// FAA AD DETAIL

FAA AD Detail

FAA 2017-19-20

FAA 2017-19-20

Current

Final rule.

Subject
Turbine Engine Compressor Section
Model
CT7-8A | CT7-9B
Docket Number
FAA-2017-0452
Amendment Number
39-19050
Publish Date
2017-09-22
Effective Date
2017-10-27
Superseded AD
Superseded By