AD 2015-14-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Airplanes |
| engine | General Electric | Company CF6-80A3 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Side link clevis bolts of the front engine mount do not meet the Design Service Goal (DSG) requirements on airplanes equipped with General Electric Company CF6-80A3 engines, which could lead to failure of the front engine mount and possible in-flight separation of the engine.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the side link clevis bolts, nuts, and bushings of the front engine mount on both engines within 18 months after the effective date of the AD, and re-identify the new installed bolts with a cross. Repeat the replacement at intervals not to exceed 29 years.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 18 months after the effective date of the AD
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Affected Aircraft
All Airbus Model A310-203 airplanes, certificated in any category, all manufacturer serial numbers, equipped with General Electric Company CF6-80A3 engines.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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