Commonwealth legislation

AD/DH114/34 Amdt 1 - Fuselage Keel Frame at Wing Rear Spar - Inspection

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legislative instrument

Plain English Summary

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This AD requires inspection of the fuselage keel frame at the wing rear spar on all DH114 (Heron) models, to be carried out per Hawker Siddeley TNS Heron (114) No. F.17, Issue 1.

An initial inspection is due within 25 hours TIS or 30 days after 1 May 1972 (whichever comes first) and then at intervals not exceeding 600 hours; prior inspections under the previous issue may satisfy the initial check.

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AD/DH114/34 Amdt 1 - Fuselage Keel Frame at Wing Rear Spar - 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/DH114/34

Amdt 1

Applicability: All models.

Fuselage Keel Frame at Wing NK Rear Spar - Inspection

Document: Hawker Siddeley TNS Heron (114) No. F.17, Issue 1.

Compliance: Within 25 hours time in service or thirty days, after 1 May 1972 whichever occurs first and thereafter at intervals not exceeding 600 hours time in service.

Note: Inspections performed in accordance with the preceding issue of this Directive may be regarded as the initial inspection required by para. 3 of the requirement document.

Source text

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