AD 2004-20-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 and B4 | Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600) |
Unsafe Condition
Several repairs and some allowable damage limits specified in the structural repair manuals do not provide adequate static and/or fatigue strength for repaired wing slats. This could result in loss of the slats and consequent reduced controllability of the airplane.
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Required Actions
Within 18 months or 1,500 flight cycles from the effective date, perform a detailed inspection of the skin panels of the wing slats for damage and certain repairs, and do all applicable related investigative/corrective actions as per the applicable service bulletin. If damage is detected, repair in accordance with an approved method. If a repair with a specific Airbus approval other than a Repair Approval Sheet signed by the DGAC is found, perform the applicable related investigative/corrective actions before further flight.
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Compliance Time
Within 18 months or 1,500 flight cycles from the effective date, whichever occurs first.
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Affected Aircraft
All Airbus Model A300 B2 and B4 series airplanes; and Airbus Model A300 B4-600, B4-600R, F4-600R series airplanes, and Model C4-605R Variant F airplanes (collectively called A300-600) with serial numbers 796 and earlier.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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