AD Amdt-39-16093
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company CF6-50C Series | Airworthiness Directives; General Electric Company CF6-50C Series Turbofan Engines |
Unsafe Condition
Uncontained fan blade failures can result in separation of airplane hydraulic lines, damage to critical airplane systems, and possible loss of airplane control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rework the forward fan stator case and install the fan module secondary containment shield using the specified service bulletin. Compliance can also be done on-wing.
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Compliance Time
Within the next engine shop visit after the effective date, but no later than June 30, 2010.
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Affected Aircraft
General Electric Company CF6-50C, CF6-50C1, CF6-50C2, and CF6-50C2R turbofan engines with specific forward fan stator case part numbers installed on, but not limited to, Airbus A300, McDonnell Douglas DC-10 series, and DC-10-30F (KC-10A, KDC-10) airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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