// FAA AD DETAIL
FAA AD Detail
FAA 95-22-06
FAA 95-22-06
HistoricalFinal rule; request for comments.
- Subject
- Main Landing Gear Shock Strut Cylinder
- Model
- DC-9-81 | DC-9-82 | DC-9-83 | DC-9-87 | MD-88
- Docket Number
- 95-NM-183-AD
- Amendment Number
- 39-9413
- Publish Date
- Effective Date
- 1995-11-08
- Superseded AD
- Superseded By
- FAA 99-06-13