AD Amdt-39-10501

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A310 Series Airplanes

AD Number
Amdt-39-10501
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-248-AD
FR Citation
63 FR 23377

Applicability

TypeManufacturerModelDetails
aircraft Airbus A310 Airworthiness Directives; Airbus Model A310 Series Airplanes

Unsafe Condition

Fatigue cracks and corrosion around and under chafing plates of the wing root could result in reduced structural integrity of the airplane.

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

Required Actions

Conduct repetitive inspections of the fuselage skin to detect corrosion or fatigue cracking around and under the chafing plates of the wing root. Perform corrective actions if necessary.

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 Model A310 series airplanes

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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