AD/AS 355/57 Amdt 1 - Tail Rotor Hub Pitch Change Bearings
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Eurocopter AS 355 (Twin Ecureuil) Series Helicopters
AD/AS 355/57 Amdt 1 (continued)
This Amendment has been issued to reflect compliance that is now relevant. The original is sue of this Directive became effective 7 March 2001.
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James Coyne
Delegate of the Civil Aviation Safety Authority 24 September 2002
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The above AD is notified in the Commonwealth of Australia Gazette on 9 October 2002.