Commonwealth legislation

AD/G159/9 - Lower Centre Section Skin - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The instrument requires removal of two lower centre‑section fairings (P/Ns 159‑W10400‑121, 159‑W10401‑121) to inspect Gulfstream (Grumman) G.159 wing planks for corrosion, with an initial inspection before 1 April 1967 and repeats at intervals not exceeding six months. Any corrosion must be repaired under a repair scheme approved by the Secretary before further flight.

It applies to all G.159 aircraft; operators/owners bear inspection and repair costs and associated downtime.

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/G159/9 - Lower Centre Section Skin - Inspection.

AD/G159/9 - Lower Centre Section Skin - 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/G159/9 Lower Centre Section Skin - Inspection 12/67

Applicability: All models.

Requirement: Remove the lower centre section fairings P/Ns 159 W10400-121 and 159-W10401- 121 and inspect the wing planks for corrosion. If corrosion is found, repair the wingplanks in accordance with a scheme approved by the Secretary before further flight.

Compliance: Before 1 April 1967 and thereafter at intervals not exceeding 6 months.

Source text

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