| Název: Name: | Let L-410NG | Let L-410NG |
| Originální název: Original Name: | Let L-410NG | |
| Kategorie: Category: | dopravní letoun | passenger aeroplane |
| Výrobce: Producer: | DD.MM.2015-DD.MM.RRRR Aircraft Industries, a.s., Kunovice | |
| Období výroby: Production Period: | DD.02.2018-DD.MM.RRRR | |
| Vyrobeno kusů: Number of Produced: | 2 prototypy 5 (Senegal, Air Senegal) | |
| První vzlet: Maiden Flight: | 15.07.2015 | |
| Osádka: Crew: | 2+19 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | ? kg | ? lb |
| Vzletová hmotnost: Take-off Weight: | 2150 kg | 4740 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 7000 kg | 15432 lb |
| Rozpětí: Wingspan: | 19,98 m | 65 ft 6 ⅝ in |
| Délka: Length: | 15,074 m | 49 ft 5 ½ in |
| Výška: Height: | 5,969 m | 19 ft 7in |
| Plocha křídla: Wing Area: | ? m2 | ? ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | turbovrtulový | turboprop |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | GE Aviation H85-200 BC04 s pětilistou vrtulí Avia Propeller AV 725 o průměru 2,3 m. | GE Aviation H85-200 BC04 with five-bladed propeller Avia Propeller AV 725, diameter 90,5 in |
| Objem palivových nádrží: Fuel Tank Capacity: | 2340 kg | 5159 lb |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | ? km/h v ? m | ? mph in ? ft |
| Cestovní rychlost: Cruise Speed: | 417 km/h v ? m | 259 mph in ? ft |
| Rychlost stoupání: Climb Rate: | 8,5 m/s | 1673 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 4200 m | 13780 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | 2570 km | 1597 mi |
| Výzbroj: Armament: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | vytrvalost 10 h maximální nosnost 2154 kg "skleněný kokpit" - avionický systém Garmin G3000 | endurance 10 hr maximum payload 4749 lb "glass cockpit" - avionic system Garmin G3000 |
| Zdroje: Sources: | Kolmann, Petr: Nastupuje nová generace "Čtyřistadesítky", Letectví a kosmonautika 2015 / 08 www.let.cz | |
Let L-410NG
The forthcoming modernization of the L-410UVP-E20. In the production of the hull is min. one of the aircraft. The changes are mainly on the fuselage and connected with its extension.
The aim of the project MOSTA (modernisation of small transport aircraft) are:
an increase of the maximum paying load
enlargement of the luggage compartments
the increase in travel speed
zoom range
improve the performance of the aircraft in hot and high altitude conditions
extend the life of at least 30 000 flight hours
the introduction of modern maintenance systems - maintenance according to the condition of
improving techno-economic parameters of the devices and aggregates
a simplification of the construction (reduce the labor intensity of production)
modernization of instrumentation in the cockpit
Engines should be of type GE H80-200 (formerly Walter M601H 80) and propellers AV-725.
Source: www.technodat.cz
www.let.cz
own visit AI Kunovice.
tohle by měl být prodloužená přední část MOSTy, vlastní foto
The aim of the project MOSTA (modernisation of small transport aircraft) are:
an increase of the maximum paying load
enlargement of the luggage compartments
the increase in travel speed
zoom range
improve the performance of the aircraft in hot and high altitude conditions
extend the life of at least 30 000 flight hours
the introduction of modern maintenance systems - maintenance according to the condition of
improving techno-economic parameters of the devices and aggregates
a simplification of the construction (reduce the labor intensity of production)
modernization of instrumentation in the cockpit
Engines should be of type GE H80-200 (formerly Walter M601H 80) and propellers AV-725.
Source: www.technodat.cz
www.let.cz
own visit AI Kunovice.
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tohle by měl být prodloužená přední část MOSTy, vlastní foto
Reklama
The first prototype L-410NG (serial number 2820).
(Aircraft Industries)
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The cockpit of the first L-410NG prototype.
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(Aircraft Industries)
The second produced aircraft L-410NG reg. OK-NGB at the NATO Days in Ostrava-Mošnov, 18 September 2022.
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Reklama
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