Flight Controls — Elevator and Rudder Rod Ends of the Power Control Units
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Affected operators must cease using specified outdated maintenance tasks within 30 days of the effective date and amend their maintenance planning manuals accordingly within 30 to 90 days depending on aircraft model and utilization. For certain aircraft, initial inspections of the elevator PCU rod ends must be completed within defined flight hour limits, with a second inspection required for some aircraft before reaching 3400 hours air time. All actions must comply with the detailed instructions in the referenced service bulletin and Transport Canada-approved manuals.
Summary
The Canadian Airworthiness Directive CF-2018-29 addresses flight control safety issues related to elevator and rudder rod ends of the Power Control Units on Bombardier Inc. aeroplanes, including models CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25. It mandates revised maintenance tasks and inspections to detect pitting corrosion and prevent rod end fractures that could compromise control surface functionality. This directive applies to specific serial numbers within these models and aims to enhance operational safety.
What changed
CF-2018-29 introduces new maintenance schedule amendments prohibiting the use of certain outdated Aircraft Maintenance Manual tasks and requires incorporation of updated inspection tasks into maintenance programs. It also mandates initial and follow-up inspections of elevator PCU rod ends for aircraft not operating under the Low Utilization Maintenance Program, with specific compliance times based on aircraft hours. These measures are new requirements to address corrosion-induced rod end fractures.
Why it matters
This directive is critical for aviation professionals to prevent potential loss of control surface function or inadequate flutter suppression caused by PCU rod end failures. Operators and maintenance organizations must update their maintenance manuals and perform timely inspections to detect corrosion early, ensuring continued airworthiness and flight safety. Compliance helps avoid in-service failures that could lead to serious flight control issues.
More for MHI RJ Aviation CL-600 (Regional Jet)
All 84- EASA AD CF-2026-48Pneumatic – 10th and 14th Stage Bleed Duct Damaged or Missing InsulationOct 7, 2026
- 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-2026-09R1Ice and Rain Protection – Engine Cowl Anti-Ice – Ejector Pipe ChafingJun 22, 2026
- EASA AD CF-2026-07R1
Get the next one by email
New ADs and bulletins for these 6 aircraft types, summarized like this page, every Monday.