AD 2020-15-07

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (Type Certificate Formerly Held by Rolls-Royce plc) Turbofan Engines

AD Number
2020-15-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2020-0617
FR Citation
85 FR 43682

Applicability

TypeManufacturerModelDetails
aircraft Rolls-Royce plc Various Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (Type Certificate Formerly Held by Rolls-Royce plc) Turbofan Engines

Unsafe Condition

A review of operational flight data revealed that some RB211-524 engines may have been operated beyond the currently valid datum flight profile (FP) published in the applicable Aircraft Maintenance Manuals. The purpose of the datum FPs is to establish the operational limits (life limits) within which the corresponding critical parts are allowed to remain installed. In addition, as this FP exceedance was investigated, it was realised that the current life limits of certain P/N corresponding to reworked LPT Stage 1 discs (time since new, or since entry into service following rework) could no longer be supported. This condition, if not corrected, could lead to disc failure, possibly resulting in engine in-flight shut-down and high energy debris release, with consequent damage to, and reduced control of, the aeroplane.

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

Required Actions

This AD requires removal from service of the affected parts. This AD also prohibits (re)installation of affected parts that have exceeded the new reduced limits. The FAA reviewed Rolls-Royce plc Alert Non-Modification Service Bulletin (NMSB) RB.211-72-AK422, Revision 1, dated March 2, 2020. The NMSB describes procedures for reducing the Declared Safe Cyclic Limit for LPT stage 1 disks. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section.

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

Compliance Time

Within 25 flight cycles after the effective date of this AD, whichever occurs later.

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Affected Aircraft

Rolls-Royce Deutschland Ltd & Co KG RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19, RB211-524G3-T-19, RB211-524H2-19, RB211-524H2-T-19, RB211-524H-36 and RB211-524H-T-36 model turbofan engines.

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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