top of page
Our Fleet
Specifications
The Cherokee Piper 140 is powered by a 160-horsepower Lycoming O-320 engine. Its key specifications include a maximum takeoff weight of 2,200 lbs, an empty weight of about 1,201 lbs, and a fuel capacity of 50 US gallons. Performance estimates show a max speed of around 127 knots, a cruise speed of 119 knots, and a service ceiling of 15,800 ft.
Specifications
The Piper Cherokee 180 PA-28-180 is a four-seat, single-engine aircraft with an 180 hp Lycoming engine. Its typical performance includes a cruise speed of about 118-124 knots, a best rate of climb of 750 feet per minute, and a stall speed of 50 knots. Key dimensions are a wingspan of 30 feet and a length of 23 feet 5 inches, while its maximum takeoff weight is 2,400 pounds.
Specifications
The Cessna 310A is a twin-engine light aircraft powered by two Continental O-470-M engines, each producing 240 horsepower. Measuring 27 feet in length, with a 35-foot wingspan and a height of 10 feet 6 inches, the aircraft combines compact dimensions with impressive performance capabilities. With a gross weight of 4,600 pounds. The 310A boasts a service ceiling of 20,000 feet, providing excellent altitude performance for its class. As the first production model in Cessna’s renowned 310 series, it set the standard for future light twin designs, featuring sleek lines, tip tanks, and retractable tricycle landing gear that contributed to its efficiency, range, and handling characteristics.
bottom of page