Commonwealth legislation

AD/AA-5/17 - Structural and Control Surface Bondlines - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires owners/operators of specified Gulfstream (Grumman American/American Aviation) AA‑5, AA‑5A and AA‑5B aeroplanes (listed serial numbers) to inspect structural and control-surface bondlines within 25 hours’ time‑in‑service after 21 September 1976 and then at intervals not exceeding 100 hours until the aircraft is modified per Grumman American SB No.155 or FAA AD 76‑17‑03. It matters because the inspections and required modification shift inspection costs and labour onto aircraft owners and remove the repetitive inspection obligation once the SB modification is carried out.

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/AA-5/17 - Structural and Control Surface Bondlines - Inspection.

AD/AA-5/17 - Structural and Control Surface Bondlines - Inspection

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-description: CASA Airworthiness Directive meta-generator: Aspose.Words for .NET 22.10.0 meta-keywords: Issue NK,Aircraft below 5700 kg,Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes,Structural and Control Surface Bondlines - Inspection,17 title: Airworthiness Directive - AD/AA-5/17 - Structural and Control Surface Bondlines - Inspection

?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 Gulfstream (Grumman American/ American Aviation) AA-5 Series Aeroplanes

AD/AA-5/17 Structural and Control Surface NK

Bondlines - Inspection

Applicability: Model AA5 with S/Nos. 0001 and subs. Model AA-5A with S/Nos. 0001 to 0196.

Model AA-5B with S/Nos. 0001 to 0324.

Document: 1. Grumman American SB No. 155; or 2. FAA AD 76-17-03.

Compliance: Within 25 hours’ time in service after 21 September 1976 and there- after at intervals not exceeding 100 hours’ time in service until modified in accordance with SB No.

Source text

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