AD 2013-26-06

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Corporation Turbofan Engines

AD Number
2013-26-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2009-0811
FR Citation
79 FR 344

Applicability

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

Unsafe Condition

Uncontained failure of the high-pressure turbine (HPT) stage 2 wheel, which could result in damage to the engine and the airplane.

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

Required Actions

Remove certain HPT stage 2 wheels with specified part numbers (P/N 23084520, 23069438, 23069592, 23074462, 23074644, or 23075345) from Rolls-Royce Corporation AE 3007A series turbofan engines, except for those listed in Table 2 through Table 5 of RRC Alert Service Bulletin No. AE 3007A-A-72-414, Revision 1.

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

Compliance Time

Before further flight

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Affected Aircraft

Rolls-Royce Corporation AE 3007A, A1, A1/1, A1/2, A1/3, A1P, A1E, and A3 turbofan engines with an installed HPT stage 2 wheel, P/N 23084520 or P/N 23069438, 23069592, 23074462, 23074644, or 23075345, except for the HPT stage 2 wheel serial numbers listed in Table 2 through Table 5 of RRC Alert Service Bulletin No. AE 3007A-A-72-414, Revision 1.

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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