Commonwealth legislation

AD/AA-1/19 - Seat Belt Attachment Bracket - Replacement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive orders replacement of the seat belt attachment bracket identified by P/N 60152-2 on all Gulfstream (Grumman American/American Aviation) AA‑1 series aeroplanes, using Gulfstream Aerospace Service Bulletin No. 173. Operators must complete the replacement within 50 hours’ time in service after 31 May 1985. The measure responds to a risk that the existing bracket can fail under severe deceleration and prescribes a single corrective action and deadline.

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-1/19 - Seat Belt Attachment Bracket - Replacement.

AD/AA-1/19 - Seat Belt Attachment Bracket - Replacement

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 5/1985,Aircraft below 5700 kg,Gulfstream (Grumman American/ American Aviation) AA-1 Series Aeroplanes,Seat Belt Attachment Bracket - Replacement,19 title: Airworthiness Directive - AD/AA-1/19 - Seat Belt Attachment Bracket - Replacement

?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-1/19 Seat Belt Attachment Bracket - Replacement 5/85

Applicability: All models AA-1, AA-1A, AA-1B and AA-1C. Requirement: Gulfstream Aerospace S.B. No. 173.

Compliance: Within 50 hours’ time in service after 31 May 1985.

Background: It is possible for the existing P/N 60152-2 to fail on some aircraft in the event of severe deceleration.

Source text

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