Document ID: chunk:federal_register_of_legislation:F2006B09844:body:0
Version: federal_register_of_legislation:F2006B09844
Segment Type: other
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Character Range: 0–716

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

 Fokker F50 (F27 Mk 50) Series Aeroplanes

AD/F50/19 Engine Controls 7/89

 Applicability: All F27-050 S/No 20103 thru 20108, 20110 thru 20135. Requirement:  Action in accordance with Fokker Service Bulletin SB F50-76-002.
            Note: RLD AD 89-39 refers.

 Compliance: Prior to 15 September, 1989.

            Background:  The manufacturer has advised that when a failure occurs in the power lever control cable system, the automatic flight idle stop mechanism will be ineffective. In certain conditions this may result in an uncontained propeller overspeed.