AD/ROTAX/16 - Inspect/Replace Engine Mount
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Terminating Action
Replacement of the engine mount, as required by Requirement 2 of this Directive, constitutes compliance with the initial inspection and repeat inspections required by Requirement 1 this Directive.
Note 1: Reference to ferry flight approval contained in the Requirement documents of this Directive DOES NOT automatically constitute approval for Australian registered aircraft.
Note 2: Austrian CAA AD 105R1 refers.
Compliance: For Requirement 1: Every 100 hours time-in-service (TIS) from the effective date of this Directive.
For Requirement 2: Before further flight.
This Airworthiness Directive becomes effective on 27 November 2003.