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Regional airliner , cargo aircraft
Aircraft Industries L 410 NG is a regional airliner , cargo aircraft. It was built by Aircraft Industries (Let Kunovice).
CzechiaRegional airliner , cargo aircraft
Aircraft Industries (Let Kunovice)
In service
2018–present
29 July 2015
Let L-410 Turbolet
2
19 passengers / 2,300 kg (5,071 lb) load
15.074 m (49 ft 5 in)
19.478 m (63 ft 11 in)
5.969 m (19 ft 7 in)
34.86 m 2 (375.2 sq ft)
root: NACA 63A418 ; tip: NACA 63A412
17.9 m 3 (632 cu ft)
0.8 m × 1.46 m (2 ft 7 in × 4 ft 9 in)
1.25 m × 1.46 m (4 ft 1 in × 4 ft 9 in)
0.76 m (2 ft 6 in)
2.31 m 3 (82 cu ft)
7,000 kg (15,432 lb)
6,800 kg (14,991 lb)
2,244 kg (4,947 lb)
2 × General Electric H85-200 turboprop engines
5-bladed Avia -725 constant-speed propellers
417 km/h (259 mph, 225 kn) TAS
2,750 km (1,710 mi, 1,480 nmi) at FL140 with reserve fuel
10 hours 30 minutes
6,100 m (20,000 ft)
3,900 m (12,800 ft) (ISA, 95% MTOW, 15 m/min (50 ft/min) climb rate )
8,230 m (27,000 ft)
8.5 m/s (1,670 ft/min)
600 m (2,000 ft)
590 m (1,940 ft)
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.
Capacity: 19 passengers / 2,300 kg (5,071 lb) load
Length: 15.074 m (49 ft 5 in)
Wingspan: 19.478 m (63 ft 11 in)
Height: 5.969 m (19 ft 7 in)
Wing area: 34.86 m 2 (375.2 sq ft)
Cabin volume for passengers: 17.9 m 3 (632 cu ft)
Passenger doors: 0.8 m × 1.46 m (2 ft 7 in × 4 ft 9 in)
Cargo door: 1.25 m × 1.46 m (4 ft 1 in × 4 ft 9 in)
Seat pitch at max. Capacity: 0.76 m (2 ft 6 in)
Luggage compartment volume: 2.31 m 3 (82 cu ft)
Max takeoff weight: 7,000 kg (15,432 lb)
Maximum landing weight: 6,800 kg (14,991 lb)
Fuel capacity: 2,244 kg (4,947 lb)
Maximum speed: 417 km/h (259 mph, 225 kn) TAS
Range: 2,750 km (1,710 mi, 1,480 nmi) at FL140 with reserve fuel
Endurance: 10 hours 30 minutes
Service ceiling: 6,100 m (20,000 ft)
Service ceiling on one engine: 3,900 m (12,800 ft) (ISA, 95% MTOW, 15 m/min (50 ft/min) climb rate )
Absolute ceiling: 8,230 m (27,000 ft)
Rate of climb: 8.5 m/s (1,670 ft/min)
1.7 m/s (6 ft/s) on one engine
Take-off run: 600 m (2,000 ft)
Landing run: 590 m (1,940 ft)
L 410 NG Czechia Propeller Transport 0/1
Reference text from Wikipedia contributors, used under CC BY-SA 4.0.
True scale
Sourced dimensions beside a 1.75 m human reference.
Points represent sourced observations, including revisions. Revisions on the same effective date are not separate inventory events. Ranges appear in the table and are not plotted as exact points.
| Observation / report period | Value | Source | Claim state |
|---|---|---|---|
| 29 Sept 2026 | 15.074 m | Wikipedia contributors | superseded |
| 29 Sept 2026 | 15.074 m | Wikipedia contributors | superseded |
| 29 Sept 2026 | 15.074 m | Wikipedia contributors | superseded |
| 29 Sept 2026 | 15.074 m | Wikipedia contributors | approved |