P68c Aircraft - Left engine
Serial number L-37075-51E
P68c Aircraft
Time since new 1, 107 hours 1, 107 hours
Partenavia P68c For Sale
TBO (March 2029) 2000 hours.
1, 107 hours 1, 107 hours
TBO 2,400 hours (March 2023) 2,400 hours
One (1) pilot + five (5) passengers in rear Club 4 configuration includes four (4) fully adjustable cabin seats with headrests and one (1) forward RH seat next to the pilot's seat. The fire stopped the Blue Leather Seats. Dark blue gray carpet. Cabin reading lights. Sound test. Pilot door option. Rear cabin door and rear cargo door. (Luggage division 1, 3m
Vulcanair P68c Victor
Cockpit seats have been removed during delivery of the aircraft so far, due to air inspection work. The Partavia P.68, now the Vulcanair P68, is a light aircraft designed by Luigi Pascale and originally built by the Italian Partavia. It made its first flight on May 25, 1970, was granted a type certificate on November 17, 1971, and was transferred to the Vulcan in 1998. The original six-seat high-wing monoplane is powered by twin piston engines and is used to transport easy and exercise. The P.68 Observer is a modification of the observation aircraft and has been developed into a 10/11-seat spread-twin turboprop product.
The type certificate for the P.68 Victor, a twin-piston, high-wing monoplane with fixed tricycle landing gear, was submitted on 22 January 1969.
The Partavia P.68 was designed as a six-seat light transport and trainer powered by two Lycoming IO-360 200 hp (149 kW) generators, it made its first flight on 25 May 1970 in Naples.
The type certificate for the 9.20 m (30.18 ft) long P.68 was issued by the Italian Civil Aviation Authority on 17 November 1971 for an MTOW of 1,860 kg (4,100 lb).
Vulcanair P68.tc Observer
After 300 hours of flight tests, production would begin in May 1972 at a new factory at Naples Capodichino Airport at a rate of three flights per month.
The prototype was built in Arzano, Italy, production began with 14 pre-production aircraft at new facilities in Casoria, Italy.
The longest P.68B Victor, 9.35 m (30.68 ft) was submitted on 18 October 1973 and awarded on 24 May 1974 for MTOW 1,960 kg (4,321 lb).
Both derived from the P.68B and 9.55 m (31.33 ft) long, the P.68R Victor has a recovery mechanism and was tested on 31 July 1978 while the P.68R has a .68C nose allowing a radar weather, larger fuel tanks and added weight, and was tested on 23 July 1979 with an MTOW of 1,990 kg (4,387 lb). P.68C-TC, certified on 29 April 1980, has Lycoming TIO-360-C1A6D turbocharged, 210 hp (157 kW) engines.
Partenavia P68 C Tc N747y
In 2021, the equipped price of the P.68C was $1.19 million, $1.22 million for the P.68R, and $1.31 million for the P.68C-TC.
The 9.43 m (30.94 t) P.68 Observer, a derivative of the P.68B with a transparent fuselage nose, modified systems and larger fuel tanks, was test-fired on 12 June 1980.
P.68TC Observer The 9.15 m (30.02 ft) long, turbocharged P.68 Observer was test-fired on 18 June 1985.
The P.68 "Observer 2" is 9.54 m (31.30 ft) longer than the P.68 "Observer", with increased weights, inverted wingtips and modified systems, and was test-fired on 30 November 1989 for 2084 kg (4594 lb) MTOW .
File:p68 Observer 2.jpg
The gear is a 10.89–11.27 m (35.73–36.97 ft) long, retractable AP68TP-600 "Viator", twin Allison 250-B17C 328 hp (245 kW) turboprops, with 2,850 kg ( 1 6 MT) was confirmed in October 6300 , 1986. In 2021, its equipped price was 3.154 million dollars.
The fixed gear 9.90 m (32.48 ft) long AP68TP-300 Spartacus was test-fired on 10 December 1983 with two Allison 250-B17C 328 kW (245 kW) and 2,600 kg (573 MTOW) turboprops.
Based in Casoria, Naples and already producing Partavia spare parts, Vulcanair (th Air Samanta) acquired the type certificate, aircraft spare parts and former manufacturing plant in Milan for 1.4 billion Le ($780,000) in April 1998.
The P.68 was involved in 86 accidents and incidents worldwide as reported in the Aviation Safety Network wiki database, including the loss of 58 shells.
Partenavia P68c Tc
September 11, 1983: A P.68C, N29561, performing an aerobatic demonstration, exploded in mid-flight at Plainview, Texas. The NTSB report found that an analysis of the video showed the plane overshot the runway, exceeding the Vne (Speed, Do Not Pass) speed by 27 mph at sea. The pilot executed a sharp nose change of about 8 degrees, which brought the aircraft's dynamic load factor to 8.3 Gs and caused both wings to fail on the main shoulder outside the two jackets, except for the aircraft, which he launched. turning, causing the rear whisker to turn on the path between his cabin and his hut. The plane fell 250 meters below just past the group of onlookers.
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