AD 2015-22-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Skin disbonding on a composite side shell panel of a rudder, starting from a previously repaired area, which could affect the structural integrity of the rudder and potentially reduce control of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect to determine if any rudder composite side shell panel has been repaired. Conduct a thermography inspection of each rudder that has received a composite rudder side shell panel repair. Perform related investigative and corrective actions if necessary, including elasticity laminate checker (ELCH) inspections, ultrasonic testing (UT) inspections, and detailed inspections. Corrective actions may include core venting, replacements, restorations, and repairs.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 24 months of the effective date (December 15, 2015).
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Affected Aircraft
All Airbus Model A318, A319, A320, and A321 series airplanes.
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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