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Fact Files  >  ATR42-300

ATR - ATR42-300
Category: Multiengine Turboprop > 12,500 lbs.
Years Aircraft Manufactured: 1985-1996
Printer friendy version
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Aerospatiale and Aeritalia (now Alenia) established Avions de Transport Regional as a Groupement d'Intéret Economique under French law to develop a family of regional airliners. The ATR-42 was the consortium's first aircraft and was launched in October 1981.The initial ATR-42-300 was the standard production version of the ATR-42 family until 1996 and features greater payload range and a higher takeoff weight than the prototypes. The similar ATR-42-320 (also withdrawn in 1996) differed in having the more powerful PW-121 engines for better hot and high performance, while the ATR-42 Cargo is a quick change freight/passenger version of the 42-300. The ATR-42-500 is the first significantly improved version of the aircraft and features a revised interior, more powerful PW-127Es for a substantially increased cruising speed (565km/h/305kt) driving six blade propellers, a 1850km (1000nm) maximum range, the EFIS cockpit, elevators and rudders of the stretched ATR-72 (described separately), plus new brakes and landing gear and strengthened wing and fuselage for higher weights. The first ATR-42-500 delivery was in October 1995.

Seating (normal) 42 Max Takeoff (lbs) 36,817
Seating (maximum) 50 Certified Ceiling (ft) 25,000
Engines P&WC PW120 To (Sealevel, ISA Temp) (ft) 3,576
Output lbs ea. Flat Rating 1800 shp Landing Distance (ft) 3,380
Maximum Mach No. 0.55 Max Range (fuel) (nm) 2,420
High Speed Cruise (Kts) 265 Max Range (payload) (nm) 1,050
Flight Time 300nm - Flight Time 1000nm -
Flight Time 600nm -    
External Internal
Length (ft) 74.40 Length (ft) 45.50
Height (ft) 24.90 Height (ft) 6.30
Span (ft) 80.70 Width: Max floor (ft) 8.50
 

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