: 17.9 m 3 (632 cu ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Passenger doors: 0.8 m × 1.46 m (2 ft 7 in × 4 ft 9 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Cargo door: 1.25 m × 1.46 m (4 ft 1 in × 4 ft 9 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Seat pitch at max. Capacity: 0.76 m (2 ft 6 in)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Luggage compartment volume: 2.31 m 3 (82 cu ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Max takeoff weight: 7,000 kg (15,432 lb)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Maximum landing weight: 6,800 kg (14,991 lb)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Fuel capacity: 2,244 kg (4,947 lb)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Maximum speed: 417 km/h (259 mph, 225 kn) TAS[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Range: 2,750 km (1,710 mi, 1,480 nmi) at FL140 with reserve fuel[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Endurance: 10 hours 30 minutes[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Service ceiling: 6,100 m (20,000 ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Service ceiling on one engine: 3,900 m (12,800 ft) (ISA, 95% MTOW, 15 m/min (50 ft/min) climb rate )[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Absolute ceiling: 8,230 m (27,000 ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Rate of climb: 8.5 m/s (1,670 ft/min)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage 1.7 m/s (6 ft/s) on one engine[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Take-off run: 600 m (2,000 ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage Landing run: 590 m (1,940 ft)[source]Aircraft Industries L 410 NG · Specification (L 410NG); only the objects and conditions stated in this passage | — |
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| Country of origin | Czechia[source]Inventory Origin column; table 2, row 6, cell 2; revision 1368823875; retrieved 2026-10-02 | — |
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| National origin | — | United States[source] |
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| Primary users | — | United States Army Air Forces Royal Air Force United States Navy Royal Canadian Air Force See operators[source] |
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| Number built | — | 10,174[source] |
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| Variants | — | Douglas XCG-17 Douglas AC-47 Spooky Douglas R4D-8[source] |
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| Time to altitude | — | 10,000 ft (3,000 m) in 9 minutes 30 seconds[source] |
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| Wing loading | — | 26.3 lb/sq ft (128 kg/m 2 )[source] |
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| Power/mass | — | 0.0926 hp/lb (0.1522 kW/kg)[source] |
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| Reported operators | — |
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