Socata TBM
Explore the Socata TBM in side view and top view to compare its silhouette and proportions.
10.72 m35.2 ft
12.83 m42.1 ft
From Wikipedia
The SOCATA TBM is a family of high-performance single-engine turboprop business and utility light aircraft manufactured by Daher. It was originally collaboratively developed between the American Mooney Airplane Company and French light aircraft manufacturer SOCATA.
Summary of “SOCATA TBM” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Socata TBM by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/TBM9/), CC BY 4.0Specifications
- Length
- 10.72 m35.2 ft
- Wingspan
- 12.83 m42.1 ft
- Max take-off weight
- 3.35 t7,400 lb
- Cruise speed
- 467 km/h290 mph
- Max speed
- 611 km/h380 mph
- Range
- 3,304 km2,053 mi
- Ceiling
- 9,449 m31,000 ft
- Engines
- 1× P&WC PT6A-66D (turboprop)
- Power
- 850 hp
- First flight
- 1988
- In service
- 2014
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
