AD 2011-14-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 | Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes |
Unsafe Condition
Fatigue cracking, accidental damage, or corrosion in principal structural elements and possible failure of certain life limited parts, 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
Revise maintenance documents to include new inspections as specified in Airbus A318/A319/A320/A321 ALI Document reference AI/SE-M4/95A.0252/96, Issue 10 or Issue 11. Comply with these inspections as required by 14 CFR 91.403(c).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times defined in Table 1 of the referenced Airbus ALI Document.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes, certificated in any category.
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.