AD/DHC-3/33 - Wing Strut to Fuselage Tie Bar
1AD/DHC-3/33 - Wing Strut to Fuselage Tie Bar
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/DHC-3/33 - Wing Strut to Fuselage Tie Bar.
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
Image unavailable in extracted text DHC-3 (Otter) Series Aeroplanes
AD/DHC-3/33 Wing Strut to Fuselage Tie Bar 13/87
Applicability: All models.
Requirement: Action in accordance with de Havilland Canada SB 3/37 Rev B.
Note: Canadian AD CF-82-26 refers.
Compliance: Prior to the initial issue of a Certificate of Airworthiness and thereafter at periods not exceeding 12 months.
Background: Tie bar lugs have been found corroded as well as the internal channel section under the cabin floor.