// FAA AD DETAIL
FAA AD Detail
FAA 2008-20-04
FAA 2008-20-04
CurrentFinal rule.
- Subject
- HP turbine discs
- Model
- RB211-22B-02 | RB211-22B/MOD 72-8700 | RB211-524B-02 | RB211-524B-B-02 | RB211-524B2-19 | RB211-524B2-B-19 | RB211-524B3-02 | RB211-524B4-02 | RB211-524B4-D-02 | RB211-524C2-19 | RB211-524C2-B-19 | RB211-524D4-19 | RB211-524D4-39 | RB211-524D4-B-19 | RB211-524D4-B-39 | RB211-524D4X-19 | RB211-524D4X-B-19 | RB211-524G2-19 | RB211-524G2-T-19 | RB211-524G3-19 | RB211-524G3-T-19 | RB211-524H-36 | RB211-524H-T-36 | RB211-524H2-19 | RB211-524H2-T-19 | RB211-535E4-37 | RB211-535E4-B-37 | RB211-535E4-B-75 | RB211-535E4-C-37
- Docket Number
- FAA-2007-0078
- Amendment Number
- 39-15683
- Publish Date
- 2008-09-29
- Effective Date
- 2008-11-03
- Superseded AD
- Superseded By