AD 91-18-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A300 B2-1C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2-1C, B2K-3C, and B2-203 Series Airplanes |
| aircraft | Airbus SAS | A300 B2-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2-1C, B2K-3C, and B2-203 Series Airplanes |
| aircraft | Airbus SAS | A300 B2K-3C | Airworthiness Directives; AIRBUS INDUSTRIE Model A300 B2-1C, B2K-3C, and B2-203 Series Airplanes |
Unsafe Condition
Reduced structural integrity of the wings due to potential cracks in the vertical web of the front spar between ribs 10 and 11.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a high frequency eddy current inspection of the vertical web of the front spar of both wings between ribs 10 and 11 prior to 11,000 landings or within 25 landings after the AD's effective date (whichever is later). Repeat inspections at intervals not exceeding 25 landings thereafter. Repair cracks prior to further flight if detected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 11,000 landings, or within the next 25 landings after the effective date of this AD, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
AIRBUS INDUSTRIE Model A300 B2-1C, B2K-3C, and B2-203 series airplanes where Modification Number 7811H1110 has not been accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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