Aircraft Description
N5760D is a 1956 Piper PA-18-150, a single-engine reciprocating (piston) aircraft registered to Crow Jack R in Bethel, AK. This aircraft holds a multiple airworthiness certificate issued by the Federal Aviation Administration on August 16, 2018. The registration certificate was issued on November 7, 2024. The registration is set to expire on November 30, 2031. Powered by a Lycoming 0-320 SERIES engine producing 180 horsepower, N5760D is. The aircraft's Mode S transponder code is A7670F (hex), used for ADS-B identification and flight tracking. The FAA registry record for N5760D was last updated on November 7, 2024. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Piper M600 represents the pinnacle of single-engine turboprop aviation, combining advanced safety technology with exceptional performance capabilities. First entering production in 2016, this low-wing single-engine aircraft seats six passengers and features the revolutionary Garmin Autoland system, making it the first certified aircraft with autonomous landing capability. Powered by a 600-shaft-horsepower Pratt & Whitney Canada PT6A-42A turboprop engine, the M600 achieves a maximum operating speed of 250 knots with a range exceeding 1,000 nautical miles. The aircraft is manufactured by Piper Aircraft Corporation at their Vero Beach, Florida facility. AviatorDB tracks 48,285 Piper aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is M600.
AviatorDB has found no NTSB accident or incident reports involving N5760D. 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 (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Oct 8, 2004 | ANC05LA001 | Substantial | None | The inadequate and unapproved design of the main landing gear assembly by the manufacturer, which resulted in a failure of the main landing gear during landing, and structural damage to the airplane. A factor in the accident was the pilot's misjudged flare. |
| May 14, 1996 | ANC96LA071 | Substantial | None | the pilot's improper planning/decision, which resulted in his failure (or inability) to maintain clearance from trees after encountering gusty crosswind conditions. The wind condition and close proximity of trees were related factors. |
The inadequate and unapproved design of the main landing gear assembly by the manufacturer, which resulted in a failure of the main landing gear during landing, and structural damage to the airplane. A factor in the accident was the pilot's misjudged flare.
the pilot's improper planning/decision, which resulted in his failure (or inability) to maintain clearance from trees after encountering gusty crosswind conditions. The wind condition and close proximity of trees were related factors.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC