AD 2019-11-09

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Airbus SAS Airplanes

AD Number
2019-11-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2018-1068
FR Citation
84 FR 28719

Applicability

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

Unsafe Condition

Failure of a crossbeam of the forward engine mount, which could result in detachment of the engine and consequent reduced controllability of the airplane.

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

Required Actions

Replacing on an aeroplane any affected crossbeam with crossbeam having P/N 642-2002-503 in accordance with instructions provided by Airbus is an acceptable alternative method to comply with the requirements of paragraph (1) of this AD, provided that, following modification, no affected crossbeam is installed on that aeroplane.

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

Compliance Time

Before exceeding the life limit of 64,000 flight cycles.

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

Affected Aircraft

All Airbus SAS Model A319-113 and -114 airplanes, and Model A320-211 and -212 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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