AD 2010-25-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A300 Series Airplanes |
Unsafe Condition
The Primary Load Path (PLP) of the THSA upper attachment may fail during an extended period, leading to the rupture of the upper attachment and consequent THSA loss of command, resulting in reduced control of the aeroplane.
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Required Actions
Perform a detailed visual inspection for metallic particles, cracks, scratches, and missing materials of the THSA upper attachment and screw shaft, in accordance with Airbus Mandatory Service Bulletin A300-27-0203. Repeat the inspection at intervals not to exceed 2,500 flight hours. If any damage is found, contact Airbus for approved corrective action instructions and accomplish those instructions before further flight.
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Compliance Time
Within 2,500 flight hours after the effective date of this AD
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Affected Aircraft
Airbus Model A300 B2-1A, B2-1C, B4-2C, B2K-3C, B4-103, B2-203, and B4-203 airplanes, all serial numbers.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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