Skip to main content

CESSNA 310Q — Airworthiness Directives

2 airworthiness directives references for the CESSNA 310Q.

Overview
SCHEDULE OF AIRWORTHINESS DIRECTIVES · 1995

This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority of Australia, specifically addressing the Cessna 310 series aircraft. It outlines mandatory inspection requirements for the main landing gear and wing structure to ensure safety and compliance with aviation regulations. The directive is applicable to all models of the Cessna 310 and includes specific instructions for inspections and compliance timelines. The background section highlights previous incidents of structural cracking, emphasizing the importance of adherence to the directive to prevent potential failures in the aircraft's landing gear and wing structure.

  • Inspect main landing gear side brace upper support attach bolts for correct torque.
  • Conduct visual inspections of the main landing gear wheel well ribs and wing upper surface skin.
  • Initial inspections due before 100 hours time in service after July 20, 1995.
  • Re-inspect at intervals not to exceed 100 hours time in service.
  • Installation of Cessna Service Kit SK414-8E cancels the requirement of this directive.
2 documents
CESSNA 310Q — Airworthiness Directives FAQ
How many Airworthiness Directives documents does Sprinkle have for the CESSNA 310Q?

Sprinkle has 2 Airworthiness Directives documents on file for the CESSNA 310Q.

What year is the CESSNA 310Q Airworthiness Directives?

The CESSNA 310Q Airworthiness Directives on file is dated 1995.

How many pages is the CESSNA 310Q Airworthiness Directives?

The CESSNA 310Q Airworthiness Directives runs 1 pages.

Where does Sprinkle's CESSNA 310Q Airworthiness Directives come from?

This CESSNA 310Q Airworthiness Directives was originally published by services.casa.gov.au and is hosted on Sprinkle with full text and specs.