1978 Cessna 310R
Description
The Cessna 310R is a light twin-engined six-seat monoplane produced by Cessna in the 1970s. It is powered by two Continental IO-520-CB 285hp engines, and features a retractable tricycle landing gear. The 310R is the stretched version of the Cessna 310Q, and is capable of a maximum cruise speed of 215 mph. It has a range of over 1,000 miles, and can reach a maximum altitude of 25,000 feet. The 310R has an operating empty weight of 3,343 lbs, and a maximum takeoff weight of 5,400 lbs. It is well-suited for business and recreational use, and is considered a reliable and safe aircraft.
Features
- Total Time: 13241
- Left Engine
- Annual 11/22/2021
- Continental IO-520-MIB
- S/N: 277228-R
- TBO 1700
- Electroair EIS-61000 Electronic Ignition Kit
- Total Time: 9640
- SMOH: 850
- Compression: 76, 62, 64, 60, 63, 79/80
- Right Engine
- S/N: 270614-R
- TBO 1700
- Electroair EIS-61000 Electronic Ignition Kit
- Total Time: 11392
- SMOH: 1561
- Compression: 76, 66, 78, 58, 66, 67/80
- Left Prop
- McCauley 3AF32C87-NR
- S/N: 773458
- SMOH: 478
- Right Prop
- S/N: 703899
- SMOH: 1561
- PS Engineering PMA 8000 Audio Panel
- Garmin MX-20 Multi-Function Display
- Garmin GNS-480 GPS/Nav/Com
- Garmin GTX-330 ES (ADS-B Out)
- Garmin Sl-30 Nav/Com
- Mid-Continent Course Deviation Indicator
- 400B Auto Pilot
- Collins ADF-650
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