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EASA Regulations for Bombardier CL-600-2D15

20 airworthiness directives and regulations affecting Bombardier CL-600-2D15.

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New ADs and bulletins for Bombardier CL-600-2D15, summarized like the ones below, every Monday.

EASA AD CF-2022-16R1

Pneumatic — Non-Conforming Bleed Air Leak Detection System Sensing Elements

Canadian Airworthiness Directive CF-2022-16R1 addresses non-conforming bleed air leak detection system sensing elements installed on MHI RJ Aviation ULC aircraft, including Bombardier CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 models. The directive mandates testing and replacement of sensing elements with insufficient salt fill that could fail to detect hot bleed air leaks, posing a safety risk. It references specific MHIRJ Service Bulletins SB 601R-36-021 and SB 670BA-36-025 for compliance procedures.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2021-19

Navigation System — Uncommanded Heading Change from Magnetic to True

Canadian Airworthiness Directive CF-2021-19 addresses an issue with uncommanded heading changes from magnetic to true on MHI RJ Aviation ULC aircraft, including Bombardier models CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 equipped with specific inertial reference system part numbers. The directive mandates updates to the Airplane Flight Manual to include revised abnormal procedures related to instrument systems. This AD aims to enhance flight safety by mitigating misleading heading information on primary flight and multi-function displays.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2020-08

Ice and Rain Protection — Wing Anti-Ice System — Introduction of Safe Life Limit for Pneumatic Telescopic Duct

The Airworthiness Directive CF-2020-08 is issued by Transport Canada and addresses the Wing Anti-Ice (WAI) system on Bombardier Inc. model CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. It introduces a safe life limit for the pneumatic telescopic duct used in the WAI system to prevent failures that could affect aircraft safety. This directive mandates maintenance updates to ensure continued airworthiness of the affected aircraft.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2020-03

Fuel System - Primary Ejector Fuel Feed Flexible Hoses Inner Tube Cracking

The Canadian Airworthiness Directive CF-2020-03 addresses cracking in the inner tube of primary ejector fuel feed flexible hoses on Bombardier aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 within specified serial number ranges. This directive mandates replacement of affected flexible hoses that may have a thinner-than-required Teflon lining, which can lead to fuel leaks and potential engine flameouts. The directive aims to ensure continued safe operation by mitigating fuel system failures related to these components.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2019-44

Maintenance Requirements Manual — Introduction of New Appendix A2-00 — Candidate Certification Maintenance Requirements Interval Limitations

Maintenance Requirements Manual — Introduction of New Appendix A2-00 — Candidate Certification Maintenance Requirements Interval Limitations is a Canadian Airworthiness Directive (AD CF-2019-44) that applies to Bombardier Inc. models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aeroplanes. This directive mandates the incorporation of a new appendix into the Maintenance Requirements Manual to establish Candidate Certification Maintenance Requirements (CCMR) interval limitations as Airworthiness Limitations. It ensures operators maintain compliance with updated maintenance intervals to uphold aircraft safety.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2019-42

Flight Controls — Rudder Control System — Rudder Feel Unit Shaft Fracture

Canadian Airworthiness Directive CF-2019-42 addresses a safety issue in Bombardier Inc. aeroplanes including models CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2C11. The directive concerns the rudder control system, specifically the rudder feel unit shaft, which has been found to fracture due to fatigue. This fracture could lead to loss of rudder feel and affect aircraft controllability.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2C11

EASA AD CF-2019-40

Navigation System — Flight Management System, Inertial Reference System and Attitude and Heading Reference System — Outdated Magnetic Variation Tables

Navigation System — Flight Management System, Inertial Reference System and Attitude and Heading Reference System — Outdated Magnetic Variation Tables is a Canadian Airworthiness Directive (CF-2019-40) issued by Transport Canada. It applies to Bombardier Inc. aircraft models CL-600-2B19, CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive addresses outdated magnetic variation tables used in navigation systems that may cause inaccurate magnetic heading displays and positioning errors.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2C11
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2019-20R1

Decompression Panel — Flight Compartment Door — Upper Panel

Airworthiness Directive CF-2019-20R1 is issued by Transport Canada and applies to Bombardier Inc. model CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 aircraft. This directive addresses the incorrect installation of cockpit door edge protection plates on the upper decompression panel, which could prevent the panel from opening during rapid decompression. The directive mandates maintenance schedule updates to ensure the decompression panel functions correctly.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2015-28R2

Equipment / Furnishings — Damaged Decompression Window Louver Panel Assemblies and Detached Blowout Panels

Airworthiness Directive CF-2015-28R2 addresses damaged decompression window louver panel assemblies and detached blowout panels on Bombardier Inc. aeroplanes, specifically models CL-600-2B19, CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25 configured with a Class C Cargo Compartment. This directive mandates inspections and corrective actions to ensure the integrity of cargo compartment components that are critical for smoke detection and fire suppression. The directive updates maintenance requirements to prevent uncontrolled cargo compartment fires.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2018-31

Landing Gear System — Alternate Extension System — Introduction of New Airworthiness Limitation

Canadian Airworthiness Directive CF-2018-31 mandates a new airworthiness limitation for the landing gear system's alternate extension system on Bombardier Inc. model CL-600-2C10, CL-600-2D15, and CL-600-2D24 aircraft. This directive introduces a new maintenance requirement to ensure the operational reliability of the alternate extension system. It applies to these specific Bombardier regional jets and aims to enhance safety through updated inspection intervals.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24

EASA AD CF-2018-29

Flight Controls — Elevator and Rudder Rod Ends of the Power Control Units

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.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2018-25

Fuselage — AFT Fuselage Fitting Not Heat Treated

Canadian Airworthiness Directive CF-2018-25 addresses an issue with aft fuselage fittings on certain Bombardier Inc. aircraft models CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive mandates inspection and replacement of affected fittings that were not heat treated as required. This ensures the structural integrity of the aircraft fuselage and prevents potential failures.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2016-14R1

Fuselage — Excessive Tape on Floor Structure - Inspection

Airworthiness Directive CF-2016-14R1 is issued by Transport Canada and applies to Bombardier Inc. aircraft models CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive addresses the issue of excessive polyurethane tape on the floor structure of these aircraft, which may not meet flammability requirements and could allow fire propagation beneath the floor. It mandates inspection and trimming of any overhanging tape on the floor structural members.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2014-44R2

Flight Controls — Elevator Control System — Disconnect

The Canadian Airworthiness Directive CF-2014-44R2 addresses the elevator control system disconnect issue on Bombardier Inc. Model CL-600-2C10, CL-600-2D15, and CL-600-2D24 aeroplanes. This directive mandates replacement and inspection of elevator lever assemblies and control rods to prevent uncommanded elevator movements that could compromise aircraft controllability and structural integrity.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24

EASA AD CF-2012-10R1

Non-Conforming Wing-to-Fuselage Attachment Nuts

The Canadian Airworthiness Directive CF-2012-10R1 addresses non-conforming wing-to-fuselage attachment nuts on Bombardier aircraft models CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25. It mandates inspections of specific wing-to-fuselage attachment nuts that lack the required double locking feature, which could lead to nut loosening and potential wing detachment. This directive applies to aircraft with serial numbers starting from 10002 for CL-600-2C10, 15001 for CL-600-2D15 and CL-600-2D24, and 19001 for CL-600-2E25.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2018-02

Landing Gear — Main Landing Gear Orifice Support Tube Fracture

Canadian Airworthiness Directive CF-2018-02 addresses the risk of fracture in the Main Landing Gear Orifice Support Tube (MLG OST) on Bombardier Inc. aeroplanes, specifically models CL-600-2C10, CL-600-2D15, CL-600-2D24, and CL-600-2E25. The directive mandates replacement of the existing MLG OST with a redesigned part and introduces a new airworthiness limitation task to ensure ongoing safety and structural integrity.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2018-03

Oxygen System — Cabin Crew and Lavatory Oxygen Masks Deployed Tangled

Canadian Airworthiness Directive CF-2018-03 addresses an issue with oxygen systems on Bombardier Inc. aeroplanes, specifically models CL-600-2B19, CL-600-2C10, CL-600-2D15/CL-600-2D24, and CL-600-2E25. The directive focuses on the tangled deployment of cabin crew and lavatory oxygen masks caused by incorrect packing of oxygen box assemblies. This AD mandates repacking and modification of affected oxygen box assemblies to ensure proper oxygen mask deployment during emergencies.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA AD CF-2017-38

Landing Gear — Main Landing Gear — Piston Axle Corrosion

Canadian Airworthiness Directive CF-2017-38 addresses corrosion issues on the piston axle of the main landing gear in Bombardier Inc. aircraft models CL-600-2C10 (serial 10002 and later), CL-600-2D15, CL-600-2D24 (serial 15001 and later), and CL-600-2E25 (serial 19001 and later). The directive mandates inspections to detect damage to the protective coating and corrosion that could lead to axle separation. It introduces maintenance requirements to ensure continued airworthiness of the affected landing gear components.

Airworthiness Directive

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24
Bombardier CL-600-2E25

EASA SIB AV-2010-02

Bombardier Inc. - Aft Nose Landing Gear Door Upper Attachment Hinge Assemblies

Transport Canada Civil Aviation Service Difficulty Advisory AV-2010-02 addresses a potential issue with the aft nose landing gear door upper attachment hinge assemblies on Bombardier Inc. CL-600-2C10, CL-600-2D15, and CL-600-2D24 aircraft. The advisory highlights incidents where a self-locking nut backing out caused hinge pin disengagement, leading to door binding and damage during landing gear extension. Bombardier has issued temporary maintenance manual revisions to mitigate this issue.

Safety Information Bulletin

Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24

EASA SIB 2008-12

CANCELLED - REPLACED BY TRANSPORT CANADA AD CF-2008-14

The EASA Safety Information Notice No. 2008-12, issued on 2008-02-27, addresses the identification and removal from service of Air Driven Generator Power Centre Contactors on Bombardier, Inc. Model CL-600-2C10, CL-600-2D15, and CL-600-2D24 aircraft. This notice references Transport Canada Airworthiness Directive CF-2008-14 and Bombardier Aerospace Service Bulletin 670BA-24-021 Revision A. It informs aviation stakeholders about a safety issue related to manufacturing defects affecting these aircraft models.

Airworthiness Directive

Bombardier CL-600-2C10
Bombardier CL-600-2D15
Bombardier CL-600-2D24