AD 2012-06-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A340-211 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking in the fuselage that could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive inspections for cracking at the fastener hole area just above stringer 28, of both left- and right-hand fuselage frame 39.1, using ultrasonic inspection methods. Repair any cracking found before further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6 months after the effective date of this AD or before the accumulation of 13,600 total flight cycles or 92,100 total flight hours, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A340-211, -212, -311, and -312 airplanes; certificated in any category; having manufacturer serial numbers (MSN) 0002, 0003, 0005 through 0009 inclusive, 0011, 0013, 0014, 0015, 0018 through 0023 inclusive, 0025, 0026, and 0027.
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.