AD/PA-20/3 Amdt 6 - Wing Lift Strut Forks
1AD/PA-20/3 Amdt 6 - Wing Lift Strut Forks
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-20/3 Amdt 6 - Wing Lift Strut Forks.
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-20/3
Amdt 6
Applicability: All models.
Wing Lift Strut Forks 5/95
Requirement: 1. Install “No Step” Decal on starboard lift strut.
- Retire lift strut fork from service.
Installation of sealed lift struts in accordance with Piper mandatory Service Bulletin 528D cancels the retirement Requirement of this Directive (AD/PA-20/17 refers).
For those models which have a fairing over the front and rear strut lower ends, a single placard on the starboard fairing will suffice.
Note: FAA AD 93-10-06 and Piper Service Bulletin 157D refer.
Compliance: 1. Install placard before 50 hours time in service after 30 September 1986.
- Retire lift strut forks before the accumulation of 1000 hours time in service. This amendment is effective from 27 April 1995.
Background: This Amendment specifies the individual actions to be taken and provides for a terminating modification. the continuing airworthiness of these components is managed on a retirement life basis. It is no longer required to perform a magnetic particle inspection at the half life (500 hours).