Aircraft › Vulcanair › Vulcanair P.68 › Vulcanair P.68C
Vulcanair P.68C
The Italian authority approved the P.68C in July 1979 and the FAA in July 1980. It is a P.68B with a nose changed for a weather radar, a hydraulic nose gear shock absorber, larger fuel tanks and a higher weight. Two Lycoming IO-360-A1B6 engines of 200 horsepower turn two-blade Hartzell propellers 72 inches across. The maximum take-off weight is 1,990 kg, the cabin has seven seats including the pilot's, and from serial number 210 the wing tanks hold 520 litres of usable fuel. It is 9.55 meters long and 3.40 meters high, with a wingspan of 12.00 meters.
- Seats
- About 7
- Engines
- Two piston engines on the wings: Lycoming IO-360-A1B6
- Max takeoff weight
- 4,400 lb (1,990 kg)
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Specifications
| Length | 31 ft 4 in (9.55 m) |
|---|---|
| Wingspan | 39 ft 4 in (12.00 m) |
| Height | 11 ft 2 in (3.40 m) |
| Fuselage width | 3 ft 11 in (1.20 m) |
| Fuel capacity | 140 US gal (520 L) |
| Status | Still flying with a few operators |
| Type codes | ICAO P68 |