CESSNA 402C

The Cessna 402C Utiliner/Businessliner is a twin-engine piston aircraft developed from the 402B, manufactured from 1979 to 1985, and notable for its versatility in cargo or high-density passenger configurations. Powered by two 325hp Continental TSIO-520-VB engines, it features a longer wingspan, new landing gear, and a higher maximum takeoff weight, making it a capable workhorse for regional airlines and cargo operations.

Key Features and Characteristics

• Engines: Equipped with two Continental TSIO-520-VB turbocharged piston engines, each producing 325 horsepower.
• Passenger & Cargo Capacity: The aircraft can be configured for up to 10 passengers or used in an all-cargo configuration, with removable seats for flexibility.
• Landing Gear: The 402C introduced improved scissor landing gear, derived from the larger Cessna 414.
• Wing Design: A longer wingspan replaced the tip tanks of earlier models, improving performance.
• Propeller: A propeller synchrophaser was added to reduce cabin noise and vibration.
• Production Period: The 402C was manufactured between 1979 and 1985.

Role in the 402 Series

• The Cessna 402C was the final and best-performing version in the 402 series.
• It served as a successor to the 401 and 402B models, which themselves evolved from the original 402 series.

Operational Use

• The 402C is commonly used by regional airlines and charter services for its ability to carry passengers and cargo.
• Its design allows for operations from small, remote airfields to larger international airport