CESSNA CONQUEST II — Airworthiness Directives
1 airworthiness directives reference for the CESSNA CONQUEST II.
This document is an Airworthiness Directive (AD) schedule specifically for the Cessna 441 series aircraft, issued by the CAA of New Zealand on March 27, 2014. It outlines mandatory compliance requirements for all Cessna 441 aircraft, detailing various FAA Airworthiness Directives that must be adhered to for safety and regulatory compliance. The document serves as a critical reference for maintaining airworthiness and ensuring that all necessary inspections and modifications are performed on the aircraft. It includes specific directives related to fuel boost pump wiring, anti-icing systems, and other essential components, emphasizing the importance of timely compliance to maintain operational safety.
- All Cessna 441 aircraft must comply with FAA Airworthiness Directives as listed in the document.
- Inspection of fuel boost pump wiring is required within 25 hours TIS or 60 days, whichever comes first.
- If wiring is found damaged, it must be replaced before further flight.
- Installation of improved design parts can terminate repetitive inspection requirements for the fuel boost pump wiring.
- Compliance with these directives is necessary for the issuance of a New Zealand Certificate of Airworthiness.