AD 2023-20-04

final rule
Data completeness: 70%

Airworthiness Directives; Airbus SAS Airplanes

AD Number
2023-20-04
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2023-1056
FR Citation
88 FR 69008

Applicability

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

Unsafe Condition

excessively deep spot faces on the front engine mounting bolt holes on the wing pylon were detected on the production line

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

Required Actions

a one-time inspection for clash (interference) of the three front engine mounting bolt holes on both the left and right wing pylons, and, depending on findings, accomplishment of applicable corrective actions, as specified in EASA AD 2023-0026

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 A350-941 and A350-1041 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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.