AD 2000-03-20

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Airbus Model A300-600 Series Airplanes

AD Number
2000-03-20
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-NM-150-AD
FR Citation
65 FR 8642

Applicability

TypeManufacturerModelDetails
aircraft Airbus A300-600 Airworthiness Directives; Airbus Model A300-600 Series Airplanes

Unsafe Condition

Cracking due to fatigue-related stress in the radius of frame 40 adjacent to the tension bolts at the center/outer wing junction.

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

Required Actions

Conduct repetitive ultrasonic inspections to detect cracks on the forward fittings in the radius of frame 40 adjacent to the tension bolts in the center section of the wings. Perform follow-on actions as specified by the AD to detect and correct fatigue cracking.

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

Affected Aircraft

All Airbus Model 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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