Commonwealth legislation

AD/CA21/2 - Wing Lift Struts

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates immediate inspection of the wing lift strut tube-to-fairing join for corrosion on Skyfox CA21/CA22A aeroplanes with specified serial numbers, to be completed before further flight after 4 January 1996.

If corrosion is found, fairings must be removed and the strut tube may need replacement. Owners/operators bear the inspection and repair costs and aircraft cannot fly until the AD’s requirements are met.

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/CA21/2 - Wing Lift Struts.

AD/CA21/2 - Wing Lift Struts

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 Skyfox Aviation (Calair/Hedaro) CA21 and CA22A Series Aeroplanes

AD/CA21/2 Wing Lift Struts 1/96

Applicability: Aircraft with serial numbers CA-21004 to CA-21039 and CA-22001 to CA-22014.

Requirement: Inspect the wing lift strut tube to fairing join for evidence of corrosion in accordance with Skyfox Aviation Service Bulletin No. 13.

Compliance: Before further flight after 4 January 1996.

Background: It has been reported that corrosion can initiate at the tube to fairing join. This AD requires removal of the fairings if corrosion is found and possible replacement of the strut tube.

Source text

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