Commonwealth legislation

AD/F27/107 - Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive requires operators of Fokker F27 aircraft S/N 10105–10635 to inspect the inboard aileron hinge bolt retention and replace bolts/bushes if migration or deterioration is found, following Fokker SB F27/57‑58, by the stated compliance date. It addresses a safety defect (restricted aileron movement), imposes inspection/repair costs and scheduling burdens on affected owners/operators.

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/F27/107 - Inboard Aileron Hinge Bolt Retention - Inspection and Replacement.

AD/F27/107 - Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

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 F27 Series Aeroplanes

AD/F27/107 Inboard Aileron Hinge Bolt Retention - Inspection and Replacement

Applicability: All model F27 with S/Nos. 10105 to 10635. Document: Fokker SB F27/57-58.

Note: RLD AD BLA 83-20-57 refers.

Compliance: Before 1st January 1984.

8/83

Background: Restricted aileron movement was reported due to migration of hinge bolt and bush.

Source text

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