Cessna

Cessna 402A

The Cessna 402A, introduced in 1970 by the American manufacturer Cessna Aircraft Company, is a twin‑engine, pressurized light aircraft designed primarily for commuter and executive transport. Evolving from the earlier 401 models, the 402A incorporated a larger cabin, strengthened landing gear, and upgraded Lycoming O‑360 engines delivering 180 hp each, which improved climb performance and payload capacity. The aircraft’s conventional high‑wing layout provides excellent visibility and short‑field capability, while its all‑metal airframe offers durability and ease of maintenance. Typical seating for six to eight passengers, combined with a modest baggage compartment, made the 402A popular among regional airlines, air‑taxi operators, and private owners throughout the 1970s and 1980s. Its reliability, low operating costs, and ability to operate from austere airstrips contributed to the expansion of short‑haul air service in remote areas of North America and the Caribbean. Over 700 units were produced before production ceased in 1985, leaving a legacy of dependable commuter service and influencing the design of later Cessna twins such as the 404 Titan. Many 402A airframes remain in active service today, supported by a robust aftermarket parts network and enthusiast groups that preserve the type’s operational heritage.
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Production & History

Units Produced
129

Design & Classification

Primary Use
Manufacturer
Cessna
Wikidata ID
Q18552373