Basic Aircraft Characteristics
The L 410 UVP-E20 is an all-metal, high-wing, turboprop commuter aircraft powered by two GE H80-200 engines and AV-725 propellers. It is designed for short-haul transport of up to 19 passengers and cargo, particularly from remote areas to major cities. Over 1,200 units have been produced since 1969, with more than 350 currently in operation across 50 countries.

Aircraft Advantages

• STOL capabilities for short unpaved runways.
• Durable structure for severe conditions.
• Performance in hot and high environments.
• Operational range in extreme climates from ±50°C.
• Versatility with quick change kits.
• Spacious passenger compartment in its category.
• Easy handling with low operating and maintenance costs.
• Excellent safety record and reliability.

Certificates
The aircraft is certified in the Commuter Category by EASA and FAA under FAR 23 Regulation Amendment 41.

Aircraft Variants
The aircraft offers a spacious oval fuselage with 18 m³ of passenger cabin volume, providing comfort and versatility for various operations including:

• Standard commuter
• Cargo
• VIP
• Air ambulance/Medivac
• Sky diving
• Photogrammetric scanning
• Maritime, patrol, and surveillance

Customers
The L 410 UVP-E20 is used globally by private airlines, governmental and non-governmental organizations, air forces, and aero clubs.

Dimensions and Capacity

• Passenger Cabin Volume: 17.9 m³ (632 cu.ft)
• Passenger Door: 0.8x1.46 m (2.6x4.8 ft)
• Cargo Door: 1.25x1.46 m (4.1x4.8 ft)
• Seats Pitch: 0.76 m (30 inch)
• Luggage Compartment Volume: 1.47 m³ (51.9 cu.ft)
• Wing Area: 34.86 sq.m (375.23 sq.ft)
• Max. Take-off Weight (MTOW): 6,600 kg (14,550 lb)
• Max. Landing Weight (MLDW): 6,400 kg (14,109 lb)
• Max. Payload: 1,800 kg (3,968 lb)
• Max. Fuel Weight (with tip tanks): 1,300 kg (2,866 lb)

Performance

• Max. Cruise Speed: 405 km/hr TAS (219 KTAS)
• Max. Range: 1,500 km (810 NM) with a 45-minute fuel reserve
• Max. Endurance: 5.1 hours
• Climb Rate: 8.5 m/s (1,673 fpm) with both engines; 1.8 m/s (354 fpm) with a single engine
• Take-off Distance to 35 ft: 510 m (1,673 ft)

Capacity
The aircraft can accommodate 19 passengers and requires a crew of 2 pilots. The interior displayed was produced by "Tulpar IG", RF.