AD Amdt-39-11313

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300 and A300-600 Series Airplanes

AD Number
Amdt-39-11313
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-249-AD
FR Citation
64 FR 49966

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300 and A300-600 Airworthiness Directives; Airbus Model A300 and 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 of the MLG attachment fittings at the lower flange for cracks. Modify Gear Rib 5 of the MLG attachment fittings as terminating action for repetitive inspections. Revise the maintenance program to include the specified repetitive inspection intervals.

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

Compliance Time

Within 12 months of the effective date of this amendment.

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

Affected Aircraft

Airbus Model A300 and A300-600 series airplanes, as specified in the existing 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.