A one off designed specifically to enter and win the “Giro de Sicilia”, the Tour of Sicily, the P.55 Tornado was a two-seat sport competition aircraft, with a mid-mounted wing, retractable tricycle landing gear, a Lycoming O-320 flat-four engine, and side-by-side seating.
First flying in 1955, the only example (I-REGJ) winning the Tour of Sicily in 1956, to be lost in a crash on 13th June 1958.
Engine: 1 x Lycoming O-290-D2, 140 h.p. Span: 23′ 7.5″ Wing area: 86.1 sq.ft Length: 19′ 9.75″ Height: 6 ft 10.75 in Empty weight: 868 lb Loaded weight: 1367 lb Max speed: 211 mph Cruise: 186 mph Time to 3280ft: 3 min Max range: 497 mi
The Partenavia P-53 Aeroscooter was designed by Luigi Pascale, expressly for Mario de Bernardi, winner of the previous year’s d ‘Annunzio Trophy on a Partenavia P-55 Tornado.
The Aeroscooter is constructed of metal, and represents the minimum safe structure required to unite pilot, engine and flying surfaces. It fitted with a two-bladed rotor to reduce descent rate and stall in the event of an engine failure.
It flew in 1951.
It was built in collaboration with one Mario de Bernardi, who went on to build a two-seat version of the Aeroscooter; but he then died of a heart attack, and that was the end of it.
Engine: Ambrosini P-25, 16 kW (22 HP) Prop: two-blade wooden Wingspan 27 ft. 2 in / 8.28 m Wing area: 8.3 m2 (89 sq ft) Airfoil: NACA 63-series Length 16 ft. 9 in / 5.12 m Height 5 ft. 7 in / 1.70 m Empty weight: 180 kg / 397 lb MTOW: 280 kg / 617 lb Maximum speed: 93 m.p.h. / 150 km/h / 81 kn Cruising speed: 74 m.p.h. / 120 km/h / 65 kn Stalling speed: 37 m.p.h. / 32 kn / 60 km/h Service ceiling: 11,500 ft / 3,500 m Range: 500 km / 310 mi / 270 nmi Seats: 1
The Astore was followed by the Tigrotto was a low-wing cabin monoplane with a retractable tailwheel landing gear. It had two-seats side-by-side and was powered by an 85 hp (63 kW) Continental C85 engine.
The all-wood prototype, and only Tigrotto, registered I-CARB, first flew in 1953.
Engine: Continental C85-12F, 63 kW (85 hp) Wingspan: 29 ft 6.5 in Length: 19 ft 3.5 in Height: 5 ft 7 in Maximum speed: 235 km/h (146 mph, 127 kn) Cruise speed: 200 km/h (124 mph, 108 kn) Ceiling: 14,764 ft Range: 597 mi Empty weight: 948 lb Loaded weight: 1598 lb Crew: 1 (pilot) Capacity: 1 (passenger)
Luigi “Gino” Pascale and his brother Giovanni “Nino” Pascale of Naples, Italy, having been enthusiastic flying model aircraft makers, decided to work on full-scale aircraft. The first, built while the brothers were college students, was the “P.48 Astore (Goshawk)” — a two-seat aircraft, with the seats in tandem, featuring a high strut-braced wing, fixed taildragger landing gear, and a Continental O-170 / A65 flat-four air-cooled engine with 48 kW (65 HP).
The Astore had two seats in tandem and was powered by a 65 hp (48 kW) Continental A65 engine. The prototype and only Astore, registered I-NAPA, was built in a garage in Naples and first flew in 1952, piloted by Mario de Bernardi.
P-48-B Engine: 1 × Continental A65, 48 kW (65 hp) Wingspan: 26 ft 9.5 in Length: 20 ft 11.75 in Height: 5 ft 10.5 in Maximum speed: 185 km/h (115 mph, 100 kn) Cruise: 99 mph Time to 3280 ft: 5 min 50 sec Service ceiling: 10,827 ft Range: 342 mi Empty weight: 617 lb Loaded weight: 1036 lb Crew: one Capacity: one passenger
The P.57 was successful enough to consider a re-thought version of all-metal construction, with the “P.64 Fachiro III” taking to the air for the first time on 2 April 1965. After some rethinking of the prototype design, mostly to add a rear window and a cut-down rear fuselage, it went into production as the “P.64B Oscar B” — the “Oscar” effectively meaning “Type O” — to then be renamed the “P.64B Oscar 180”.
One of the very few water-based gliders, the Sea-Sky was designed and produced in the early 1960s by Partenavia of Naples. The Sea-Sky was a small single-seater with the pilot seated in a single-step speed boat-like wooden semimonocoque hull, with a small water rudder under the step, and the cantilever tail unit, of fabric covered metal construction, carried on a steel tube tail boom. The tailplane is a one-piece all-moving surface, with a tab on the port trailing edge. The braced parasol wing is of constant chord and is carried on an inverted vee steel tube structure at the rear of the hull, with steel tube bracing struts at the sides; the wing is a two-spar wooden structure, fabric-covered, with plain fabric-covered wooden ailerons and small fixed floats at the squared-off wing tips. The pilot sits in an open cockpit and has an overhanging control column and conventional rudder bars; the Sea-Sky is designed to be towed behind a motor boat. It is, however, capable of free flight and the wings and tailplane can be easily removed for transport and storage.
Span: 24ft 7in Length: 20 ft 0 in Height: 7 ft 3 in Wing area: 121.1 sqft Empty weight: 187 lb Max weight: 375 lb Min sinking speed: 4.90 ft/sec at 33.5 mph Best glide ratio: 9:1
The aircraft was designed by Professor Luigi Pascale, professor of aeronautics at Naples University, and his influence over the marketing department is there to see in the P68B’s very clean aerodynamic shape. Six place, powered by two 200hp Lycoming 10-360’s, with room for 400lbs of passenger baggage. The aircraft is designed for optimum aerodynamic efficiency, and this com¬bined with a simple but robust struc¬ture and its fixed undercarriage are factors that have endeared it to operators, who range from outback freight carrying outfits to third levels and executive users. The aerodynamic streamlining is demonstrated in the fuel economy; at optimum performance at 65 percent power (160 kts) the P68B can get through close on 900 miles at a fuel flow rate of some 15 gallons an hour. Entry to the aircraft is by a single door on the port side; simple enough for your average passenger but some¬what small to load any freight. A baggage door is also provided on the starboard side.
The P.68 Victor first flew in May 1970 with two 200-hp (149-kW) 10-360 engines as the prototype of a six/seven-seat lightplane. The type has an unusual appearance, with a racy fuselage and swept fin/rudder assembly married to fixed tricycle landing gear (with attractive speed fairings) and a straight wing and tailplane.
The first production P-68 Victor featured a six-inch fuselage stretch and higher gross weight among modifications developed as a result of field and customer-acceptance trials.
With the Victor established in production and further development, Partenavia then collaborated with a West German company, Sportavia-Putzer, in the development of a patrol and observation version.
In 1980, turbocharging was added for a slight increase in speed and a significant boost in service ceiling.
The Observer has a new forward fuselage incorpo¬rating a Plexiglas nose that offers forward and downward fields of vision comparable with those of a helicopter. The first Observer flew in West Germany during February 1976, and aircraft emerged from the Italian production line from July 1980. Since that time small but useful sales have been made to several police and para-military air arms. The Italian police use the type with the ATAL video surveillance system developed in France by Aérospatiale.
The P-68C features a lengthened nose, oleo-type nosewheel strut, an integral fuel tank in each wing and other refinements. Some featured a crew door.
Partenavia P68C
The certification RAI A-365 came from Registro Aeronautico Italiano for the P-68B, P-68C, and P-68C-TC.
Partenavia P68C
AD’s include “Extended safe life” kit 68-038 (Spar Caps replaced) and Max takeoff weight increase kit P68-051.
The Partenavia P.68R’s main wheels fold into the fuselage fairings with a speed gain averaging about eight knots. The version provided so little improvement over the standard that it never went into production.
Several versions of the P.68 are offered for military and paramilitary roles, including the P.68 Observer twin-piston-engined observation/surveillance aircraft, the AP.68TP-300 Spartacus for coastal patrol, troop transport, and medevac with two 240 hp Allison 250-B17C engines and underwing hard-points; and the AP.68TP-600 Viator, which is similar to the Spartacus but has a lengthened fuselage and a retractable undercarriage. The AP-68TP being jointly developed with Aeritalia.
Taneja Aerospace & Aviation Ltd in India undertook to set up a project for manufacture of P-68 aircrafts with three variants: P-68C (twin piston engine, non pressurised), P-68 C-TC (twin piston engine turbo Charged) and P-68 Observer (same as P-68 C-TC with forward and downward view equal to that of a helicopter). It has an empty weight of 1320 Kgs and payload of 764 Kgs, with a capacity to attain a maximum speed of 322 Kmph, 1550 ft./min rate of climb, landing run of 215 mtrs and an optimum cruising range of 2170 Kms at 12000 ft.
The aircraft was manufactured by Taneja Aerospace in India, while Aerocosmos, which held the production rights, was purchased by Air Samanta in 1998.
Vulcanair S.P.A of Naples, Italy, were manufacturers of Partenavia P68 aircraft in 2004. Vulcanair was converting one of its P68 Observer airframes to diesel power with an SMA engine. This was due to fly in September 2003 and if successful will be offered onto the light twin market.
More than 500 P68s had been built to 2003, of which some 35 are of the Observer vari¬ant for law enforcement and paramilitary use.
P-68B Observer Engines two 200-hp (149-kW) Lycoming IO- 360-A1B6 Wing span 39 ft 4.5 in / 12.00 m Length 30 ft 8 in / 9.35 m Height 11 ft 1.75 in / 3.40 m Wing area 200.2 sq ft / 18.60 sq.m Gross wt. 4,321 lb / 1,960 kg Empty wt. 2,822 lb / 1,280 kg Max Speed 174 kts / 200 mph / 322 km/h at sea level Max Cruise 165 kts Initial climb rate 1,160 / 488 m fpm Range 920 nm / 1,358 miles / 2,186 km Service ceiling 20,000 ft / 6,095 m Armament: none Seats 7
P.68 Observer 2
P-68C Engines: 2 x 200 hp Lycoming IO-360-A1B6 Seats: 6/7 Empty Wt: 2787 lbs Gross wt: 4387 lbs Useful load: 1600 lbs Max Cruise: 175 mph Max range: 900 sm
P-68TC Engines two 210-hp turbocharged Lycoming IO-360C-1A6D Gross wt. 4,387 lb Empty wt. 2,866 lb Fuel capacity 137-196 USG Max Speed 190 kts Max Cruise 175 kts Initial climb rate 1,130 fpm Range 1,040 nm Ceiling 27,000 ft Seats 7
AP-68TP Engines: 2 x 240 hp Allison 250 Seats: 7/8 Empty Wt: 3415 lbs Gross wt: 5787 lbs Useful load: 2372 lbs Max Cruise: 240 mph Max range: 820 sm
AP 68 TP 600 Viator Engines: 2 x Allison 250 B17C, 222 shp Length: 35.761 ft / 10.9 m Height: 11.811 ft / 3.6 m Wingspan: 39.37 ft / 12.0 m Wing area: 200.21 sq.ft / 18.6 sq.m Max take off weight: 6284.3 lb / 2850.0 kg Weight empty: 3616.2 lb / 1640.0 kg Max. weight carried: 2668.1 lb / 1210.0 kg Max. speed: 220 kts / 408 km/h Landing speed: 70 kts / 130 km/h Cruising speed: 170 kts / 315 km/h Initial climb rate: 1929.13 ft/min / 9.8 m/s Service ceiling: 25000 ft / 7620 m Wing loading: 31.37 lb/sq.ft / 153.0 kg/sq.m Range: 445 nm / 824 km Crew: 2 Payload: 9-12pax
Partenavia’s next effort was the “P.59 Jolly (Joker)”, a two-seater with fixed taildragger landing gear and a Continental O-200 flat-four engine with 75 kW (100 HP). The structure wooden/metal.
It was designed in response to a competition for a trainer for the Italian Aero Club in 1960 but the P.59 lost to the Aviamilano P.19 Scricciolo, and the P.59 remained a one-off.
Engine: Continental O-200, 75 kW / 100 hp Max speed: 105 kt
The P-57 Fachiro of 1957 was a touring aircraft of conventional configuration, with a high braced wing, four seats, forward-hinged doors on each side, fixed tricycle landing gear, of mixed steel tube / fabric construction.
First flown on 7 November 1958 with a 150 hp Lycoming O-320 engine, the Fachiro was Pascale’s first production machine, introduced in 1958 by Partenavia, which the Pascales had set up the year before to mass-produce their aircraft.
The P.57 The first machine, the “Fachiro I” was powered by a Lycoming O-320 with 112 kW (150 HP); it was followed by three “Fachiro II” machines with an O-360-B2A engine with 125 kW (168 HP).
Then 33 “Fachiro III” machines, with an O-320-A2A engine providing 134 kW (180 HP) and swept vertical tail surfaces.
The P.57 was successful enough to consider a re-thought version of all-metal construction, with the “P.64 Fachiro III” taking to the air for the first time on 2 April 1965.
Partenavia P-57 Fachiro III Engine: Lycoming O-320-A2A. 180 hp Wingspan: 30 ft 0 in Length: 21 ft 9 in Height: 7 ft 11 in Wing area: 144.2 sq.ft Empty weight: 1367 lb Loaded weight: 2315 lb Max speed: 152 mph at SL Max cruise: 135 mph at 3280 ft Econ cruise 65%: 127 mph ROC: 985 fpm Service ceiling: 13,780 ft Range: 560 mi at 127 mph
