Commonwealth legislation

AD/F27/111 - Reduced Span Rudder Trim Tab

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive mandates a specific modification to the rudder trim tab on certain Fokker F27s, carried out exactly as Fokker Service Bulletin F27/55-62, to be completed by 31 March 1988. It affects owners/operators of the listed serial-numbered aircraft and the maintenance organisations that must perform and fund the work; the change is intended to remedy problems with the previous trim-tab design.

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/F27/111 - Reduced Span Rudder Trim Tab.

AD/F27/111 - Reduced Span Rudder Trim Tab

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/F27/111 Reduced Span Rudder Trim Tab 12/86

Applicability: All model F27 with S/Nos. 10102 to 10684; 10686, 10687 and 10689 to 10692. Requirement: Action in accordance with Fokker S.B. F27/55-62.

Note: RLD BLA 86-53 refers.

Compliance: Prior to 31 March 1988.

Background: This modification alleviates most of the problems associated with the previous design rudder trim tab.

Source text

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