Commonwealth legislation

AD/G159/21 - Wing Rear Beam Upper Cap Splice Angles - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive mandates inspection of the wing rear beam upper cap splice angles on all Gulfstream (Grumman) G.159 aeroplanes, to be carried out per Grumman Customer Bulletin No. 230. If not already done, inspect before the next issue of MR or by 31 July 1973, then repeat at intervals not exceeding one year. It affects all owners/operators and maintenance organisations; inspection costs, repairs and downtime are borne by operators under the Civil Aviation Safety Authority’s directive.

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/G159/21 - Wing Rear Beam Upper Cap Splice Angles - Inspection.

AD/G159/21 - Wing Rear Beam Upper Cap Splice Angles - Inspection

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 ORDERS CIVIL AVIATION SAFETY AUTHORITY PART 105 SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source GULFSTREAM (GRUMMAN) G.159 SERIES AEROPLANES

AD/G159/21 Wing Rear Beam Upper Cap Splice Angles - Inspection 6/73

Applicability: All models.

Document: Grumman Customer Bulletin No. 230.

Compliance: Unless already accomplished, before next issue of MR or 31 July 1973 whichever occurs first and thereafter at intervals not exceeding 1 year.

Source text

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