AD 2022-02-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Cracking of the web holes at the door stop fittings, which could affect the structural integrity of the airplane.
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Required Actions
Perform repetitive rototest inspections of the holes at the door stop fittings for any cracking, and repair if necessary, as specified in EASA AD 2018-0289R1. The next inspections are done at the times specified in the approved method. For paragraph (3) of EASA AD 2018-0289R1, the next inspections are done at the times specified in the approved method. The approved method may be in the form of an Airbus RDAS or an RDAF, and the compliance time is specified in the repair approved by the Manager, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
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Compliance Time
Within 30 days of the effective date of this AD for airplanes affected by condition "A" in "Table 1: Inspection Thresholds" of AD 2018-0289R1, and before further flight.
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Affected Aircraft
Airbus SAS Model A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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