EASA Regulations for Fokker F28

5 airworthiness directives and regulatory documents affecting Fokker F28.

EASA AD 26-019

Time Limits / Maintenance Checks — Airworthiness Limitations Section Part 2 —Airworthiness Limitations Items and Safe life Items — Amendment

EASA Airworthiness Directive 26-019 is a proposed amendment affecting Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It updates the Airworthiness Limitations Section Part 2, which includes Airworthiness Limitation Items and Safe Life Items, to ensure continued airworthiness of these aircraft. The directive applies to all serial numbers of the specified models and mandates compliance with updated maintenance tasks and life limits.

Feb 2, 2026

Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

EASA AD 2025-0250

Fuselage — Frame Inboard Boom — Inspection

EASA Airworthiness Directive 2025-0250 is an airworthiness directive addressing Fokker F28 Mark 0070 and Mark 0100 aeroplanes. It mandates a one-time inspection of the fuselage frame inboard boom area at specific wing spar joint locations to detect cracks that could compromise structural integrity. The directive also requires reporting inspection results to Fokker Services.

Nov 10, 2025

Airworthiness DirectiveMaintenanceSafety MgmtFokker F28

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.

Oct 10, 2024

Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100

EASA AD 2024-0176

SUPERSEDED BY EASA AD 2024-0192

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.

Sep 11, 2024

Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker 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.

Jun 28, 2024

Airworthiness DirectiveMaintenanceSafety MgmtFokker F28Fokker F28 Mark 0070Fokker F28 Mark 0100