Reims-Cessna F152 — Service Bulletins

This document is an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA) of Australia, specifically addressing safety concerns related to the vertical fin attach brackets, nutplates, and fittings on various Cessna and Reims-Cessna aircraft models. The directive mandates inspections and potential replacements of specific components to prevent structural failures that could lead to the separation of the tail assembly from the aircraft. The AD applies to multiple models, including the Reims-Cessna F152, and outlines compliance timelines and methods for inspection. It is essential for operators and maintenance personnel to adhere to the requirements to ensure the safety and airworthiness of the affected aircraft.

• The AD applies to Cessna 150, F150, 152, and Reims-Cessna F152 models.
• Inspect vertical fin attach brackets and nutplates as per specified service bulletins.
• Compliance for FRA150L and FRA150M is within 100 hours after 26 October 2006; other models within 100 hours after 31 November 1984.
• If cracks or corrosion are found during inspection, brackets must be replaced immediately.
• The directive was issued due to safety concerns regarding potential structural failures.