CESSNA TURBO 210L — Type Certificate

This Type Acceptance Report provides an overview of the Cessna 210 Series, including the Cessna 210L model. It outlines the aircraft's certification details, including the FAA Type Certificate and the models covered under this certificate. The report confirms that all models listed under the FAA type certificate have been accepted for operation in New Zealand, subject to compliance with local operational requirements. The document serves as a reference for aircraft operators and aviation authorities, detailing the specifications, certification history, and operational compliance of the Cessna 210 Series.

• The Cessna 210L has a maximum takeoff weight (MCTOW) of 3800 lb (1723 kg).
• The aircraft is powered by a Continental IO-520-L engine.
• The Cessna 210 Series includes multiple models, all accepted for operation in New Zealand.
• The report confirms compliance with New Zealand operational requirements for the Cessna 210 Series.
• The first turbocharged version of the Cessna 210 was the T210F introduced in 1966.