Commonwealth legislation

AD/AA-1/16 - Structural and Control Surface Bondlines - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

What this does: Requires owners/operators of Gulfstream (Grumman American/American Aviation) AA‑1 series aeroplanes (specified serial numbers) to inspect structural and control‑surface bondlines. Who it affects and why it matters: Applies to AA‑1/AA‑1A from S/N 0001 onward and AA‑1B S/N 0001–0641; inspections must occur within 25 hours' time‑in‑service after 21 September 1976 and then every 100 hours until the aeroplane is modified per Grumman American SB No.155 (or FAA AD 76‑17‑03). Owners/operators bear inspection and modification costs; CASA requires compliance.

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-1/16 - Structural and Control Surface Bondlines - Inspection.

AD/AA-1/16 - 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 9/1976,Aircraft below 5700 kg,Gulfstream (Grumman American/ American Aviation) AA-1 Series Aeroplanes,Structural and Control Surface Bondlines - Inspection,16 title: Airworthiness Directive - AD/AA-1/16 - 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-1 Series Aeroplanes

AD/AA-1/16 Structural and Control Surface Bondlines - Inspection

9/76

Applicability: All models AA1 and AA1A with S/Nos. 0001 and subsequent and all model AA1B with S/Nos. 0001 to 0641.

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.