AD 2016-20-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking of the No. 2 flap beams, which may propagate from the bolt holes of the base member and side members, could result in rupture of the flap beams and reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections of the No. 2 flap beam base and side members using ultrasonic methods. Replace the flap beams if cracking is detected. Reduce inspection thresholds and intervals as specified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within reduced compliance times as specified in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 series airplanes, Airbus Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). Exempts certain Model A300-600 airplanes with specific Airbus modifications.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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