AD/PA-32/65 - Fuselage Firewall - Modification
1AD/PA-32/65 - Fuselage Firewall - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-32/65 - Fuselage Firewall - 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 Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/65 Fuselage Firewall - Modification 3/80
Applicability: All model PA-32RT-300T with S/Nos. as referenced in Piper SB No. 655. Document: Piper SB No. 655.
Compliance: Within 100 hours time in service after 30 November 1979.
Background: The manufacturer has received reports of a small crack developing in the firewall adjacent to the lower forward corner of the forward baggage door.