1966 Piper Twin Comanche PA-30B
Description
The Piper Twin Comanche PA-30B is a twin-engined light aircraft built by Piper Aircraft. It was produced from 1965 to 1975 and is powered by two Lycoming IO-360-B1B engines. The aircraft has a maximum speed of 195mph and a range of 1,000 miles. It has a gross weight of 4,400 pounds and can accommodate up to six passengers.
Features
- J.W. Miller Full Conversion, 200HP
- Clear and clean title
- Full & complete log books and Miller build sheet
- AFTT: 9,200
- LE Lycoming IO-360-C1C
- LE 1078 SMOH
- LE serial: L-23018-51A
- RE Lycoming IO-360-C1C
- RE 1455 SMOH
- RE serial: L-23019-51A
- Last annual 07/11/2011
- LE has a cracked block
- Props: Hartzell model HC-C2YK-2CUF
- LE Prop overhaul time: 889.7
- LE Prop total time: 6240.7
- RE prop overhaul time: 889.7
- RE prop total time: 6240.7
- Fuel: 158 Gallons total, 8 fuel tanks (4 standard, 4 STC)
- Range: 1899nm @ 65% power @ 18.3 GPH
- Max take off weight: 3780lb
- Basic empty weight: 2573lb
- Useful load: 1207lb
- Seats: 6
- FIKI: Full de-ice (windshield, props, wings, tail, rudder)
Location
