// FAA AD DETAIL
FAA AD Detail
FAA 97-09-02 R1
FAA 97-09-02 R1
HistoricalFinal rule; request for comments.
- Subject
- High Pressure Turbine rotor (HPTR) front shaft
- Model
- CFM56-5C2/G | CFM56-5C2/G4 | CFM56-5C3/G | CFM56-5C3/G4 | CFM56-5C4 | CFM56-5C4/1
- Docket Number
- 95-ANE-64-AD
- Amendment Number
- 39-12876
- Publish Date
- 2002-09-09
- Effective Date
- 2002-09-24
- Superseded AD
- FAA 97-09-02
- Superseded By
- FAA 97-09-02 R2