L 410 NG

Aircraft Industries, a.s. • Kunovice • Czech Republic • phone: +420 572 817 310 • sales@let.cz • www.let.cz

L 410 NGBasic Aircraft Characteristics

The L 410 NG, brand new turboprop commuter, inheriting the best of L 410 family aircraft, offers now improved flight parameters and operational characteristics, modern technologies and advanced avionics. Thanks to the new wing structure, with integral fuel tank and increased capacity, the L 410 NG enables significantly longer range and endurance. The all-metal, high-wing twin turboprop, powered by new more powerful GE H85 engines and AV-725 propellers, is in its standard version, intended for short-haul transport from remote and undeveloped areas to major cities. The multipurpose aircraft can accommodate 19 passengers and thanks to its increased payload and larger luggage compartment can carry up to approx. 400 kg more cargo. With its spacious oval fuselage provides the highest standard of passenger comfort and offers maximum versatility and opportunity to use the aircraft for a number of different operations. Since 1969, more than 1 200 aircraft in the L 410 series have been produced. Currently, there are over 350 aircraft in more than 50 countries all over the world in operation. The L 410 NG is developed for private airlines as well as governmental and non-governmental organizations and air forces.

Aircraft Advantages

• Ability to land and to take off on short unpaved runways (STOL capabilities)

• Remarkable hot and high performance

• Modern Glass Cockpit

• Tough and durable structure which enables operation in severe conditions

• Ability to operate under extreme climatic conditions ranging from ±50 °C

• Outstanding versatility with a number of quick change kits

• The most spacious passenger compartment in the commuter category

• Easy handling and low operating and maintenance costs

• Excellent safety record and reliable operation

EMB-110 Bandeirante L 410 NG

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Standard Passenger Version

Cargo Version

VIP Version

Dimensions Passenger Cabin Volume 17,9 m3 632 cu.ftCabin length 6,35 m 249,803 inchCabin width 1,95 m 76,9 inchCabin height 1,66 m 65,4 inchPassenger Door 0,8x1,46 m 2,6x4,8 ftCargo Door 1,25x1,46 m 4,1x4,8 ftSeats Pitch 0,76 m 30 inchLuggage Compartment Volume 2,98 m3 105,238 cu.ftWing Area 34.86 sg.m. 375.23 sq.ft

Weight Max. Take-off Weight (MTOW) 7 000 kg 15 435 IbMax. Landing Weight (MLDW) 6 800 kg 14 991 IbMax. Payload 2 154 kg 4 749 IbMax. Fuel Weight (with tip tanks) 2 340 kg 5 159 Ib

Performance Max. Cruise Speed 417 km/hr TAS 225 KTASMax. Range 2 500 km 1 350 NM(ISA, FL140, fuel reserve for 45 min.)Max. Endurance 10 h

Climb rateBoth Engines Operative (ISA, SL, MTOW) 9,0 m/s 1 773 fpmSingle Engine Operative (ISA, SL, MTOW) 2,0 m/s 394 fpm

Take-off Distance to 35 ft 590 m 1 936 ft(ISA, SL, MTOW)Landing Distance over 15 m (50 ft) 520 m 1 706 ft(ISA, SL, MTOW)

Capacity 19 PAX

Crew 2 pilots