AD/PA-36/18 - Wing Main Spar Carry Through Assembly - 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
View image in the official source Piper PA-36 (Pawnee Brave) Series Aeroplanes
AD/PA-36/18 Wing Main Spar Carry Through Assembly - Inspection
5/77
Applicability: All models with S/Nos. 36-7360001 to 36-756003 inclusive, with Main Spar Carry Through Assembly P/N 97370-00 installed.
Document: Piper SB No. 552.
Compliance: As detailed in the requirement document.
Note: Retirement of Wing Main Spar Carry Through Assembly is detailed in AD/PA- 36/6A.