AD/PA-11/2 Amdt 5 - Wing Lift Strut Forks
1AD/PA-11/2 Amdt 5 - Wing Lift Strut Forks
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Piper PA-11 (Cub) & J3 Series Aeroplanes
AD/PA-11/2
Amdt 5
Wing Lift Strut Forks 5/95
Applicability: All model PA-11 AND J3.
Requirement: 1. Install “No Step” Decal on starboard lift strut.
- Retire lift strut forks from service.
Installation of sealed lift struts in accordance with Piper mandatory Service Bulletin 528D cancels the retirement Requirement of this Directive (AD/PA-11/5 refers).
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).