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blended in with a curved leading edge. The front section included the enclosed cabin with two pairs of seats. Dual controls were fitted. There were wide doors on either side into the cabin; the baggage compartment behind it could be accessed from inside the cabin or by a separate external hatch. The only Airone completed carried its fuel in a tank ahead of the cabin, though production aircraft would have used wingtip tanks instead.
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structure and that of the conventional tail unit was similar, though the rudder and elevators were fabric covered. The fuselage was built in two sections, bolted together behind the wing trailing edge. The rear section tapered towards the tail, where the tailplane was fitted on its top and the fin
105:, who was responsible for several fast light wooden aircraft powered by either piston or turbine engines. The Airone (Heron in English) was a low-winged, twin piston engine driven, four seater. It was intended as a general light four seater for private or executive use, or as an
148:
inverted inline engines with variable pitch airscrews, though there were other possible engine choices in the 90 to 140 hp (67 to 104 kW) range. In
February 1958 there was a report that
152:
would produce the Airone powered with unspecified 150 hp (112 kW) engines in place of the
Walters. As with other proposals to produce the Airone, this too came to nothing.
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engines of 90 hp (67 kW) each, driving fixed pitch propellers. Production aircraft would have been powered by two 105 hp (78 kW)
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was a low-wing, twin-engined, wooden, four seat civil aircraft built in Italy in the 1950s. Production was considered but only one was completed.
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140:(knee action) main gear legs mounted below the engines. The prototype was powered by two flat 4-cylinder
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The Airone's wings were built around a one piece single wooden spar and clad with stress bearing
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The F in the designation of the
Pasotti built F.6 Airone stood for its designer,
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334:. London: Jane's All the World's Aircraft Publishing Co. Ltd. p. 178.
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4-cylinder inverted inline air cooled, 78 kW (105 hp) each
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Reference 3 states that the prototype's tanks were in the wings.
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132:The Airone had a conventional retractable
380:. No. 21 February 1958. p. 260.
250:1,200 km (750 mi, 650 nmi)
244:260 km/h (160 mph, 140 kn)
238:300 km/h (190 mph, 160 kn)
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360:. No. 15 July 1956. pp. 80–1.
352:"Flight-testing the Pasotti Airone F.6"
332:Jane's All the World's Aircraft 1956-57
294:
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223:2-bladed variable pitch and featherable
195:14.7 m (158 sq ft) gross
163:Jane's All the Worlds Aircraft 1956-57
26:
7:
613:Twin piston-engined tractor aircraft
603:1950s Italian civil utility aircraft
156:Specifications (production aircraft)
189:10.25 m (33 ft 8 in)
262:5.97 m/s (1,176 ft/min)
183:7.25 m (23 ft 9 in)
25:
580:
568:
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1:
256:5,500 m (18,000 ft)
207:1,400 kg (3,086 lb)
63:Legname Pasotti SpA, Brescia
302:James Gilbert (July 1978).
201:850 kg (1,874 lb)
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330:Bridgman, Leonard (1956).
426:
29:
372:"Club and Gliding News"
168:General characteristics
134:tricycle undercarriage
97:Design and development
418:Aircraft designed by
118:differential ailerons
122:trailing edge flaps
531:F.1300 Jet Squalus
91:Pasotti F.6 Airone
608:Low-wing aircraft
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536:F.3500 Sparviero
350:Rosaspina, Vico.
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16:(Redirected from
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116:. They carried
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42:Type of aircraft
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304:"Stelio Frati"
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260:Rate of climb:
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471:F.15 Picchio
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307:. Retrieved
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103:Stelio Frati
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79:Number built
72:Stelio Frati
516:F.400 Cobra
476:F.20 Pegaso
466:F.14 Nibbio
436:F.4 Rondone
229:Performance
221:Propellers:
211:Powerplant:
597:Categories
446:F.6 Airone
441:F.5 Trento
309:2010-07-31
289:References
193:Wing area:
575:Companies
456:F.8 Falco
187:Wingspan:
175:Capacity:
161:Data from
136:with its
68:Designer
587:Aviation
506:Airtruck
150:Aeromere
126:fuselage
549:Portals
181:Length:
114:plywood
30:Airone
526:F.1000
377:Flight
357:Flight
248:Range:
124:. The
563:Italy
511:F.200
501:F.260
496:F.250
269:Notes
54:Italy
35:Role
491:F.30
213:2 ×
120:and
89:The
599::
374:.
354:.
340:^
318:^
109:.
83:1
551::
411:e
404:t
397:v
312:.
177:4
20:)
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