Piper Malibu

Engine
Continental TSIO-520-BE
Horsepower: 310

Weights
Maximum Takeoff Weight: 4,100 lbs
Standard Useful Load: 1,640 lbs

Fuel Capacity
Usable: 120 gal

Cruising Speed
Maximum Cruise Power: 203 ktas

Range with 45 Minute Reserve
1,261 nm
 
Development of the PA-46 began in the late 1970's to compete against Cessna's P210 Centurion.  The first production variant of the PA-46 flew in 1982 and FAA Certification was received in 1983.  The FAA designation of the Malibu is PA-46-310P.