Cessna 303 Crusader — Service Bulletins

This document is an Airworthiness Directive (AD) schedule for the Cessna T303 series aircraft, issued by the Civil Aviation Authority of New Zealand. It outlines mandatory compliance requirements for various inspections, modifications, and operational limitations to ensure the safety and airworthiness of the aircraft. The directives are applicable to all T303 aircraft and cover a range of issues from operating limitations to specific component inspections. Pilots and maintenance personnel must adhere to these directives to maintain compliance with safety regulations and ensure the aircraft operates within its certified limits.

• All T303 aircraft must comply with FAA AD 86-01-01R2 before further flight.
• NLG actuator attachment fittings must be inspected at 550 hours TTIS or within 50 hours, with modifications required by 31 July 1992.
• Auxiliary fuel pump wiring modifications are required within the next 100 hours TIS for specific serial numbers.
• Fuel inlet float valves must be tested within the next 200 hours TIS to prevent engine power loss.
• Severe icing conditions require specific procedures to be followed as outlined in the flight manual revision effective by 10 May 1998.
• Alternate static source selector valves must be inspected before further flight to ensure proper indications.
• Seat adjustment mechanisms must be inspected within the next 100 hours TIS to prevent inadvertent seat movement.