1959 Beechcraft D95A Travel Air
Description
The Beechcraft D95A Travel Air is a light twin-engine aircraft manufactured by the Beech Aircraft Corporation. It is a 6-seat, low-wing aircraft with retractable landing gear, first introduced in 1959. The aircraft is powered by two Lycoming IO-360-A1A engines and features a range of up to 981 nautical miles, a maximum cruise speed of 183 knots (214 mph/344 km/h), and a service ceiling of 17,000 feet. The aircraft is capable of carrying up to 1,475 lbs of useful load and has a maximum take-off weight of 4,100 lbs. It is typically used for corporate and private transport, air taxi, and air charter operations.
Features
- Total Time: 5877
- Engines / Mods / Prop
- Lyc 360A1A
- L/1126 SMOH 2000TBO
- R/669 SMOH 2000TBO
- RAY JAY TURBOS
- Prop accumulators
- Avionics / Equipment
- GNS430W
- G1106 VOR HEAD
- MD41-1488W ANNUCIATOR
- GMA340 AUDIO PANEL
- GTX 330 ES
- ACKA30.9 encoder alt
- STEC 60 PPS AP
- CENTRY IIb AP
- COLLINS DME TCR 451
- INSIGHT STRIKE FINDER
- MX 170C glide slope.
Location
1959 Beechcraft D95A Travel Air 0 reviews
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