AD 2019-19-16

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus SAS Airplanes

AD Number
2019-19-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2019-0495
FR Citation
84 FR 53997

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS Airworthiness Directives; Airbus SAS Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus SAS Airplanes

Unsafe Condition

Reports of low clearance between the electrical harness and nearby hydraulic pipes in the inboard trailing edge of the wing, which could lead to chafing of electrical harnesses in the vicinity of hydraulic pipes and could result in a potential source of ignition in the flammable fluid leakage zone, and possibly result in a fire or explosion and loss of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Retained actions from AD 2019-05-09: repetitive detailed inspections of certain electrical harnesses for discrepancies and corrective actions, if necessary. New proposed actions: a terminating modification for the repetitive detailed inspections.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Airbus SAS Model A320-251N and -271N airplanes, and Model A321-253N airplanes, certificated in any category, as identified in European Aviation Safety Agency (EASA) AD 2019-0035, dated February 15, 2019.

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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