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Cessna 340A
The FAA approved the 340A in November 1975. Two turbocharged Continental TSIO-520-N or TSIO-520-NB engines of 310 horsepower, with a critical altitude of 20,000 feet, turn propellers up to 76.5 inches across. The data sheet gives a maximum take-off weight of 5,990 lb, or 2,717 kg, and six seats, with other layouts in the manufacturer's equipment list. Its two wingtip tanks hold 100 US gallons of usable fuel, and optional wing tanks add more. Its ICAO code is C340. No acceptable source read gives its dimensions or speeds, so this page has no drawing.
- Seats
- About 6
- Engines
- Two piston engines on the wings: Continental TSIO-520-N or TSIO-520-NB
- Max takeoff weight
- 6,000 lb (2,717 kg)
Photos from members
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Specifications
| Fuel capacity | 100 US gal (379 L) |
|---|---|
| Status | Still flying with a few operators |
| Type codes | ICAO C340 |