AD 2024-19-04

final rule
Data completeness: 80%

Airworthiness Directives; Airbus S.A.S Airplanes

AD Number
2024-19-04
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2024-1881
FR Citation
89 FR 84806

Applicability

TypeManufacturerModelDetails
aircraft Airbus S Airworthiness Directives; Airbus S.A.S Airplanes
aircraft Aviat Various Airworthiness Directives; Airbus S.A.S Airplanes

Unsafe Condition

Engine nacelle anti-icing (NAI) forward bulkheads may have elongated locating holes. The fasteners, if loose, may vibrate and cause further elongation of the locating holes, which can reduce NAI performance.

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

Required Actions

Conduct a one-time detailed inspection of the engine NAI forward bulkhead locating holes for elongation and loose fasteners. Take applicable corrective actions as specified in EASA AD 2024-0060R1. Prohibit the installation of affected parts unless they are serviceable and inspected before installation.

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

Compliance Time

Within the compliance times specified in EASA AD 2024-0060R1, unless already done.

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

Affected Aircraft

All Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category.

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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