Commonwealth legislation

AD/F28/13G - Retirement Times - Fatigue Critical Components

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

AD/F28/13G (Retirement Times – Fatigue Critical Components) for Fokker F28 aircraft has been cancelled. Its retirement and fatigue‑critical requirements are now enforced through the Structural Integrity Program Document specified in AD/F28/45. Operators and maintainers must consult AD/F28/45 and that program document to learn the current inspection, retirement and compliance obligations.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/F28/13G - Retirement Times - Fatigue Critical Components.

AD/F28/13G - Retirement Times - Fatigue Critical Components

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Fokker F28 Series Aeroplanes

AD/F28/13G Retirement Times - Fatigue Critical Components 10/82

CANCELLED.

The requirements of this Directive are now covered by the Structural Integrity Program Document Specified in AD/F28/45.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.