Spectrum S-40 Freedom

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by BD2412 (talk | contribs) at 20:10, 23 June 2015 (Consensus at Template talk:Aviation lists#RfC: Should this navbox be removed from non-mentioned articles? using AWB). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

S-40 Freedom
Role Very Light Jet (VLJ), personal business jet
National origin United States
Manufacturer Spectrum Aeronautical
Developed into Spectrum S-33 Independence

The Spectrum S-40 Freedom is a business jet developed by Carlsbad, California based Spectrum Aeronautical, which has its development center located in Spanish Fork, Utah. The aircraft was first announced at the 2006 NBAA Conference in Orlando, Florida.

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 shall 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.

Specifications

Data from {name of first source}

General characteristics

  • Crew: one, pilot
  • Capacity: 7-9 passengers
  • 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)

Performance

  • 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

References

  1. ^ NBAA 2006: Spectrum enjoys a new Freedom Flightglobal, 17 October 2006
  2. ^ "Honda Engine a Step Closer with Plant Groundbreaking" Aviation International News, November 29, 2007
  3. ^ Kate Sarsfield: EBACE: New aircraft in the works, Flightglobal, 10 May 2011.

External links