AD 2012-25-09

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

AD Number
2012-25-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2012-0482
FR Citation
78 FR 5

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Unsafe Condition

Intermediate-pressure (IP) turbine discs produced before 1997 may contain steel inclusions, which could lead to uncontained IP turbine disc failure, engine failure, and damage to the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove and inspect affected IP turbine discs for steel inclusions. Remove discs from service if they fail inspection. Remove some discs from service at reduced life limits.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Rolls-Royce plc RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36, RB211-524H-T-36, RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75, and RB211-535E4-C-37 turbofan engines with IP discs listed in Appendix 1 and Appendix 2 of RR Alert Service Bulletin RB.211-72-AG493, Revision 2.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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