AD 2007-25-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Series Airplanes and Model A300-600 Series Airplanes |
Unsafe Condition
Failure of the sliding rod of the main landing gear (MLG) retraction actuator before reaching the life limit established by the manufacturer, which could result in reduced structural integrity of the MLG.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect to determine the part number of the sliding rods of the MLG retraction actuators. For sliding rods with part numbers C69029-2 or C69029-3, perform detailed and high-frequency eddy current (HFEC) inspections for discrepancies, including cracking, and perform corrective actions if necessary. Return affected sliding rods to the manufacturer.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,000 flight cycles or 12 months, whichever occurs first, after the applicable time specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A300 series airplanes and all Airbus Model A300-600 series airplanes, certificated in any category.
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
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