Commercial Aircraft Directory - Aircraft Specification

ATR - 42-320

The aircraft was designed as a high wing regional airliner and cargo transport that could quickly be fitted for other requirements such as VIP essentially a replacement for older types such as the early Fokkers and Convairs. Production of the first generation aircraft occurred between 1985 and 1996. The new generation variant the -500 is now the standard production model. The first flight was made on 16th of August 1984 and after successful trials went into active service with AIR LITTORAL in March 1986. The next generation models of the ATR 42 received certification on July 28th 1995 before entering service with AIR DOLOMITI. Construction materials included light alloys and greater use of composites for the wing roots. The next generation -500 variant utilises noise absorbing Carbon/Nomex and Kevlar/Nomex construction including 7 stiffened forward fuselage frames and active vibration absorbers. A 40% increase on the overhead baggage space and an all new air conditioning system. To Date Models are: ATR42-300, 300C (Cargo model, notably an additional large door version was added to the family in 2000), 300F (Military Freighter version), 320, and the next generation -500 which included improvements noted above and with 6 rather than 4 bladed propellers featuring electronic control, a composite tail and new undercarriage wheels and brakes.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: 16 Aug 1984  
Certification date: 10 1985  

PRINCIPAL DIMENSIONS

Fuselage width: 2.87 m 
Fuselage height: 7.59 m 
Fuselage length: 22.67 m 
Cabin length: 14.72 m 
Cabin width: 2.57 m 
Cabin height: 1.91 m 
Cabin volume: 58 m3 
Hold volume: 11 m3 

WEIGHTS

Empty operating: 10,285 kg 
Max zero fuel: 15,200 kg 
MTOW: 16,700 kg 
MLW: 16,400 kg 
Standard fuel capacity: 5,736 kg 
Max fuel capacity: 5,736 kg 

SPEEDS

Normal cruise:  
Max cruise: 490 km/h 

PERFORMANCE

Long Range Cruise alt:  
Max ceiling: 7,620 m 
Take off field length: 1,040 m 
Landing field length: 1,034 m 
Max Payload Range: 1,167 m 
Range notes:  
Max passengers: 50  
Typical passengers: 42  

POWERPLANT

Category: Turboprop  
Manufacturer: Pratt & Whitney Canada  
Model/Submodel: PW121  
Thrust: 0 kN  

MAINTENANCE PROVIDERS

Air Madagascar
Airlinair
Mountain Air Cargo
Precisionair
Santa Barbara Airlines
Solenta Aviation
Top Fly SL
Trans Maldivian Airways
White Eagle Aviation