Piper PA-28RT Arrow IV Turbo — Other Documents

This Type Acceptance Report provides details on the Piper PA-28 Cherokee Series, specifically focusing on the Type Acceptance Certificate No. 99/21B/31 granted in New Zealand. The report validates the FAA Type Certificate number 2A13 and outlines the models covered, including the PA-28RT-201. It serves as a comprehensive reference for compliance with New Zealand operational requirements and airworthiness standards. The document is intended for aviation authorities, aircraft operators, and maintenance personnel involved with the Piper PA-28 series. It includes certification details, operational requirements, and a summary of models accepted under the type certificate.

• The Piper PA-28RT-201 has a Maximum Certified Takeoff Weight (MCTOW) of 2750 lb (1247 kg).
• The aircraft is powered by a Lycoming IO-360-B1E engine.
• Type Acceptance Certificate No. 99/21B/31 is valid for all models listed under FAA Type Certificate number 2A13.
• Compliance with New Zealand operational requirements is mandatory for type acceptance.
• The report includes specific operational and equipment requirements for IFR and VFR operations.