AD 2019-08-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Bell | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Cracks at the lower riveting of the four titanium angles that connect the belly fairing to the keel beam side panels on both sides of the fuselage, which could affect the structural integrity of the airplane.
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Required Actions
Inspect the titanium angles between the belly fairing and the keel beam side panel, inspect the open holes of cracked titanium angles, and correct any necessary actions. Perform a detailed inspection for, and replacement of, certain rivets, and applicable corrective actions.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus SAS Model A318 series airplanes; Airbus SAS Model A319 series airplanes; Airbus SAS Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Airbus SAS 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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