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EASA Regulations for Fokker F28

36 airworthiness directives and regulations affecting Fokker F28.

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.

Jan 8, 2020
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker 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.

Sep 6, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker 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.

Jul 10, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2018-0076R1

Landing Gear — Hydraulic Line T-Union — Replacement

The document titled 'Landing Gear — Hydraulic Line T-Union — Replacement' is a service communication issued by FOKKER SERVICES concerning the F28 aircraft type. It addresses the replacement of the hydraulic line T-union component within the landing gear system to ensure continued airworthiness and safety. This document is relevant to operators and maintenance organizations responsible for F28 aircraft maintenance.

Jul 10, 2019
OtherMaintenanceSafety MgmtFokker F28

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.

May 29, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0100

EASA AD 2019-0104

Landing Gear — Main Landing Gear Hydraulic Hose Assemblies — Replacement

EASA Airworthiness Directive 2019-0104 is an airworthiness directive addressing the replacement of main landing gear hydraulic hose assemblies on Fokker F28 aeroplanes, including Mark 0070, 0100, 1000, 2000, 3000, and 4000 models. The directive mandates replacing certain hose assemblies with updated parts featuring strengthened restrictor check valves to ensure safe landing gear operation.

May 10, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

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.

Apr 30, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker 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.

Feb 19, 2019
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2018-0259R1

SUPERSEDED BY EASA AD 2021-0234

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.

Feb 7, 2019
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Airbus A330Airbus A340ATR ATR42ATR ATR72Boeing 737Boeing 757Boeing 767Boeing 777Bombardier CL-600 (Challenger)De Havilland Canada DHC-8Fokker CRR-0185Fokker CRR-0186Fokker CRR-0190Fokker CRR-0210Fokker CRR-0241Fokker CRR-0265Fokker CRR-0300MHI RJ Aviation CL-600 (Regional Jet)Fokker F27Fokker F28Boeing 747Bombardier CL-600Bombardier DHC-8

EASA AD 2018-0159

SUPERSEDED BY EASA AD 2020-0024

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.

Jul 25, 2018
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker 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.

Jun 4, 2018
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2018-0077

SUPERSEDED BY EASA AD 2024-0123

EASA Airworthiness Directive 2018-0077 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Fokker Services B.V. F28 aeroplanes, specifically the F28 Mark 0070 and Mark 0100 models. It addresses issues with hydraulic line restrictor check valves in the parking brake shut-off valve (PBSOV) hydraulic return line that may become obstructed by debris. The directive mandates replacement of these valves with improved versions incorporating a filter screen to ensure safe landing gear operation.

Apr 6, 2018
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

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.

Jan 4, 2018
Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA SIB 2010-32

WITHDRAWN - REPLACED BY EASA AD 2011-0043

EASA Safety Information Bulletin 2010-32 is an informational bulletin addressing the potential loss of ATC transponder transmissions caused by a loose resistor connection in Gables Engineering Inc ATC/TCAS control panels, specifically the G7490, G7492, and G7493 series. These control panels are installed on various aircraft types including Airbus A310, ATR 42, BAE Systems BAe146, Boeing 707 through 777 series, Fokker F28, Lockheed Hercules and Tristar, McDonnell Douglas DC and MD series, and Sabreliner NA-265 series. The bulletin provides guidance but does not mandate corrective action.

May 25, 2011
Safety Information BulletinSafety MgmtMaintenanceAirbus A310ATR 42BAE Systems BAe146Boeing 707Boeing 717Boeing 727Boeing 737Boeing 747Boeing 757Boeing 767Boeing 777Fokker F28Lockheed HerculesLockheed TristarMcDonnell Douglas DC seriesMcDonnell Douglas MD seriesSabreliner NA-265

EASA SIB 2010-25

Cabin Oxygen Mask Service Recommendations from Original Equipment Manufacturers, and Cabin Oxygen Masks with B/E Aerospace In-line Flow Indicators Part Number (P/N) 118023-02

EASA Safety Information Bulletin SIB No. 2010-25 provides service recommendations regarding cabin oxygen masks equipped with B/E Aerospace in-line flow indicators part number 118023-02. The bulletin applies to CS1-23 and CS-25 category aeroplanes, including Airbus A318, A319, A320, A321, Boeing 737, 747, 757, 767, 777, and Fokker F28 models. It addresses failures of the in-line flow indicators that can cause oxygen flow interruption during use.

Aug 27, 2010
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321Boeing 737Boeing 747Boeing 757Boeing 767Boeing 777Fokker F28

EASA SIB 2009-29

Fokker F28 Mark 0070 and Mark 0100 — Liftdumper Mechanical Control System Bolts

EASA Safety Information Bulletin 2009-29 is an informational bulletin addressing a safety concern with certain shouldered bolts, Part Number A16189-001, used in the liftdumper mechanical control system of Fokker F28 Mark 0070 and Mark 0100 aircraft. The bulletin highlights that some bolts were wrongly manufactured with a thinner shoulder, which may affect the mechanical fit but not immediate safety. It provides guidance to operators and maintenance organizations on identifying and replacing these bolts.

Aug 27, 2009
Safety Information BulletinMaintenanceSafety MgmtFokker F28