AD/PA-34/40 - Stabilator Attach Fitting Corrosion
1AD/PA-34/40 - Stabilator Attach Fitting Corrosion
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-34/40 - Stabilator Attach Fitting Corrosion.
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-34/40 Stabilator Attach Fitting Corrosion 5/87
Applicability: All models listed in Piper SB No 856. Requirement: Action in accordance with Piper SB No 856.
Compliance: At the next scheduled inspection for Maintenance Release issue after 7 May 1987 and thereafter at intervals not exceeding one year.
Background: The manufacturer reports instances of severe corrosion between the steel attach fittings and fuselage structure.