AD 2001-17-29

final rule
Data completeness: 70%

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

AD Number
2001-17-29
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-263-AD
FR Citation
66 FR 45581

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 B2 and B4 Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes, 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, which 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

Inspect gear rib 5 (left and right) of the MLG attachment fittings at the lower flange and vertical web for cracks. Repair if necessary.

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

Compliance Time

Within 12 months of the effective date (September 13, 2001).

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, and Model A300 B4-600, B4-600R, and F4-600R (collectively called A300-600) 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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