AD/PA-20/13 - Wing Fuel Tank Cap - Modification
1AD/PA-20/13 - Wing Fuel Tank Cap - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-20/13 - Wing Fuel Tank Cap - 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-20 (Pacer) Series Aeroplanes
AD/PA-20/13 Wing Fuel Tank Cap - Modification 3/78
Applicability: All models. Applicable only if a wing fuel tank cap has been replaced with either tank cap P/N 15296-02 since 1 June 1976, or, tank cap P/N 60707-02 modified as per Piper SB No 522.
Document: Piper SB No 573.
Compliance: Within 100 hours time in service after 31 May 1978.