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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08945 In force Legislative Instrument

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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

 

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.