Aircraft Description
N8888X is a 1989 Piper PA 46-350P, a single-engine reciprocating (piston) aircraft registered to 82 Saratoga LLC in Bryant, AR. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on September 28, 1989. The registration certificate was issued on May 11, 2022. The registration is set to expire on May 31, 2029. Powered by a Lycoming TI0-540 SER engine producing 310 horsepower, N8888X is. The aircraft's Mode S transponder code is AC3F13 (hex), used for ADS-B identification and flight tracking. N8888X was last tracked by AviatorDB at coordinates 34.6131, -92.4427 on June 25, 2026. The FAA registry record for N8888X was last updated on August 4, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Piper PA-46-310P Malibu pioneered affordable pressurized single-engine aviation when it first flew in August 1982, becoming only the third pressurized single-engine piston aircraft in civil aviation history. This low-wing, six-seat monoplane featured a Continental TSIO-520BE engine producing 310 horsepower and 5.5 psi cabin pressurization for high-altitude comfort. With a maximum cruise speed of 234 knots and service ceiling of 30,000 feet, the Malibu delivered cabin-class performance previously reserved for twin-engine aircraft. Manufactured by Piper Aircraft in Vero Beach, Florida, exactly 404 examples were built between 1983 and 1988. AviatorDB tracks 48,181 Piper aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is PA46.
AviatorDB has found no NTSB accident or incident reports involving N8888X. 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 |
|---|---|---|---|---|
| Dec 3, 1995 | MIA96LA055 | Substantial | None | THE FAILURE OF THE PILOT-IN-COMMAND TO MAINTAIN DIRECTIONAL CONTROL. CONTRIBUTING TO THE ACCIDENT WAS THE INADEQUATE AMOUNT OF RUDDER INPUT TO COMPENSATE FOR ENGINE TORQUE DURING TAKEOFF. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-07-01 01:32:20 UTC