AD Amdt-39-10059

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

AD Number
Amdt-39-10059
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-182-AD
FR Citation
62 FR 35072

Applicability

TypeManufacturerModelDetails
aircraft Airbus Industrie Model A300-600 Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes

Unsafe Condition

Fatigue cracks in the outer skin of the fuselage at certain frames could reduce structural integrity and cause rapid decompression.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Conduct repetitive eddy current inspections of the outer skin at specified frames. Repair or reinforce the structure if cracks are found. Reinforce the structure at certain frames to terminate repetitive inspections.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Airbus Industrie Model A300-600 series airplanes as specified by the AD.

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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