AD/P68/6 - Rudder Trim Tab Control Rod P/N 68-506053 - Inspection
1AD/P68/6 - Rudder Trim Tab Control Rod P/N 68-506053 - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/P68/6 - Rudder Trim Tab Control Rod P/N 68-506053 - 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 Partenavia P68 Series Aeroplanes
AD/P68/6 Rudder Trim Tab Control Rod P/N 68-506053 - Inspection
Applicability: All models P68 and P68B.
Requirement: 1. Inspect rudder trim tab control rod for correct installation according to the instructions contained in the Partenavia SB No. 32.
10/77
- If rudder trim tab control rod installation is incorrect remove rod and inspect rod visually for distortion and the rod and rod-ends for cracks using a magnetic particle technique.
Compliance: Unless already accomplished, before further flight and thereafter at intervals not exceeding 100 hours time in service.