AD 2001-20-06

final rule
Data completeness: 60%

Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplane, and Model A300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600) Series Airplanes

AD Number
2001-20-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-282-AD
FR Citation
66 FR 50529

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplane, and Model A300 B4-600, B4-600R, and F4-600R (Collectively Called A300-600) Series Airplanes

Unsafe Condition

Fatigue cracking of the main landing gear (MLG) attachment fittings at gear rib 5 (left and right) at the lower flange and vertical web 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 a one-time inspection to detect cracks in gear rib 5 (left and right) of the MLG attachment fittings at the lower flange and vertical web, repair if necessary. Compliance must be done in accordance with repair methods approved by FAA or DGAC.

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, and Model A300 B4-600, B4-600R, F4-600R (collectively A300-600) series airplanes, including those with series numbers 789, 790, and 791.

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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