Commonwealth legislation

AD/DH114/27 Amdt 1 - Flap Datum Hinge Assembly - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The instrument amends AD/DH114/27 to mandate inspections of the flap datum hinge assembly on all Hawker Siddeley DH114 (Heron) aeroplanes, using procedures/timing in Hawker Siddeley TNS Heron (114) No. CF.14, Issue 1. Owners/operators must comply (Para.4.1 within 25 flight‑hours after 17 July 1970); costs, downtime and any repairs fall to them, and reliance on the external document creates implementation and scheduling risks.

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/DH114/27 Amdt 1 - Flap Datum Hinge Assembly - Inspection.

AD/DH114/27 Amdt 1 - Flap Datum Hinge Assembly - 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 DH114 (Heron) Series Aeroplanes

AD/DH114/27

Amdt 1

Flap Datum Hinge Assembly - Inspection NK

Applicability: All models.

Document: Hawker Siddeley TNS Heron (114) No. CF.14, Issue 1. Compliance: For Para. 4.1 - Within 25 hours time in service after 17 July 1970.

For Paras. 4.2 & 4.3 - In accordance with the requirement document.

Source text

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