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FAA AD Detail

FAA 2011-12-08

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FAA 2011-12-08

Historical

Final rule; request for comments.

Subject: Tail rotor (T/R) blades
Model: 205A | 205A-1 | 205B | 212 | 412 | 412CF | 412EP
Docket Number: FAA-2011-0561
Amendment Number: 39-16715
Publish Date: 2011-06-17
Effective Date: 2011-07-05
Superseded AD
Superseded By: FAA 2020-12-10

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