AD 2018-02-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracks were found in the horizontal stabilizer (HS) centre box (CB) top skin of an aeroplane in pre-modification 41330 configuration. The cracks were initiated at the upper flange corner at Rib 3 rear spar area on left hand side of the CB.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
A one-time special detailed inspection (SDI) of the HS CB top skin integral flange area and, depending on findings, accomplishment of applicable corrective action(s).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A330-301, -321, -322 and A330-342 airplanes, manufacturer serial numbers 0012, 0017, 0030, 0037, 0045, 0050, 0060, 0062, 0064, 0065, 0071, 0082, 0083, 0098, 0099, 0102, 0106, 0109
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.