AD 2015-02-22

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Corporation Turboprop and Turboshaft Engines

AD Number
2015-02-22
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2011-0961
FR Citation
80 FR 5452

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Corporation Airworthiness Directives; Rolls-Royce Corporation Turboprop and Turboshaft Engines

Unsafe Condition

Failure of 3rd-stage and 4th-stage turbine wheel blades, which could cause engine failure and damage to the aircraft.

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

Required Actions

Replace the one-time visual inspection and fluorescent-penetrant inspection (FPI) with repetitive visual inspections and FPIs on certain 3rd-stage and 4th-stage turbine wheels.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

Rolls-Royce Corporation 250-C20, -C20B, and -C20R/2 turboshaft engines, including certain added engine models.

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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