AD/DO-27/2 - Tailplane Front Spar - Modification
1AD/DO-27/2 - Tailplane Front Spar - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/DO-27/2 - Tailplane Front Spar - 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
Image unavailable in extracted text Dornier DO-27 Series Aeroplanes
AD/DO-27/2 Tailplane Front Spar - Modification 2/64
Applicability: All DO27Q series prior to S/No. 2139.
Requirement: 1. Modify the centre section of the front tailplane spar in accordance with Dornier Technical Bulletin No. 27/13 Rectification part “B” unless Part “A” has been carried out. or
- Dornier TB No. 27/13. Compliance: Before 1 September 1971.