Ice and Rain Protection — Wing Anti-Ice System — Additional Operating Limitations
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of Bombardier CL-600-2B19 aircraft must incorporate the approved AFM revisions specified in AFM CSP A-012, Revision 72 or later, within 30 days of the directive's effective date. They must also brief all flight crews on the updated wing anti-ice operating procedures. Compliance with these actions is mandatory to continue legal flight operations.
Summary
Canadian Airworthiness Directive CF-2019-41 addresses additional operating limitations for the wing anti-ice system on Bombardier Inc. CL-600-2B19 aircraft. This directive mandates changes to the Airplane Flight Manual to ensure the wing anti-ice system is activated under specific conditions to prevent ice accumulation on wing leading edges. The directive aims to enhance safety by mitigating risks associated with undetected ice during landing.
What changed
CF-2019-41 introduces revised Airplane Flight Manual procedures requiring the wing anti-ice system to be selected ON at airspeeds above 230 knots, correcting previous guidance that did not mandate this. It mandates incorporation of these changes into the AFM chapters related to operating limitations and normal procedures. Flight crews must be informed of these procedural updates to ensure compliance.
Why it matters
This directive is critical for operators and maintenance teams to prevent wing stall incidents caused by ice accumulation during landing. Ensuring the wing anti-ice system is used correctly reduces the risk of uncommanded roll and enhances flight safety. Compliance teams must update manuals and train crews to meet regulatory requirements and avoid operational hazards.
More for MHI RJ Aviation CL-600 (Regional Jet)
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- EASA AD CF-2026-43Ice and Rain Protection – Wing Anti-Ice – Aircraft Flight Manual Procedure Anomaly - AmendmentSep 11, 2026
- EASA AD CF-2026-09R2Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe ChafingAug 5, 2026
- EASA AD CF-2026-07R1Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe ChafingJun 22, 2026
- EASA AD CF-2026-09R1
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