Cessna
Cessna 310J
The Cessna 310J, introduced by the American manufacturer Cessna Aircraft Company in 1961, is the fifth major variant of the storied Model 310 twin‑engine line. Building on the success of earlier 310B through 310F models, the 310J incorporated a more powerful 260‑hp Continental IO‑520‑B engines, a strengthened all‑metal airframe, and a redesigned, aerodynamically cleaner nose and cowl. The aircraft features a retractable tricycle landing gear, a spacious 2‑plus‑2 cabin with side‑by‑side seating, and a maximum cruise speed of roughly 190 knots (219 mph) at 12 000 ft. Its fuel capacity of 124 gallons gives a range of about 1,200 nautical miles, making it popular for business travel, air‑taxi service, and flight training.
The 310J’s significance lies in its balance of performance, reliability, and relatively low operating costs, which helped cement the twin‑engine light aircraft market in the 1960s. Over 400 units were built before production ended in 1964, and many remain active today, praised for their handling and versatility. The model also served as a testbed for later Cessna innovations, influencing the development of the 310R and the modern 340/350 series that dominate corporate aviation.
The 310J’s significance lies in its balance of performance, reliability, and relatively low operating costs, which helped cement the twin‑engine light aircraft market in the 1960s. Over 400 units were built before production ended in 1964, and many remain active today, praised for their handling and versatility. The model also served as a testbed for later Cessna innovations, influencing the development of the 310R and the modern 340/350 series that dominate corporate aviation.
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Classification
Production & History
- Units Produced
- 200
Design & Classification
- Primary Use
- Manufacturer
- Cessna
- Engine
- IO-470-U
- Wikidata ID
- Q19799809