EASA Regulations for MHI RJ Aviation CL-600 (Regional Jet)

84 airworthiness directives and regulations affecting MHI RJ Aviation CL-600 (Regional Jet).

EASA AD CF-2020-09

Apr 14, 2020

Landing Gear — General — Nose Landing Gear and Main Landing Gear Components Repaired by Bombardier Repair Engineering Orders Affected by Specific Airworthiness Limitation.

Airworthiness Directive CF-2020-09 is issued by Transport Canada and applies to Bombardier Inc. model CL-600-2B19 aeroplanes, serial numbers 7003 through 8999. It addresses issues with nose landing gear (NLG) and main landing gear (MLG) components repaired by Bombardier Repair Engineering Orders that were missing specific airworthiness limitation structural deviation inspection requirements. The directive mandates verification and corrective actions to ensure compliance with revised life limits for these components.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2020-08

Apr 7, 2020

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

Mar 9, 2020

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

Dec 12, 2019

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

Nov 18, 2019

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-2019-41

Nov 18, 2019

Ice and Rain Protection — Wing Anti-Ice System — Additional Operating Limitations

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.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2019-40

Nov 6, 2019

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-2002-39R2

Aug 2, 2019

Fuselage Pressure Floor Skin

Airworthiness Directive CF-2002-39R2 addresses the fuselage pressure floor skin on Bombardier Inc. model CL-600-2B19 aeroplanes, serial numbers 7003 through 8999. This directive mandates revised inspection requirements to detect and correct fatigue cracks that could lead to rapid decompression during flight. It updates maintenance schedules and inspection tasks to enhance structural safety of the affected aircraft.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2019-22

Jun 11, 2019

Electrical Power - Electrical Wires Chafing With Auxiliary Aft Cabin Fuel Tank Bracket

Canadian Airworthiness Directive CF-2019-22 addresses an electrical wiring issue on Bombardier Inc. CL-600-2B19 aircraft. The directive targets specific serial numbers of this model where generator power cables may chafe against the auxiliary aft cabin fuel tank bracket. This condition could lead to electrical short circuits and generator malfunctions.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2019-20R1

Jun 3, 2019

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-2019-21

May 22, 2019

Wing Structure — Lower Wing Plank — Cracking at Stringer Run-out

The Canadian Airworthiness Directive CF-2019-21 addresses fatigue cracking detected in the lower wing plank at the stringer run-out area on Bombardier Inc. CL-600-2B19 aircraft, serial number 7003 and later. This directive mandates updated inspection procedures to detect potential cracks in the right lower wing plank to ensure structural integrity. It applies specifically to the wing structure of these Bombardier regional jets.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2016-19R2

Apr 26, 2019

Cold Weather Operations — Introduction of Low Temperature Ground Wing Anti-Ice System

The Canadian Airworthiness Directive CF-2016-19R2 addresses cold weather operations for Bombardier Inc. model CL-600-2B19 aeroplanes, serial numbers 7003 and subsequent. It mandates the installation of a Low Temperature Ground Wing Anti-Ice System to prevent wing contamination during ground operations in cold weather. This directive updates previous revisions and includes maintenance and flight manual changes to enhance take-off safety.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2015-28R2

Feb 7, 2019

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 2018-0259R1

Feb 7, 2019

Information Systems – Electronic Flight Bag Universal Serial Bus Receptacle – Modification

EASA Airworthiness Directive 2018-0259R1 is an updated directive addressing safety concerns related to USB receptacles installed in various aircraft including Fokker F27 and F28 models, Airbus A318 through A340 series, ATR42 and ATR72, Boeing 737 through 777, and Bombardier CL-600 and DHC-8 aircraft. The directive mandates modifications to the affected Lone Star Aviation USB receptacle part number LS03-05050-A to prevent overheating and smoke/fumes in the cockpit. It applies to aircraft with these USB receptacles installed via Fokker Services Supplemental Type Certificates, Service Bulletins, or minor modifications.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • ATR ATR42
  • ATR ATR72
  • Boeing 737
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Bombardier CL-600 (Challenger)
  • De Havilland Canada DHC-8
  • Fokker CRR-0185
  • Fokker CRR-0186
  • Fokker CRR-0190
  • Fokker CRR-0210
  • Fokker CRR-0241
  • Fokker CRR-0265
  • Fokker CRR-0300
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Fokker F27
  • Fokker F28
  • Boeing 747
  • Bombardier CL-600
  • Bombardier DHC-8

EASA AD CF-2018-31

Dec 11, 2018

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

Nov 12, 2018

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

Oct 10, 2018

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

Jul 23, 2018

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-2018-17

Jul 9, 2018

Stall Protection System — Out of Tolerance Angle of Attack Transducers

Canadian Airworthiness Directive CF-2018-17 addresses the stall protection system on Bombardier Inc. model CL-600-2B19 aeroplanes, specifically those with serial numbers 7003 through 7067 and 7069 through 7891 equipped with Angle of Attack (AOA) Transducers part numbers 45-150-340, C16258AA, and C16258AB. This directive mandates actions to ensure the accuracy of AOA transducers to maintain proper stall protection system function. It aims to prevent potential loss of control due to late stall protection activation caused by erroneous AOA signals.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2B19

EASA AD CF-2014-44R2

Feb 27, 2018

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