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EASA Regulations for Fokker F28 Mark 0100

19 airworthiness directives and regulations affecting Fokker F28 Mark 0100.

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New ADs and bulletins for Fokker F28 Mark 0100, summarized like the ones below, every Monday.

EASA AD 2024-0192

Landing Gear — Main Landing Gear Piston — Inspection

EASA Airworthiness Directive 2024-0192 is issued for Fokker F28 Mark 0070 and Mark 0100 aeroplanes equipped with Collins Aerospace main landing gear pistons having part numbers 41050-7 to -16 or 41060-3 to -6, except those already modified by Fokker Services Service Bulletin SBF100-32-172. This directive mandates inspections of the main landing gear piston, specifically targeting pistons modified by Aerospace NDI Pty Ltd with part number 41141-5, to detect cracks caused by stress corrosion. The directive aims to prevent structural failure and potential collapse of the main landing gear during operation.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2024-0176

Landing Gear – Main Landing Gear Piston – Inspection

EASA Airworthiness Directive 2024-0176 is issued for Fokker F28 Mark 0070 and Mark 0100 aeroplanes equipped with Collins Aerospace main landing gear pistons having specific part numbers. The directive addresses a crack found in the main landing gear piston modified by an Australian landing gear shop, which could lead to structural failure and landing gear collapse. It mandates inspections and replacement of affected parts to ensure continued airworthiness.

Airworthiness DirectiveSuperseded

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2024-0123

Landing Gear — Hydraulic Line Restrictor Check Valve — Replacement

EASA Airworthiness Directive 2024-0123 is issued for Fokker Services B.V. F28 Mark 0070 and Mark 0100 aeroplanes. It addresses the replacement of hydraulic line restrictor check valves in the main landing gear hydraulic system to ensure continued airworthiness and safety. The directive applies to specific part numbers of restrictor check valves installed in the hydraulic return line of the parking brake shut-off valve.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2024-0043

Wings — Outer Wing Stringers and Stringer Joint Pieces — Inspection

EASA Airworthiness Directive 2024-0043 is an airworthiness directive addressing inspection requirements for the outer wing stringers and stringer joint pieces on Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates a one-time special detailed inspection using high frequency eddy current techniques to detect cracks in specific wing areas. The directive applies to all serial numbers of these aircraft models with 34,000 or more flight cycles since entry into service.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2023-0005-CN

CANCELLED: Fuselage — Stubwing Upper Skin — Inspection / Repair

EASA Airworthiness Directive 2023-0005-CN is a cancellation notice affecting Fokker Services B.V. F28 Mark 0070 and Mark 0100 aeroplanes. It cancels a previous Dutch AD related to inspection and repair of the fuselage stubwing upper skin due to bleed air leakage concerns. The directive confirms that updated maintenance manuals and structural repair procedures now adequately address the safety issues.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2022-0070

Fuselage — Stubwing Bay Area Skin — Inspection

EASA Airworthiness Directive 2022-0070 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates inspections of the fuselage stubwing bay area skin to detect cracks related to heat damage repairs. The directive aims to ensure continued structural integrity of the affected aircraft.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2022-0027

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Airworthiness Limitations Items and Safe Life Items – Implementation

EASA Airworthiness Directive 2022-0027 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates compliance with updated Airworthiness Limitations Items and Safe Life Items as specified in Fokker Services Engineering Report SE-623 issue 21. The directive ensures continued airworthiness by requiring operators to implement maintenance tasks and life limits according to the latest approved instructions.

Airworthiness DirectiveSuperseded

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2021-0059

Wings — Front Spar Lower Boom — Inspection

EASA Airworthiness Directive 2021-0059 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates inspection of the wing front spar lower boom for corrosion on aircraft that completed a specific maintenance task before 2015. The directive aims to ensure continued structural integrity of the wing by detecting and correcting corrosion issues.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2020-0238

Airplane Flight Manual — Section Abnormal Procedures — Amendment

EASA Airworthiness Directive 2020-0238 is an amendment to the Airplane Flight Manual (AFM) Section on Abnormal Procedures for Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses a safety issue related to the cabin pressurization control fault procedure following an incident where a passenger door opened under residual cabin pressure after landing. This directive mandates updates to the AFM to improve the procedure and prevent similar occurrences.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2020-0024

Time Limits / Maintenance Checks – ALS Part 2 – Airworthiness Limitations Items and Safe Life Items – Implementation

EASA Airworthiness Directive 2020-0024 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates compliance with updated Airworthiness Limitation Items and Safe Life Items as specified in Fokker Services Engineering Report SE-623 issue 19. This directive ensures continued airworthiness by requiring operators to implement maintenance tasks and life limits defined in the updated Airworthiness Limitations Section.

Airworthiness DirectiveSuperseded

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2020-0002

Fuselage — Frame Inboard Boom — Inspection

EASA Airworthiness Directive 2020-0002 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0100 aeroplanes with serial numbers 11244 to 11371 inclusive. The directive mandates inspection of the fuselage frame inboard boom at fuselage station 17011 to detect cracks that could compromise structural integrity. It requires operators to perform a detailed inspection and report the findings to Fokker Services.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0100

EASA AD 2019-0224

Landing Gear — Main Landing Gear / Piston — Inspection / Replacement / Modification

EASA Airworthiness Directive 2019-0224 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses inspection, replacement, and modification requirements for main landing gear (MLG) pistons, specifically parts with P/N 41141-3, 41141-5, and 41141-7, to prevent cracking and potential landing gear failure. The directive mandates actions to ensure the continued airworthiness of affected landing gear components.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2019-0162

Fuselage — Bottom Skin — Inspection

EASA Airworthiness Directive 2019-0162 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates inspection of the fuselage bottom skin to detect corrosion, cracks, bulges, or missing fasteners that could compromise structural integrity. The directive requires reporting inspection results to Fokker Services and applying repairs if defects are found.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2019-0120

Electrical Power — Power Transfer Contactors — Replacement

EASA Airworthiness Directive 2019-0120 is an official regulatory document addressing electrical power transfer contactors on Fokker Services B.V. F28 Mark 0100 aeroplanes. It mandates the replacement of specific generator, essential bus, and auxiliary power transfer contactors with new parts to prevent smoke and electrical power loss in the cockpit.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0100

EASA AD 2019-0095

Equipment / Furnishings — Lavatory Waste Bins / Fire Extinguishers — Inspection / Modification / Replacement

EASA Airworthiness Directive 2019-0095 is an airworthiness directive addressing Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It focuses on the inspection, modification, and replacement of lavatory waste bins and fire extinguishers to prevent interference that could cause fire extinguisher failure. The directive applies to specific lavatory waste bin part numbers and fire extinguishers with certain part numbers installed on these aircraft.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2019-0037

Landing Gear — Nose Landing Gear Turning Tube Assembly — Replacement

EASA Airworthiness Directive 2019-0037 is an airworthiness directive addressing the nose landing gear turning tube assemblies on Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates the replacement of certain affected nose landing gear turning tube assemblies with serviceable parts to ensure continued airworthiness. The directive applies to parts with specific part numbers installed on these aircraft models.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2018-0159

Time Limits / Maintenance Checks – ALS Part 2 – Airworthiness Limitations Items and Safe Life Items – Implementation

EASA Airworthiness Directive 2018-0159 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates the implementation of updated maintenance tasks and airworthiness limitations as specified in Fokker Services Engineering Report SE-623 issue 18. This directive ensures continued airworthiness by requiring compliance with the latest Airworthiness Limitations Section Part 2.

Airworthiness DirectiveSuperseded

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2018-0122

Placards and Markings — Auxiliary Power Unit Air Intake — Introduction

EASA Airworthiness Directive 2018-0122 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It addresses safety concerns related to the auxiliary power unit (APU) air intake, specifically to prevent uncontained APU turbine rotor rim failures during de-/anti-icing operations. The directive mandates installation of specific placards and markings near the APU air intake to warn ground personnel.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100

EASA AD 2018-0001

Landing Gear — Main Landing Gear Retraction Actuator — Inspection

EASA Airworthiness Directive 2018-0001 is an airworthiness directive addressing the inspection of the main landing gear retraction actuators on Fokker F28 Mark 0070 and Mark 0100 aeroplanes equipped with Goodrich main landing gear part numbers 41050-x or 41060-x. It mandates a one-time inspection of the left-hand and right-hand main landing gear retraction actuators to check for interference, damage, and correct orientation of the greasing nipple. This directive aims to ensure continued safe operation of the affected aircraft.

Airworthiness Directive

Fokker F28
Fokker F28 Mark 0070
Fokker F28 Mark 0100