The Eclipse 400 ECJ, otherwise known as simply the Eclipse 400, is a civil utility aircraft that was designed by Swift Engineering & Eclipse Aviation. The developing aircraft was first revealed publicly during the 2007 AirVenture event. As a single-engine, very light jet, the Eclipse 400 was to compete with aircraft such as the Piper PA-47 PiperJet, Cirrus Vision SF50, Epic Victory, and Diamond D-Jet. The first flight of the Eclipse 400 was conducted in 2007, shortly before its public unveiling, and orders began only a year later in 2008. Due to financial difficulties during 2008, Eclipse Aviation filed for bankruptcy and the project was cancelled.
Model No :
Eclipse 400 Ecj
Manufacturer :
Eclipse Aviation
Country :
United States
Manufactured :
2009 to: Onward
ICAO :
NA
Avionics :
Avio NG avionics
Engine :
1 × Pratt Whitney PW615F turbofan
Power :
1,200 pound-force
Max Cruise Speed :
205 knots - 380 Km/h
Approach Speed :
NA
Travel Range :
NA
Fuel Economy :
14.6 nautical mile / gallon - 7.143 kilometres / litre
Service Ceiling :
NA
Rate of Climb :
NA
Take Off Distance :
623 metre - 2,043.94 feet
Landing Distance :
640 metre - 2,099.71 feet
Max Tak eOff Weight :
10,538 Kg - 23,232 lbs
Max Payload :
839 Kg - 1,850 lbs
Fuel Tank Capacity :
NA
Baggage Volume :
1 m3 / 35 ft3
Seats Economy/General Class :
4 seats
Seats Business Class :
0
Seats First Class :
0
Cabin Height :
NA
Cabin Width :
NA
Cabin Length :
NA
Exterior Length :
NA
Tail Height :
NA
Fuselage Diameter :
NA
Wing Span Rotor Diameter :
NA
With a single
Pratt & Whitney PW615F turbofan engine producing 1,200 pound-force, the Eclipse 400 ECJ would be capable of reaching a maximum cruise speed of 205 knots. The range of the aircraft was stated to be 1,445 miles, and it could perform with an average fuel economy of 14.6 nautical miles per gallon. For flight, one to two pilots would be required for operation, meanwhile upwards of three passengers could be situated across available seating. With a combination of personnel and cargo, the Eclipse 400 ECJ would be capable of operating with a maximum payload of 1,850 pounds.
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