AD Amdt-39-9644

final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes, Excluding Model A300-600 Series Airplanes

AD Number
Amdt-39-9644
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-NM-161-AD
FR Citation
61 FR 28497

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes, Excluding Model A300-600 Series Airplanes

Unsafe Condition

Stress corrosion cracking in the skin at the longitudinal lap joint at certain stringers of the fuselage caused by increased stress levels from rework beyond specified limits.

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

Required Actions

Measure the thickness of the inner skin of the longitudinal lap joint from the inside of the fuselage at certain stringers. Inspect for stress corrosion cracking in the subject area and repair 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 A300 B2 and B4 series airplanes, excluding Model A300-600 Series.

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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