AD 2018-15-01

final rule
Data completeness: 80%

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

AD Number
2018-15-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2017-1237
FR Citation
83 FR 34755

Applicability

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

Unsafe Condition

An occurrence was reported where, following N2 vibration and multiple messages, the flight crew performed an engine in-flight shut-down (IFSD) and returned to the departure airport, landing uneventfully. The post-flight borescope inspection of the engine revealed an intermediate pressure turbine blade (IPTB) missing at the shank. Analysis shows that this kind of failure is due to sulphidation corrosion cracking.

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Required Actions

Remove one engine from an airplane before both engines exceed their respective IPT blade operating restrictions. De-pairing of the affected engines is required.

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Compliance Time

Before further flight

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Affected Aircraft

Rolls-Royce plc, Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-A2, Trent 1000-C2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 engine models.

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Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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