MS 760 Paris
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The Morane-Saulnier MS.760 Paris is a French four-seat jet trainer and liaison aircraft designed and manufactured by Morane-Saulnier. The Paris was based upon an earlier proposed trainer aircraft, the MS.755 Fleuret. Following the failure of the French Air Force to select the Fleuret, Morane-Saulnier opted to develop the design into a liaison aircraft and compact business jet. The primary difference between the two designs was the altered seating arrangement, the original side-by-side seating two-seat cockpit was modified to allow for the addition of another row of two seats to accommodate passengers. The Paris retained the flight characteristics of the Fleuret along with the option for installing armaments, which maintained its potential for use as a military trainer as well for civil aviation. On 29 July 1954, the prototype performed the type's maiden flight. The primary operators of the Paris were the French air services, who used the type for liaison purposes between 1959 and 1997. During 1955, Morane-Saulnier and American aviation company Beech Aircraft formed a joint venture to market the Paris as the first business jet on the North American market, but the venture was dissolved a few years later due to a lack of customer interest. During the 1960s more advanced variants were developed such as the MS.760B Paris II and the six-seat MS.760C Paris III; the latter would not enter production however. While four-seat propeller planes are commonplace, jet-powered aircraft with this seating arrangement, such as the Grumman EA-6B Prowler combat aircraft, have remained comparatively rare.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Morane-Saulnier
- Category
- Trainers
- Country of origin
- France
- First flight
- 1954-07-29
- Length
- 10.05 m
- Wingspan
- 10.15 m
Specifications
- Cruise speed
- 310 kt
- Max speed
- 350 kt
- Range
- 810 nm
- Service ceiling
- 33,000 ft
- Rate of climb
- 2,264 ft/min
- Max takeoff weight
- 7,650 lb
- Empty weight
- 4,288 lb
- Fuel capacity
- 245 US gal
- Powerplant
- 2 × Turboméca Marboré II turbojets
- Engines
- 2
- Seats
- 4
- Length
- 33 ft
- Wingspan
- 33 ft
- Height
- 8 ft
- Number built
- 219
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.