AD/PL 12/20 Amdt 3 - Main Wing and Stub Wing Fatigue Life Limitation
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AD/PL 12/20 Amdt 3 - Main Wing and Stub Wing Fatigue Life Limitation
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AD/PL 12/20 Amdt 3 (continued)
Background: The manufacturer has carried out fatigue life evaluations which have established the above fatigue life limitations.
Amendment 1 was raised to include the model PL 12/T400. Amendment 2 corrected some transcription errors.
Amendment 3 corrects a typographical error.
Signature of James Coyne, Delegate of the Civil Aviation Safety Authority.
James Coyne
Delegate of the Civil Aviation Safety Authority 25 June 2004
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The above AD is notified in the Commonwealth of Australia Gazette on 14 July 2004.