AD/DH114/34 Amdt 1 - Fuselage Keel Frame at Wing Rear Spar - Inspection
1AD/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
Image unavailable in extracted text 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.