// FAA AD DETAIL

FAA AD Detail

FAA 2008-23-04

FAA 2008-23-04

Current

Final rule; request for comments.

Subject
Intermediate pressure (IP) turbine blade
Model
RB211 Trent 553-61 | RB211 Trent 553A2-61 | RB211 Trent 556-61 | RB211 Trent 556A2-61 | RB211 Trent 556B-61 | RB211 Trent 556B2-61 | RB211 Trent 560-61 | RB211 Trent 560A2-61
Docket Number
FAA-2008-1063
Amendment Number
39-15725
Publish Date
2008-11-14
Effective Date
2008-12-01
Superseded AD
Superseded By