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EASA Regulations for Bombardier BD-700-1A10

41 airworthiness directives and regulations affecting Bombardier BD-700-1A10.

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New ADs and bulletins for Bombardier BD-700-1A10, summarized like the ones below, every Monday.

EASA AD CF-2024-27

Flight Controls — Incorrect Airplane Flight Manual Approach Speed Adder and Landing Distance Factors for SLAT-FLAP FAIL Caution Crew Alerting System Message and Jammed or Inoperative Slat/Flap Control Lever

Airworthiness Directive CF-2024-27 is issued by Transport Canada and addresses incorrect approach speed adders and landing distance factors in the Airplane Flight Manual (AFM) for Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft models. This directive applies to specific serial numbers of these models and corrects errors related to the SLAT-FLAP FAIL caution Crew Alerting System message and jammed or inoperative Slat/Flap Control Lever procedures. The directive mandates updates to the AFM to ensure accurate performance data is used during approach and landing.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2024-07

Hydraulic Power — Engine Driven Pump Hydraulic Hoses Fouling with Pylon

Canadian Airworthiness Directive CF-2024-07 addresses hydraulic power issues related to engine driven pump hydraulic hoses fouling with the pylon on Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aircraft, specifically serial numbers 60001 through 60076, 60083, 60087, and 60089. The directive mandates inspections and corrective actions to prevent hydraulic hose chafing that could lead to system leaks and failures. This AD aims to maintain the integrity of hydraulic systems No. 1 and No. 2 on these aircraft.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD 2022-0110R1

Engine — Low Pressure Compressor Rotor (Fan) Disc — Inspection

EASA Airworthiness Directive 2022-0110R1 is a regulatory update addressing inspection requirements for low pressure compressor rotor (fan) discs on Rolls-Royce Deutschland BR700-710 series engines. This directive applies to engines installed on aircraft such as Bombardier BD-700-1A10, BD-700-1A11, Gulfstream G500, and G550. It mandates inspections to detect cracks that could lead to fan disc or blade failure, posing safety risks.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg BR700-710
Bombardier BD-700-1A10
Bombardier BD-700-1A11
Gulfstream G500
Gulfstream G550

EASA AD CF-2020-29R1

Flight Controls — Elevator Control System — Vertical Torque Tube Seizure — Sand Contamination of Bearing

The Airworthiness Directive CF-2020-29R1 titled "Flight Controls — Elevator Control System — Vertical Torque Tube Seizure — Sand Contamination of Bearing" applies to Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9001 through 60081. It addresses contamination and corrosion of elevator torque tube bearings caused by sand, which can restrict free rotation and potentially lead to loss of pitch control. This directive mandates inspections and maintenance tasks to ensure continued safe operation of the elevator control system.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-65

Time Limits / Maintenance Checks (TLMC) — TLMC Manual Revision to Introduce New or Revised Tasks Affecting the Main Landing Gear (MLG), Nose Landing Gear (NLG) and Pitch Trim Actuator

Canadian Airworthiness Directive CF-2023-65 mandates revisions to the Time Limits/Maintenance Checks (TLMC) manual for Bombardier BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9001 through 9879, 9998, and 60001 through 60065. The directive introduces new or revised maintenance tasks affecting the Main Landing Gear (MLG), Nose Landing Gear (NLG), and Pitch Trim Actuator. These changes are required to ensure continued airworthiness and safety of the affected aircraft models.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-44

Navigation — Minimum Equipment List (MEL) Item Prohibition in the Presence of 5G C-Band Wireless Broadband Interference

Canadian Airworthiness Directive CF-2023-44 addresses navigation Minimum Equipment List (MEL) item prohibitions related to 5G C-Band wireless broadband interference for Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft. It updates previous directives by refining operational restrictions in U.S. airspace where 5G interference affects radio altimeters. The directive clarifies conditions under which dispatch is prohibited based on aircraft radio altimeter tolerance and airport 5G deployment status.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-42

Wings — Inboard Flap Seal Plate Lost or Damaged

Canadian Airworthiness Directive CF-2023-42 addresses the issue of lost or damaged inboard flap seal plate assemblies on Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft, specifically affecting certain serial numbers. The directive mandates inspections and replacement of the flap seal plate assemblies to prevent potential in-flight detachment and subsequent aircraft damage.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-25

Doors — Passenger Door — Detent Mechanism Aircraft Maintenance Manual Procedure

Airworthiness Directive CF-2023-25 is a Canadian regulatory document addressing the passenger door detent mechanism on Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9002 through 60065. It mandates revisions to the Aircraft Maintenance Manual procedure for the functional test of the passenger door mechanism to include inspections that were previously omitted. This directive aims to enhance safety by preventing latent failures that could lead to door opening during unpressurized flight.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-17

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

Canadian Airworthiness Directive CF-2023-17 addresses a safety issue with non-conforming bleed air leak detection system sensing elements on Bombardier BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9002 through 9879, 9998, and 60001 and subsequent. The directive mandates testing and replacement of sensing elements that may have insufficient salt fill, which could impair detection of hot bleed air leaks. This AD supersedes previous directives CF-2022-38 and CF-2022-38R1 and incorporates Bombardier service bulletins for corrective actions.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2023-02

Landing Gear — Nose Landing Gear — Steering Shutoff Valve Slow to Deactivate

Canadian Airworthiness Directive CF-2023-02 addresses an issue with the nose landing gear steering shutoff valve on Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes, serial numbers 9002 through 9998 and 60001 through 60068. The directive mandates replacing the existing steering selector valve part number 23600-101 with a redesigned valve part number 23600-103 to improve response time. This AD aims to prevent runway excursions caused by slow deactivation of the steering valve under low temperature conditions.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-60

Superseded by TCCA AD CF-2023-44

The Canadian Airworthiness Directive CF-2022-60 addresses the impact of 5G C-band wireless technology interference on Bombardier BD-700-1A10 and BD-700-1A11 aircraft models. It mandates modifications to the aircraft flight manual (AFM) and restricts the use of certain minimal equipment list (MMEL) items to mitigate radio altimeter signal disruptions caused by 5G signals. This directive aims to ensure safe aircraft operation during takeoff, approach, and landing phases in airspace where 5G C-band deployment affects radio altimeter reliability.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-53

Landing Gear — Brake Control System — Uncommanded Brake Pressure due to Brake Control Unit Failure

Canadian Airworthiness Directive CF-2022-53 addresses an issue with the landing gear brake control system on Bombardier BD-700-1A10 and BD-700-1A11 aircraft models. The directive targets uncommanded brake pressure caused by a failure in the Brake Control Unit (BCU), which can lead to tire bursts and braking difficulties. It mandates inspection and replacement of affected BCUs to ensure safe braking performance.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-49

Information Systems — Incorrect Airplane Flight Manual (AFM) Wet and Contaminated Runway Stopping Distance

Information Systems — Incorrect Airplane Flight Manual (AFM) Wet and Contaminated Runway Stopping Distance is a Canadian Airworthiness Directive (CN CF-2022-49) addressing incorrect stopping distance data in the AFM for Bombardier BD-700-1A10 and BD-700-1A11 aircraft. The directive mandates corrections to specific performance tables related to wet and contaminated runway landing distances. It applies to certain serial numbers of these Bombardier Global 6000 and Global 5000 models.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-38R1

Pneumatic – Non-Conforming Bleed Leak Detection System Sensing Elements

Airworthiness Directive CF-2022-38R1 is issued by Transport Canada and applies to Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes with specific serial numbers. It addresses a safety issue involving non-conforming bleed air leak detection system sensing elements that may have insufficient salt fill, potentially preventing detection of hot bleed air leaks. The directive mandates operational restrictions and maintenance actions to mitigate the risk of undetected bleed air leaks.

Airworthiness DirectiveSuperseded

Bombardier BD-7001A101A11

EASA AD CF-2022-40

Wings — Revised Non-Destructive Testing Manual Procedure for Airworthiness Limitation Task Number 57-51-00-109

Wings — Revised Non-Destructive Testing Manual Procedure for Airworthiness Limitation Task Number 57-51-00-109 is a Canadian Airworthiness Directive (CF-2022-40) affecting Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft with specific serial numbers. It mandates the use of a revised non-destructive testing procedure to ensure proper inspection of the metal ribs at the ends of the inner, middle, and outer flaps. This directive aims to prevent undetected cracks that could lead to structural failure of the flaps.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-30

Flight Controls — Flap Fail on Approach

Canadian Airworthiness Directive CF-2022-30 addresses a flap, slat, or slat-flap failure issue on approach for Bombardier BD-700-1A10 and BD-700-1A11 aircraft models. The directive mandates revisions to the Airplane Flight Manual (AFM) and Quick Reference Handbook (QRH) to modify procedures related to flap failure warnings. This AD aims to prevent unexpected stall warnings and stick shaker activation caused by resetting the slat flap control unit during flight.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-25

Landing Gear — Introduction of New Brake Accumulator Life Limit

Canadian Airworthiness Directive CF-2022-25 introduces a new brake accumulator life limit for Bombardier BD-700-1A10 and BD-700-1A11 aircraft, serial numbers 9002 through 9998 and 60001 through 60046. This directive updates maintenance requirements to prevent brake accumulator failures that could lead to loss of hydraulic pressure and braking capability. It supersedes the previous AD CF-2022-14 and corrects certain service bulletin references.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-15

Time Limits / Maintenance Checks — Introduction of Certification Maintenance Requirements

Canadian Airworthiness Directive CF-2022-15 introduces new Certification Maintenance Requirements (CMRs) for Bombardier Inc. model BD-700-1A10 and BD-700-1A11 aeroplanes with specific serial numbers. This directive mandates updates to maintenance schedules to include new tasks related to landing gear emergency extension, brake shutoff valve operation, and passenger door vent-flap mechanism checks. The directive aims to enhance safety by addressing maintenance tasks that have reached escalation limits.

Airworthiness Directive

Bombardier BD-7001A101A11

EASA AD CF-2022-14

Landing Gear – Introduction of New Brake Accumulator Life Limit

Canadian Airworthiness Directive CF-2022-14 introduces new brake accumulator life limits for Bombardier BD-700-1A10 and BD-700-1A11 aircraft, specifically serial numbers 9002 through 9998 and 60001 through 60046. This directive mandates updates to maintenance schedules to incorporate these life limits for specific brake accumulator part numbers GW415-1250-1 and GW415-1200 series. It aims to prevent brake accumulator failures that could lead to loss of hydraulic pressure and reduced braking capability.

Airworthiness DirectiveSuperseded

Bombardier BD-7001A101A11

EASA AD CF-2021-41

Doors — Passenger Door — Rapid Opening

The Canadian Airworthiness Directive CF-2021-41 titled "Doors — Passenger Door — Rapid Opening" applies to Bombardier Inc. BD-700-1A10 and BD-700-1A11 aircraft with serial numbers 9002 to 9998 and 60001 to 60045. This directive addresses issues related to the rapid opening of passenger doors that can cause significant damage and safety risks. It mandates the use of revised Aircraft Maintenance Manual (AMM) tasks to ensure proper maintenance of the passenger doors.

Airworthiness Directive

Bombardier BD-7001A101A11