Jump to content

Falco F8L

From Wikipedia, the free encyclopedia
(Redirected from Aviamilano Falco)
Falco F8L
1993 Sequoia Falco F8L
General information
TypeHomebuilt aircraft
National originItaly
ManufacturerAviamilano
Aeromere
Laverda
Sequoia Aircraft Company
Designer
StatusProduction completed (2014)
Number built90 (2011)[1]
History
First flight1955
VariantsSequoia 300, Sequoia 300, Sequoia Kodiak
Sequoia Falco takeoff
Sequoia Falco takeoff

The Falco F8L is an Italian-designed lightweight 2-seater aerobatic aircraft.[2]

Design and development

[edit]

The aircraft was designed by the renowned Italian designer Stelio Frati[3] in 1955, with the prototype, powered by a 90 hp (67 kW) Continental C-90 engine, flying for the first time on 15 June 1955.[4] The prototype was soon re-engined with a 135 hp (101 kW) Lycoming O-290-D2B, forming the basis for the initial production batch.[4] It was originally built in Italy by Aviamilano then Aeromere and later Laverda.[5]

The aircraft is single-engined, propeller driven and designed for private and general aviation use.[1][3] The Falco was sold in kit or plans form for amateur construction by the Sequoia Aircraft Company of Richmond, Virginia from the 1980s until its closure in 2014.[6]

Laverda-built Falco IV from Denmark attending a UK air rally in 1984

The aircraft is widely considered to be one of the best handling, strongest, and most aesthetically pleasing designs ever made available to home builders. Pilots sometimes refer to the Falco as "the Ferrari of the air."[3][7]

Performance includes a 175 knot cruise speed and full aerobatic capability, with an inverted fuel tank an optional item.[3]

The Falco F8L is constructed of spruce and typically Finnish birch plywood. The structure is built from laminated spruce bulkheads and the birch plywood is used for the skin.[8] The plywood is often softened with hot steam, formed over the various structures and glued in place. The aircraft is rated for 6g positive and 3g negative.

Reviewers Roy Beisswenger and Marino Boric described the design in a 2015 review as "a complex all-wooden construction in spruce and plywood and is therefore time-consuming to build. But the results in terms of weight and speed are remarkable., so much so that the Falco is considered a classic, with outstanding performance and handling."[9]

Variants

[edit]
F.8L Series I
Initial production model powered by 101 kW (135 hp) Lycoming engine. Ten built by Aviamilano starting in 1956.[10][5]
F.8L Series II
Improved model built by Aviamilano, with 112 kW (150 hp) engine.[10] Twenty built.[11][5]
F.8L Series III
(Also known as F.8L America) Modified version of Series II built by Aeromere in conformance with US airworthiness requirements.[10][5] 35 built by Aeromere.[12]
Super Falco Series IV
Similar to America, but with more powerful engine (160 hp (120 kW) Lycoming O-320-B3) and constant speed propeller. Built by Laverda.[10][13][5] Twenty built.[13]
Sequoia Falco
Similar to the production aircraft but re-designed for homebuilding from kits or plans,[5] by Alfred Scott of Sequoia Aircraft Company and David Thurston of Lake Buccaneer fame.

Specifications (Laverda Super Falco Series IV)

[edit]

Data from Jane's All The World's Aircraft 1965-66 [14]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.50 m (21 ft 4 in)
  • Wingspan: 8.00 m (26 ft 3 in)
  • Height: 2.27 m (7 ft 5 in)
  • Wing area: 10.0 m2 (108 sq ft)
  • Aspect ratio: 6.4:1
  • Airfoil: NACA 64213
  • Empty weight: 550 kg (1,213 lb)
  • Max takeoff weight: 820 kg (1,808 lb)
  • Fuel capacity: 120 L (32 US gal; 26 imp gal)
  • Powerplant: 1 × Lycoming O-320-B1A air-cooled flat-four engine, 120 kW (160 hp)
  • Propellers: 2-bladed Hartzell fixed-pitch propeller, 1.75 m (5 ft 9 in) diameter

Performance

  • Maximum speed: 325 km/h (202 mph, 175 kn) at sea level
  • Cruise speed: 250 km/h (160 mph, 130 kn) (econ. cruise)
  • Stall speed: 98 km/h (61 mph, 53 kn) (30% flaps)
  • Never exceed speed: 385 km/h (239 mph, 208 kn)
  • Range: 1,400 km (870 mi, 760 nmi)
  • Service ceiling: 6,000 m (19,700 ft)
  • Rate of climb: 5.00 m/s (984 ft/min)

See also

[edit]

Notes

[edit]
  1. ^ a b Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 69. Belvoir Publications. ISSN 0891-1851
  2. ^ Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 251. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1
  3. ^ a b c d Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 118. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  4. ^ a b Archive 1982, No. 3, p. 69
  5. ^ a b c d e f Munson, Kenneth; Taylor, John: Jane's Pocket Book Light Aircraft Second Edition, pages 130-131. Jane's Publishing Company, 1982. ISBN 0 7106 0195 6
  6. ^ "AeroSports Update: Falco Kit Producer Closes Its Doors". Aero-News Network. Jim Campbell. August 15, 2014. Retrieved October 19, 2018.
  7. ^ Tom Woodward (July 2018). "Falco: The Ferrari of the Air". Aero News Network.
  8. ^ Jack Cox (September 1991). "Grand Champion Falco". Sport Aviation.
  9. ^ Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 124. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  10. ^ a b c d Taylor 1965, p. 94
  11. ^ Taylor 1968, p. 108
  12. ^ Archive 1982, No. 3, p. 71
  13. ^ a b Archive 1982, No. 3, p. 74
  14. ^ Taylor 1965, pp. 94–95

References

[edit]
  • "Aircraft of European Civil Registers: 3 : The designs of Stelio Frati". Archive. No. 3. Air-Britain. 1982. pp. 67–74. ISSN 0262-4923.
  • Taylor, John W. R. (1965). Jane's All The World's Aircraft 1965-66. London: Samson Low, Marston.
  • Taylor, John W. R. (1968). Jane's All The World's Aircraft 1968-69. London: Samson Low, Marston & Company, Ltd.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
[edit]