AD/DH114/15 - Top Centre Section Spar Attachment - Inspection and Modification
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
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/DH114/15 Top Centre Section Spar NK Attachment - Inspection and Modification
Applicability: All models.
Requirement: 1. Inspect Channels P/N 14FS2839-42 and Reinforcing Channels P/N 14FS383 and 386 in accordance with Hawker Siddeley Technical News Sheet Heron (114) F.7, Issue 2.
- If found cracked, modify the channels in accordance with Heron Modification No. 792.
Compliance: 1. At intervals not exceeding 300 hours time in service after 30 April 1964.
- When Mod. 792 has been incorporated the inspection interval may be extended to 5,000 hours time in service or five years whichever occurs first.