AD/PA-34/33 - Window Curtain Rod Support Area - Inspection
1AD/PA-34/33 - Window Curtain Rod Support Area - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-34/33 - Window Curtain Rod Support Area - 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 Piper PA-34 (Seneca) Series Aeroplanes
AD/PA-34/33 Window Curtain Rod Support Area - Inspection 10/79
Applicability: All model PA-34-200T with S/Nos. referenced in Piper SB No. 656. Document: Piper SB No. 656.
Compliance: Within 100 hours time in service after 30 November 1979.
Background: Damage to the fuselage longerons at the lower window line may have been caused when installing the window curtain rods at manufacture.