AD 2018-03-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
fatigue damage in the structure for the door stop fittings on certain fuselage frames (FR) 66 and FR 68 on left hand (LH) and right hand (RH) sides
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
repetitive rototest inspections for cracking of the fastener holes in certain door stop fittings, and repair if necessary
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 30 days of March 19, 2018
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A318 series airplanes; Model A319 series airplanes; Model A320-211, -212, -214, -231, -232, and -233 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 6, 2026
Rights: U.S. Government Public Domain
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