AD/EMB-110/6 - Wing Upper Skin - Inspection
1AD/EMB-110/6 - Wing Upper Skin - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/EMB-110/6 - Wing Upper Skin - Inspection.
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 Embraer EMB-110 (Bandeirante) Series Aeroplanes
AD/EMB-110/6 Wing Upper Skin - Inspection 6/79
Applicability: All models.
Document: Embraer Service Bulletin 110-57-012. Compliance: As per requirement document.
Background: This inspection is a precautionary measure following discovery of skin cracks in the manufacturer’s fatigue test.