// FAA AD DETAIL

FAA AD Detail

FAA 2008-20-04

FAA 2008-20-04

Current

Final 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Superseded AD
Superseded By