Commonwealth legislation

AD/GAF-N22/32 - Trim Tab Hinge to Horizontal Stabiliser Attachment - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The AD mandates a one‑time inspection of the trim‑tab hinge attachment on GAF N22/N24 aeroplanes that have had replacement hinge part MS20001‑4 fitted, to detect rivet holes with nil edge distance. It must be done within 20 hours’ time in service after 14 Feb 1980, follows GAF Telex SB ANMD‑27‑16 for procedure, and is a mandatory regulatory cost on affected owners/operators.

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/GAF-N22/32 - Trim Tab Hinge to Horizontal Stabiliser Attachment - Inspection.

AD/GAF-N22/32 - Trim Tab Hinge to Horizontal Stabiliser Attachment - 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 Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source GAF N22 and N24 Series Aeroplanes

AD/GAF-N22/32 Trim Tab Hinge to Horizontal Stabiliser

Attachment - Inspection

3/80

Applicability: All N22 and N24 series which have had replacement trim tab hinge P/N MS20001-4 fitted in service.

Document: GAF Telex Alert SB ANMD-27-16.

Compliance: Unless already accomplished, within 20 hours time in service after 14 February 1980.

Background: An operator has had a replacement hinge fitted in which the rivet holes in the horizontal stabiliser attach section of the hinge were drilled with nil edge distance.

Source text

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