This report details the type acceptance of the Cessna 210 Series aircraft, including ICAO type certificate details, type acceptance certificate, type data, and additional requirements in New Zealand.
The Type Acceptance Report (TAR 4/21B/25 – Revision 4) documents the New Zealand type‑acceptance of the Cessna 210 Series aircraft. It references the FAA Type Certificate No 3A21 and outlines the models and serial numbers that are eligible for an Airworthiness Certificate in the Standard Category.
The report includes ICAO type‑certificate details, a list of applicable New Zealand requirements, and extensive attachments such as photographs, three‑view drawings and copies of FAA certification data sheets. It also records the history of each model’s acceptance and any special conditions or limitations.
| Maximum Takeoff Weight (MCTOW) | 2900 lb (1315 kg) |
|---|---|
| Maximum Seats | 4 |
| Engine (base model) | Continental IO-470‑E |
| Maximum Takeoff Weight (T210R) | 4100 lb (1860 kg) |
The FAA Type Certificate number for the Cessna 210 is 3A21.
The latest revision (Revision 4) was issued on 6 July 2010.
The base Cessna 210 is equipped with a Continental IO‑470‑E engine.
The standard Cessna 210 provides seating for four occupants.