Spectrum S-40 Freedom
S-40 Freedom | |
---|---|
Role | Very light jet (VLJ), personal business jet |
National origin | United States |
Manufacturer | Spectrum Aeronautical |
Developed from | Spectrum S-33 Independence |
The Spectrum S-40 Freedom was a business jet developed by Spectrum Aeronautical. The aircraft was first announced at the 2006 NBAA Conference in Orlando, Florida.
Design and development
The S-40 is expected to be classified as a very light jet, albeit it is planned to feature a cabin comparable to the Lear 60, Hawker 800, Phenom 300 and the Citation XLS, at a Maximum Take-Off Weight of less than 10,000 lb (4,500 kg).[1]
It will be built using a graphite-epoxy construction process that makes the aircraft one third the weight of comparably sized aluminium airplanes. The aircraft is designed to cruise at 45,000 ft (14,000 m) at speeds up to 435 knots (Mach 0.76) and fly as far as 4170 km - while consuming about 40% less fuel than conventionally built planes - using two GE Honda HF120 engines.[2]
The retail sales price of the aircraft is supposed to be US-$6.8 million. In May 2011 Spectrum president Austin Blue is quoted: "We are still trying to get the programmes advancing, but it is not easy" The aircraft is to be released about 12 months before the smaller Spectrum S-33 Independence.[3] FAA and JAA Type Certifications of the S-40 Freedom were initially estimated for 2010.
In 2016, the company stated that it was looking for funding to produce the S-40 in Mexico.[4]
Specifications
General characteristics
- Crew: one, pilot
- Capacity: 7-9 passengers
- Length: 53 ft 10 in (16.4 m)
- Wingspan: 45 ft 6 in (13.9 m)
- Height: 11 ft 8 in (3.6 m)
- Max takeoff weight: 9,550 lb (4,336 kg)
- Interior Height: 6 ft 0 in (1.8 m)
- Interior Width: 6 ft 0 in (1.8 m)
- Interior Length (Cabin Divider to PB): 16 ft 0 in (4.9 m)
- Interior Length (Total; PB to PB): 21 ft 2 in (6.45 m)
- Powerplant: 2 × GE Honda HF120 turbofan engines, 2,095 lbf (9.32 kN) thrust each
Performance
- Maximum speed: 440 kn (506 mph, 815 km/h)
- Range: 2,200 nmi (2,513 mi, 4,074 km)
- Service ceiling: 45,000 ft (13,725 m)
- Specific Range at LRC (nm/lbs. of fuel): 0.81 nmi (1.50 km)
- Time Between Engine Overhauls: 5,000 hours
- Time to FL450 (MTOW): Less than 20 minutes
See also
Related lists
References
- ^ NBAA 2006: Spectrum enjoys a new Freedom Flightglobal, 17 October 2006
- ^ "Honda Engine a Step Closer with Plant Groundbreaking"[permanent dead link] Aviation International News, November 29, 2007
- ^ Kate Sarsfield: EBACE: New aircraft in the works, Flightglobal, 10 May 2011.
- ^ "Spectrum to build S-40 business jet in Mexico".
External links
- All articles with dead external links
- Articles with dead external links from May 2018
- Articles with permanently dead external links
- Articles with short description
- Aircraft specs templates using more general parameter
- Aircraft specs templates using more performance parameter
- Spectrum aircraft
- Abandoned civil aircraft projects
- Very light jets