Aircraft Description
N750AB is a 1991 Socata TBM 700, a single-engine turbo-prop aircraft registered to Npa Aviation LLC in Lafayette, LA. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on February 18, 1999. The registration certificate was issued on May 21, 2025. The registration is set to expire on May 31, 2032. Powered by a P&w PT6A SER engine producing 750 horsepower, N750AB is. The aircraft's Mode S transponder code is AA1A0B (hex), used for ADS-B identification and flight tracking. N750AB was last tracked by AviatorDB at coordinates 30.0790, -91.8936 on June 22, 2026. The FAA registry record for N750AB was last updated on May 21, 2025. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The SOCATA TBM-700A was the world's first pressurized single-engine turboprop to enter production, establishing an entirely new market segment in business aviation. First flown on July 14, 1988, it was a low-wing monoplane powered by a single Pratt & Whitney Canada PT6A-64 turboprop engine that could seat six to seven passengers. With a maximum cruise speed of 300 knots and a service ceiling exceeding 30,000 feet, the 37-foot aircraft delivered jet-like performance with turboprop efficiency. The aircraft was manufactured by SOCATA as part of a joint venture with Mooney Aircraft. AviatorDB tracks 1,070 Socata aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is TBM7.
AviatorDB has found no NTSB accident or incident reports involving N750AB. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| May 23, 2010 | WPR10LA260 | Substantial | None | A loss of engine power for reasons that could not be determined because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation. Contributing to the accident was the pilot's failure to obtain the proper touchdown point on the runway, which led to the runway overrun. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-06-15 01:32:20 UTC