Document ID: chunk:federal_register_of_legislation:F2006B08945:body:0
Version: federal_register_of_legislation:F2006B08945
Segment Type: other
Provision Reference: 
Character Range: 0–727

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.