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FAA AD Detail

FAA 2001-01-12

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FAA 2001-01-12

Current

Final rule

Subject
Fittings Connecting the Fuselage to Stiffener Rods
Model
CN-235 | CN-235-100 | CN-235-200
Docket Number
2000-NM-264-AD
Amendment Number
39-12082
Publish Date
2001-01-24
Effective Date
2001-02-28
Superseded AD
Superseded By
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