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The FAA is adopting a new airworthiness directive (AD) for all Airbus Canada Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. This AD was prompted by a design review that discovered software protection logic for potential large leaks from the engine bleed duct inside the engine core compartments was partially impaired. This AD requires revising the existing airplane flight manual (AFM) to incorporate the procedures for the flightcrew to manually isolate the opposite functional engine in the event of an engine bleed duct large leak condition, as specified in a Transport Canada AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.
Published
Mar 18, 2025
Effective
Apr 22, 2025
Citation
90 FR 12457
Agencies
2
Full text not available in our database.
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Docket No. FAA-2024-2554
Project Identifier MCAI-2024-00492-T
Amendment 39-22989
AD 2025-06-01
2120-AA64
14 CFR 39