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FAA AD Detail

FAA 2000-14-16

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FAA 2000-14-16

Current

Final rule

Subject: Tail Rotor System
Model: 407
Docket Number: 2000-SW-10-AD
Amendment Number: 39-11827
Publish Date: 2000-07-25
Effective Date: 2000-08-29
Superseded AD: FAA 99-06-15
Superseded By

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