Document ID: chunk:federal_register_of_legislation:F2006B05638:body:0
Version: federal_register_of_legislation:F2006B05638
Segment Type: other
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Character Range: 0–1219

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-28 Series Aeroplanes

                       AD/PA-28/84 Nose Landing Gear - Inspection and Modification Parts I and II

5/82

Applicability:   PART I -   All models PA-28R-201T Turbo Arrow III S/Nos. 28R-7703001 to 28R- 7803373 and PA-28RT-201T Turbo Arrow IV S/Nos. 28R-7931001 to
                            28R- 8131193.
                 PART II -  All models PA-28R-200 Arrow II S/Nos. 28R-7635522 to 28R-7635545. All models PA-28R-201 Arrow III S/Nos. 28R-7737001 to 28R-7837317.
                            All models PA-28RT-201 Arrow IV S/Nos. 28R-7918001 to 28R- 8118082.

 Document: Piper SB No. 724 Parts I and II.

            Note: FAA AD 82-06-011 refers.

 Compliance: Within 100 hours time in service after 31 May 1982.

            Background: There have been incidents involving inadvertent retraction of the nose landing gear. These incidents were caused by failures of various components of the nose landing gear retraction/extension system including the down lock, link and brace assemblies, actuator housings and attachment brackets.