AD 2017-22-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 and A319 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking, accidental damage, or corrosion in principal structural elements, and widespread fatigue damage (WFD), which 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
Revising the maintenance or inspection program to incorporate new or revised structural inspection requirements.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A318, A319 series airplanes; Model A320-211, -212, -214, -231, -232, -233, -251N, and -271N airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
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
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