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FAA 2009-14-08

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FAA 2009-14-08

Current

Final rule.

Subject
High-pressure compressor rotor (HPCR) stages 11-14 spool/ shafts
Model
CF6-80C2B5F
Docket Number
FAA-2009-0121
Amendment Number
39-15958
Publish Date
2009-07-01
Effective Date
2009-08-05
Superseded AD
Superseded By
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