AD 2023-20-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
The cold working process was partially completed on the circumferential joint at frame 58, which could affect the structural integrity of the airplane and result in catastrophic failure.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the circumferential joint at frame 58 as specified in EASA AD 2023-0054, including rotating probe inspections for cracks, cold working fastener holes, and measuring maximum hole diameter. Repair any discrepancies (cracks or excessive hole diameters) before further flight using an approved method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in EASA AD 2023-0054.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus SAS Model A330-202, A330-203, A330-223, A330-243, and A330-841 airplanes, serial numbers 1780, 1782, 1784, 1785, 1805, 1823, 1835, 1845, 1847, 1854, 1859, 1864, 1872, 1877, 1878, 1882, 1888, 1932, 1936, 1964, and 1969.
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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