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Cessna 310R
The FAA approved the 310R in August 1974, the last model of the 310 family; the turbocharged T310R was approved the same day. Two Continental IO-520-M or IO-520-MB engines of 285 horsepower turn propellers up to 76.5 inches across. The data sheet gives a maximum take-off weight of 5,500 lb, or 2,495 kg, and five seats as standard, with other layouts in the manufacturer's weight and balance data. Its two wingtip tanks hold 100 US gallons of usable fuel, and optional wing tanks add more. No acceptable source read gives its dimensions or speeds, so this page has no drawing.
- Seats
- About 5
- Engines
- Two piston engines on the wings: Continental IO-520-M or IO-520-MB
- Max takeoff weight
- 5,500 lb (2,495 kg)
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Specifications
| Fuel capacity | 100 US gal (379 L) |
|---|---|
| Status | In service |
| Type codes | ICAO C310 |