AD 2005-25-19

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus Model A300 B2 Series Airplanes, Model A300 B4 Series Airplanes, Model A310-200 Series Airplanes, Model A310-300 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 Series Airplanes)

AD Number
2005-25-19
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-22384
FR Citation
70 FR 73930

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 Airworthiness Directives; Airbus Model A300 B2 Series Airplanes, Model A300 B4 Series Airplanes, Model A310-200 Series Airplanes, Model A310-300 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 Series Airplanes)

Unsafe Condition

could result in the reduced structural integrity of the floor and rods around FR 12A.

Required Actions

repetitive eddy current inspections for cracks of the stiffener fittings of the fuselage at frame (FR) 12A, and corrective actions if necessary

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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