AD Amdt-39-11286
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 and A310 | Airworthiness Directives; General Electric Company CF6-50, -80A1/ A3, and -80C2A Series Turbofan Engines |
| engine | General Electric | Company CF6-50 | Airworthiness Directives; General Electric Company CF6-50, -80A1/ A3, and -80C2A Series Turbofan Engines |
Unsafe Condition
Higher than anticipated center drive unit (CDU) cone brake failure rate reduces thrust reverser system protection against inadvertent deployment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Initial and repetitive thrust reverser inspections and checks are required. Extended repetitive inspection intervals are allowed if an optional double p-seal configuration is installed.
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 the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
General Electric Company CF6-50, -80A1/A3, and -80C2A series turbofan engines installed on Airbus A300 and A310 series airplanes.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.