CESSNA 501 Citation 1SP G600 — Airworthiness Directives

This document is an Airworthiness Directive (AD) schedule specifically for the Cessna 501 series aircraft, issued by the Civil Aviation Authority of New Zealand (CAA) on September 24, 2015. It outlines compliance requirements for various FAA Airworthiness Directives applicable to the Cessna 501 aircraft. The document serves as a reference for ensuring that the aircraft meets safety and operational standards as mandated by the FAA. It includes details on inspections, modifications, and compliance timelines necessary for maintaining airworthiness. The schedule will be reactivated once a Cessna 501 aircraft is registered in New Zealand, at which point all applicable ADs will be enforced.

• The document is specifically for Cessna 501 aircraft, not the Cessna 550 Citation II.
• Compliance with FAA ADs is required before issuing a New Zealand Certificate of Airworthiness.
• Upper and lower spar caps must be inspected for cracks at wing station 37.0, with specific intervals for inspections based on findings.
• Brake assembly stator disks must be inspected to prevent loss of braking performance, with strict compliance timelines.
• Fire extinguisher wiring must be inspected and reworked to ensure proper functionality.