AD 2004-26-03

final rule
Data completeness: 90%

Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines

AD Number
2004-26-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NE-62-AD
FR Citation
69 FR 77881

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211 Series Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines

Unsafe Condition

Cracks in the rim cooling air holes of certain high pressure (HP) turbine discs, manufactured between 1989 and 1999, which could propagate further than expected and lead to disc failure, resulting in an uncontained engine failure and damage to the airplane.

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

Required Actions

Inspect certain HP turbine discs for cracks in the rim cooling air holes. Replace the discs with serviceable parts if necessary. Reduce inspection schedules for high-risk discs, which include all models except the RB211-22B-02 engine.

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

Compliance Time

Within the reduced inspection schedules specified in the AD.

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

Affected Aircraft

Rolls-Royce plc RB211 Series Turbofan Engines, including models RB211-535E4-37, RB211-535E4-B-37, RB211-535C-37, RB211-535E4-B-75, RB211-535E4-C, and RB211-22B-02, with HP turbine discs manufactured between 1989 and 1999.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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