Aircraft Description
N752CF is a 1964 Piper PA-30, a twin-engine reciprocating (piston) aircraft registered to Jpg Aviation Services LLC in Phoenix, AZ. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on October 19, 1964. The registration certificate was issued on August 5, 2025. The registration is set to expire on August 31, 2032. Powered by a Lycoming IO-320 SERIES engine producing 150 horsepower, N752CF is. The aircraft's Mode S transponder code is AA21AF (hex), used for ADS-B identification and flight tracking. The FAA registry record for N752CF was last updated on August 5, 2025. 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 N752CF. 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 |
|---|---|---|---|---|
| Dec 26, 2002 | MIA03CA037 | Substantial | None | the pilot's improper start procedure which resulted in an unintentional engine start, and unoccupied aircraft collision with hangar structure. |
| Sep 23, 1990 | CHI90GA273 | MINR | None | EXCESSIVE PLAY IN THE LANDING GEAR EXTENSION LINKAGE. A FACTOR IN THE INCIDENT WAS UNRELIABILITY OF THE GEAR INDICATING SYSTEM. |
the pilot's improper start procedure which resulted in an unintentional engine start, and unoccupied aircraft collision with hangar structure.
EXCESSIVE PLAY IN THE LANDING GEAR EXTENSION LINKAGE. A FACTOR IN THE INCIDENT WAS UNRELIABILITY OF THE GEAR INDICATING SYSTEM.
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