Eclipse
EA500
#

Photo: Robert Deering 10/6/2008
Orange County Convention Center
Orlando, Florida

The Eclipse 500 is a small six-seat business jet aircraft manufactured by Eclipse Aviation.

Eclipse 500 became the first of a new class of Very Light Jet when it was delivered in late 2006. The aircraft is powered by two lightweight Pratt & Whitney Canada PW610F turbofan engines in aft fuselage-mounted nacelles.

Production of the Eclipse 500 was halted in mid-2008 due to lack of funding and the company entered Chapter 11 bankruptcy on 25 November 2008.  The company was then entered Chapter 7 liquidation on 24 February 2009.  After lengthy Chapter 7 procedure, Eclipse Aerospace was confirmed as the new owner of the assets of the former Eclipse Aviation on 20 August 2009 and opened for business on 1 September 2009. In October 2011 Eclipse Aerospace announced that they will put a new version of the aircraft, to be called the Eclipse 550, into production with deliveries starting in 2013.

The Eclipse 500 is based on the Williams V-Jet II, which was designed and built by Burt Rutan's Scaled Composites in 1997 for Williams International. It was intended to be used as a testbed and demonstrator for their new FJX-2 turbofan engine. The aircraft and engine debuted at the 1997 Oshkosh Airshow.

The V-Jet II had an all-composite structure with a forward-swept wing, a V-tail, each fin of which was mounted on the nacelle of one of the two engines. Williams had not intended to produce the aircraft, but it attracted a lot of attention, and Eclipse Aviation was founded in 1998 to further develop and produce the aircraft.

Founder and former Eclipse CEO Vern Raburn was one of the first business executives at Microsoft. Subsequently, Bill Gates became a major stake-holder in the Eclipse project.  The VLJ concept has been pursued by a number of manufacturers, and because the V-Jet II had been designed around one of the primary VLJ engines, Eclipse believed it was an ideal design to refine and market.

The airframe was significantly redesigned as an all-metal structure with a T-tail and straight wings. The main cabin shape is essentially all that was retained from the V-Jet II. It was recognized that for an aluminum structure to be cost effective, new manufacturing techniques would have to be developed. One of the primary processes used was friction stir welding, in which the skin and underlying aluminum structure are welded together rather than riveted, as traditional for aluminum aircraft. Anti-corrosion bonding techniques were also developed.

Besides materials processes, the general process of building the airframe was redesigned, with techniques taken from the automotive industry. Traditionally, aircraft structure is mounted in a jig, and the skin is riveted on to the outside of it. For the Eclipse 500, lessons were taken from composite airframe manufacturing, and the aluminum skin is first laid in a mold, and then the structure is built into it. The result is much more precise control of the aircraft's final shape, resulting in a cabin that is more robust and can be pressurized to a higher differential. In addition, the manufacturing techniques are designed so that one crew can assemble an airframe in a single shift. The complete interior is designed to be installed on a moving assembly line in 45 minutes.

Originally Eclipse selected a pair of Williams International EJ-22 engines (a production variant of the FJ22/FJX-2) for the Eclipse 500, but as the aircraft's weight increased, performance was not satisfactory. Pratt & Whitney Canada agreed to participate in the project, and modified the design of their PW615 engine, designating it the Pratt & Whitney Canada PW610F. The prototype Eclipse 500 first flew with the Williams engines in 2002.  The redesign to incorporate the new engines resulted in a significant delay to the development program. The first flight of the Eclipse 500 with the new engines occurred on December 31, 2004.

At the time of bankruptcy filing on 25 November 2008 Eclipse had delivered 259 EA500s. Serial number 260 had been paid for on the morning of the filing and in advance of the filing, but the company refused to release the aircraft to its owner. The bankruptcy judge noted the fate of this particular aircraft and ordered that the company maintain it and insure it until its final disposition is decided. In the final judgement the aircraft was ordered released within five days of the closing of the sale of the company, but the sale was not completed due to the incomplete Chapter 11 procedure and move to Chapter 7. The aircraft was finally released and was registered to its owner on 4 June 2009.

SPECIFICATIONS: PERFORMANCE:
Span:  37 ft 3 in (11.4 m) Maximum speed:  370 knots (425 mph, 685 km/h)
Length:  33 ft 1 in (10.1 m) Cruising speed: 
Height:  11 ft 0 in (3.4 m) Range:  1,125 nm (IFR with 45min NBAA reserve) (1,295 mi, 2,084 km)
Empty Weight:  3,550 lb (1,610 kg) Service ceiling:  41,000 ft (12,500 m)
Gross Weight:  5,950 lb (2,699 kg)  
Crew:  One or two pilots and up to 5 passengers
Engines:  2 × Pratt & Whitney Canada PW610F turbofan engines, 900 lbf (4 kN flat-rated to > ISA+10C) each
   
SOURCE:  Wikipedia