Commonwealth legislation

AD/DH114/30 - Main Undercarriage - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

The AD requires operators of Hawker Siddeley DH114 (Heron) aeroplanes fitted with down‑lock operating lever assemblies P/N 14‑2U to carry out the inspection and any corrective actions specified in Hawker Siddeley TNS Heron (114) No. U.12 Issue 1. Issued by CASA under Part 39, compliance (and associated labour, parts and downtime costs) rests with aircraft owners/operators and their maintenance organisations, who must obtain and follow the referenced manufacturer document.

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Current sections

Direct links to the current provisions in AD/DH114/30 - Main Undercarriage - Inspection.

AD/DH114/30 - Main Undercarriage - Inspection

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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/DH114/30 Main Undercarriage - Inspection NK Applicability: All models fitted with down lock operating lever assemblies P/N 14-2U. 181A/1. Document: Hawker Siddeley TNS Heron (114) No. U.12 Issue 1.

Compliance: As detailed in requirement document.

Source text

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

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

DH114 (Heron) Series Aeroplanes

Compliance: As detailed in requirement document.