// FAA AD DETAIL
FAA AD Detail
FAA 95-22-04
FAA 95-22-04
HistoricalFinal rule; request for comments
- Subject
- Main Landing Gear Axle
- Model
- CL-215-1A10 | CL-215-6B11 (CL-215T Variant) | CL-215-6B11 (CL-415 Variant)
- Docket Number
- 95-NM-173-AD
- Amendment Number
- 39-9411
- Publish Date
- Effective Date
- 1995-11-08
- Superseded AD
- Superseded By
- FAA 2004-03-13