AD/PA-23/41 - Auxiliary Front Spar - Inspection
1AD/PA-23/41 - Auxiliary Front Spar - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-23/41 - Auxiliary Front Spar - 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-23 (Apache and Aztec) Series Aeroplanes
AD/PA-23/41 Auxiliary Front Spar - Inspection 2/71
Applicability: All models.
Requirement: Visually inspect the web of auxiliary front spar P/N 16010 at the outboard end in the area adjacent to rib P/N 16042 (STA 56) for vertical cracks especially near the bend radius.
Compliance: Within 50 hours time in service after 4 January 1971.