// FAA AD DETAIL
FAA AD Detail
FAA 87-13-05 R1
FAA 87-13-05 R1
Current- Subject
- Components Fatigue Failure
- Model
- AS355E | AS355F | AS355F1 | AS355F2
- Docket Number
- Unknown
- Amendment Number
- 39-5927
- Publish Date
- Effective Date
- 1988-06-08
- Superseded AD
- Superseded By