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The Mooney 301 was a prototype aircraft created by American manufacturer Mooney Aircraft Company in 1983. It was a low-wing single-engine six-place monoplane with retractable gear and a pressurized fuselage. The Mooney 301 design team was led by Roy LoPresti. It was an attempt to create an alternate to pressurized single-engine airplanes being introduced by Beechcraft Cessna and Piper Aircraft. Only one prototype was constructed.

The turboprop Mooney 301 eventually became the TBM700 and was produced by Socata Aircraft.1

Made by Mooney Aviation Company.

Empty Weight Lb
2548
Wing Area Sqm
14
Eng 1 Type
Lycoming O-540
Max Speed Mph
301
Cruise Speed Kmh
259
Ceiling Ft
25000
Cruise Speed Mph
417
Eng 1 Kw
269
Span In
9
Gross Weight Lb
4000
Capacity
5
Number Built
1
Crew
1
Climb Rate Ftmin
1450
Empty Weight Kg
1156
Gross Weight Kg
1814
Height In
10
Range Km
1850
Climb Rate Ms
7
Manufacturer
Mooney Aviation Company
Range Miles
1149
First Flight
7
Max Speed Kmh
484
Height Ft
9
Span Ft
36
National Origin
United States
Wing Area Sqft
150
Met Or Eng
eng
Span M
11
Length Ft
29
Height M
3
Ceiling M
7620
Eng 1 Hp
360
Eng 1 Number
1
Length In
9
Length M
9
Category
Low wing aircraft
Mooney aircraft
Propeller aircraft
Single-engine aircraft
United States civil utility aircraft 1950-1959

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