AD 2012-02-03

final rule
Data completeness: 70%

Airworthiness Directives; CFM International, S.A. Turbofan Engines

AD Number
2012-02-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0946
FR Citation
77 FR 6666

Applicability

TypeManufacturerModelDetails
engine CFM International Airworthiness Directives; CFM International, S.A. Turbofan Engines

Unsafe Condition

This AD was prompted by a normal quality sampling at CFM International, S.A. that isolated a production batch of fan blades with nonconforming geometry of mid-span shroud tips of the fan blades. This defect could cause the upper panel of the fan blade to be liberated following foreign object damage (FOD) or a bird strike, and likely result in an inflight shutdown (IFSD).

Required Actions

Remove fan blades from service within 5,000 flight hours after the effective date of this AD. Do not install any fan blade, P/N 338-002-114-0, that has a S/N listed in Appendix A of CFM International SB No. CFM56-5B S/B 72-0777, Revision 1, dated April 11, 2011, onto any engine.

Compliance Time

Within 5,000 flight hours after the effective date of this AD

Affected Aircraft

CFM International, S.A. CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3, CFM56-5B4/3, CFM56-5B5/3, CFM56-5B6/3, CFM56-5B7/3, CFM56-5B8/3, CFM56-5B9/3, CFM56-5B3/3B1, and CFM56-5B4/3B1 engines equipped with fan blades part number (P/N) 338-002-114-0 that have a serial number (S/N) listed in Appendix A of CFM International Service Bulletin (SB) No. CFM56-5B S/B 72-0777, Revision 1, dated April 11, 2011.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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