AD 2012-06-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A340-500 and Model -600 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking in the external radius on the upper horizontal cruciform fitting at frame (FR) 47 on the left- and right-hand sides, which could adversely affect the structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive high frequency eddy current inspections of the external radius on the upper horizontal cruciform fitting at frame (FR) 47 on the left- and right-hand sides for cracks, and repair the cracks if necessary, in accordance with Airbus Mandatory Service Bulletin A340-57-5029, including Appendices 01 and 02.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in Airbus Mandatory Service Bulletin A340-57-5029, or within 90 days 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 Model A340-541 and -642 airplanes, certificated in any category, all manufacturer serial numbers.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.