Commonwealth legislation

AD/DH114/16 Amdt 1 - Engine Mounting Frames - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Owners/operators of DH114 (Heron) aeroplanes with engine mount frames P/N 14EM-11A or 14EM-12A must perform visual and radiographic inspections for internal corrosion (per Hawker Siddeley TNS Heron No. E3 Issue 2), at intervals not exceeding four years after 31 August 1970. Operators fund and arrange inspections, submit radiographs and reports to the Secretary for examination—imposing recurring technical, administrative and procurement costs.

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AD/DH114/16 Amdt 1 - Engine Mounting Frames - 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/DH114/16

Amdt 1

Engine Mounting Frames - Inspection NK

Applicability: All models fitted with engine mount frames P/N 14EM-11A and 14EM-12A.

Requirement: 1. Inspect the engine mounting frames for evidence of internal corrosion by visual and radiographic means.

The inspection shall be carried out in accordance with Hawker Siddeley TNS Heron (114) No. E3 Issue 2. Radiographs and any associated reports shall be submitted to the Secretary for examination.

Compliance: At intervals not exceeding 4 years after 31 August 1970.

Source text

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