// FAA AD DETAIL
FAA AD Detail
FAA 62-25-02
FAA 62-25-02
Current- Subject
- Main Landing Gear Shock Strut Cylinder
- Model
- DC-6 | DC-6A | DC-6B | DC-7 | DC-7B | DC-7C
- Docket Number
- Unknown
- Amendment Number
- Publish Date
- 1962-11-28
- Effective Date
- Superseded AD
- Superseded By