AD 2026-03-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | SAS | Airworthiness Directives; Airbus SAS Airplanes |
Unsafe Condition
Occurrences of electronic centralized aircraft monitor (ECAM) messages requiring flight control remote module (FCRM) replacement have been reported, and further investigation identified an issue linked to solder structural fatigue. This condition, if not corrected, could lead to failure of a flight control actuator, possibly resulting in reduced control of the airplane.
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Required Actions
Replace each affected part with a serviceable part within the applicable compliance time specified in table 1 of EASA AD 2025-0008, except as provided by paragraph (h)(1) of this AD. Test each installed serviceable part in accordance with paragraph 3.E. of the Airbus service bulletin and limit the installation of affected parts under certain conditions.
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Compliance Time
Before exceeding the life limit of 9,000 flight cycles (FC) or 50,000 flight hours (FH), whichever occurs first.
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Affected Aircraft
All Airbus SAS Model A350-941 and -1041 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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