AD 2014-24-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Crack found in the fuselage side box beam flange at frame (FR) 43 level, which could affect the structural integrity of the airplane.
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Required Actions
Conduct repetitive rototest inspections for cracking in the fuselage side box beam flange at FR43. Perform corrective actions (repair) if cracks are found. Modify the torsion box to terminate repetitive inspections.
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Compliance Time
Within 12 months of effective date (January 9, 2015)
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Affected Aircraft
Airbus Model A318, A319, A320, and A321 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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