Document ID: chunk:federal_register_of_legislation:F2006B06224:body:0
Version: federal_register_of_legislation:F2006B06224
Segment Type: other
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Propellers - Variable Pitch - Hartzell

AD/PHZL/66 Blade Pitch Change Knob 9/94 DM

            Applicability: All model HC-E4A-3A/E10950( ) propellers prior to and including S/N HJ198 installed on Beech 1900D aircraft.

            Requirement: Unless previous carried out action in accordance with Hartzell Alert Service Bulletin A190.

            Note: FAA AD 94-10-01 Amdt 39-8908 refers.

 Compliance: As specified in the Requirement Document effective from 6 July 1994.

            Background: The manufacturer has advised that failure of the pitch change knob attachment screws can cause vibration and failure of the propeller to completely go into the feather position.