Aircraft Industries L 410 NG vs Pilatus PC-24

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Aircraft Industries L 410 NG — licensed reference photograph

ASupport aircraft

Aircraft Industries L 410 NG

Regional airliner , cargo aircraft

Credit

Julian Herzog ( Website ) · CC BY 4.0 · Resized · CC BY 4.0 · Source ↗ · Modified

Pilatus PC-24 — licensed reference photograph

BSupport aircraft

Pilatus PC-24

Light business jet

Credit

Stephan Widmer · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Aircraft Industries L 410 NGL 410NG · Length

15.074 m

Length source ↗

Pilatus PC-24Length

16.85 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

17 of 50 rows sourced on both sides

15.07mL 410NG · Length

16.85m

Length

All recorded figures & sources

15.074 m

L 410NG · Length

Single source

15.074 m (49 ft 5 in)^[source]

16.85 m

Length

Single source

Configuration

Details

Aircraft Industries L 410 NG and Pilatus PC-24 configuration
Specification	Aircraft Industries L 410 NG	Pilatus PC-24
Type	Regional airliner , cargo aircraft^[source]	Light business jet^[source]
Manufacturer	Aircraft Industries (Let Kunovice)^[source]	Pilatus Aircraft^[source]
Status	In service^[source]	In production^[source]
Manufactured	2018–present^[source]

First flight	29 July 2015^[source]	11 May 2015^[source]

Developed from	Let L-410 Turbolet^[source]	—

Capacity	19 passengers / 2,300 kg (5,071 lb) load^[source]	10 passengers^[source]

Airfoil	root: NACA 63A418 ; tip: NACA 63A412^[source]	—

Cabin volume for passengers	17.9 m 3 (632 cu ft)^[source]	—

Passenger doors	0.8 m × 1.46 m (2 ft 7 in × 4 ft 9 in)^[source]	—

Cargo door	1.25 m × 1.46 m (4 ft 1 in × 4 ft 9 in)^[source]	—

Seat pitch at max. Capacity	0.76 m (2 ft 6 in)^[source]	—

Luggage compartment volume	2.31 m 3 (82 cu ft)^[source]	—

Maximum landing weight	6,800 kg (14,991 lb)^[source]	—

Fuel capacity	2,244 kg (4,947 lb)^[source]	2,705 kg (5,964 lb), 888.5 US gal (3,363 L)^[source]

Powerplant	2 × General Electric H85-200 turboprop engines^[source]	—

Propellers	5-bladed Avia -725 constant-speed propellers^[source]	—

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]	—

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	—

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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