EASA Regulations & Airworthiness Directives

Browse 5,158 EASA regulations with AI-powered summaries.

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EASA AD 2023-0064

Mar 20, 2023

Main Rotor — Pitch Rod Upper Links — Marking / Inspection

EASA Airworthiness Directive 2023-0064 is issued for Airbus Helicopters AS 350, EC 130, AS 355, AS 365, and SA 365 models. It addresses the main rotor pitch rod upper links, specifically the pitch rod lever axis attachment screws with Part Number 350A31-1873-20, requiring marking and inspection to detect loss of screw torque. The directive aims to prevent potential loss of control due to failure of these components.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters AS 355
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters SA 365

EASA AD 2023-0063

Mar 20, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2023-0063 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 7X aeroplanes, including those modified with Dassault modification M1000 (Falcon 8X). It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Dassault Falcon 7X Aircraft Maintenance Manual, Airworthiness Limitations Section, Revision 11. The directive ensures continued airworthiness by enforcing replacement of life-limited parts and adherence to maintenance intervals.

Airworthiness DirectiveSuperseded
  • Dassault Falcon 7X

EASA AD 2023-0062

Mar 20, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section Chapter 5-40 – Amendment

EASA Airworthiness Directive 2023-0062 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Mystère-Falcon 20-( )5 series aeroplanes. It mandates compliance with updated structural inspection and maintenance requirements as specified in the Dassault Mystère-Falcon 20 Aircraft Maintenance Manual Airworthiness Limitations Section Chapter 5-40 Revision 11. This directive ensures continued airworthiness by enforcing life limits and maintenance tasks for these aircraft.

Airworthiness DirectiveSuperseded
  • Dassault Mystère-Falcon 20
  • Dassault Mystère-Falcon 20

EASA SIB 2023-04

Mar 17, 2023

Exhaust System Modification

EASA Safety Information Bulletin 2023-04 is an airworthiness bulletin addressing exhaust system modifications for AQUILA AT01 and AT01-100 aeroplanes equipped with the BRP-Rotax 912S3 engine. The bulletin provides information about an improved exhaust system designed to enhance engine reliability and life. It is intended to inform operators and maintenance personnel about this recommended modification.

Safety Information BulletinSuperseded
  • Aquila Aviation Gmbh AT01
  • Brp-Rotax Gmbh & Co Kg 912 S

EASA AD 2023-0061

Mar 17, 2023

Nacelles / Pylons — Nacelle Panels — Inspection

The document titled 'Nacelles / Pylons — Nacelle Panels — Inspection' is an explanatory statement issued by EASA regarding the absence of an Airworthiness Directive (AD) for the Airbus A400M aircraft in civil service. It clarifies that no public AD exists because the Airbus A400M is currently not operated in civil aviation, and the document serves as an informational record for military authorities and design approval holders. The document recommends that military airworthiness authorities issue their own ADs for the affected aircraft.

Safety Information Bulletin
  • Airbus Military A400M
  • Airbus A400M

EASA AD 2023-0057

Mar 16, 2023

Airborne Auxiliary Power — Auxiliary Power Unit Fuel Control Unit — Replacement

EASA Airworthiness Directive 2023-0057 is an airworthiness directive addressing Airbus A330 and A340 aeroplanes equipped with Honeywell GTCP331-350 auxiliary power units (APUs). The directive targets specific APU fuel control units with part numbers 3883240-3, 3883240-5, or 3883240-6 that have known cracks in the housing assembly, which could cause fuel leakage. The AD mandates replacement of affected fuel control units to ensure continued safe operation.

Airworthiness Directive
  • Airbus A330
  • Airbus A340

EASA AD 2023-0055

Mar 16, 2023

Landing Gear — Wheels and Brakes / Brake unit — Replacement

Landing Gear — Wheels and Brakes / Brake unit — Replacement is a regulatory document concerning the replacement procedures for brake units on the Aircraft Industries L 410/420 (Turbolet) aircraft. It addresses maintenance and safety requirements specific to the landing gear's wheels and brakes system for these aircraft models. The document provides guidance to ensure proper brake unit replacement to maintain airworthiness.

Airworthiness Directive
  • Aircraft Industries L 410
  • Aircraft Industries 420 (Turbolet)
  • Aircraft Industries L 410/420

EASA AD CF-2023-18

Mar 16, 2023

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

Canadian Airworthiness Directive CF-2023-18 addresses the pneumatic system on Bombardier Inc. model BD-700-2A12 aeroplanes, serial numbers 70005 and subsequent. It focuses on non-conforming bleed air leak detection system sensing elements that may have insufficient salt fill, potentially impairing hot bleed air leak detection. This directive mandates testing and replacement of affected sensing elements to ensure continued safe flight and landing.

Airworthiness Directive
  • Bombardier BD-7002A12

EASA SIB SAIB-2023-04

Mar 16, 2023

Propeller Assembly by Trinity Specialized Services, LLC

The Special Airworthiness Information Bulletin SAIB: 2023-04 is an FAA information bulletin addressing airworthiness concerns related to Hartzell and McCauley propellers that were returned to service by Trinity Specialized Services, LLC between January 29, 2016 and March 25, 2021. The bulletin highlights improper maintenance and overhaul practices affecting these propellers but does not mandate regulatory action. It is intended to inform owners, operators, maintenance technicians, and inspectors about potential reliability issues with these propellers.

Safety Information Bulletin
  • Hartzell Propeller 2A1
  • Hartzell Propeller 3A1
  • Hartzell Propeller 3C1
  • Hartzell Propeller 5D3
  • Hartzell Propeller HA-A2V, HA-A2MV
  • Hartzell Propeller HA-B3Z
  • Hartzell Propeller HC-12V
  • Hartzell Propeller HC-12X
  • Hartzell Propeller HC-13X
  • Hartzell Propeller HC-82V
  • Hartzell Propeller HC-83V
  • Hartzell Propeller HC-92W
  • Hartzell Propeller HC-92Z
  • Hartzell Propeller HC-A2V, HC-A2MV
  • Hartzell Propeller HC-A3V, HC-A3MV
  • Hartzell Propeller HC-A6A
  • Hartzell Propeller HC-B3M
  • Hartzell Propeller HC-B3P
  • Hartzell Propeller HC-B3R
  • Hartzell Propeller HC-B3T
  • Hartzell Propeller HC-B3W
  • Hartzell Propeller HC-B3Z
  • Hartzell Propeller HC-B4M
  • Hartzell Propeller HC-B4T
  • Hartzell Propeller HC-B5M
  • Hartzell Propeller HC-C2Y
  • Hartzell Propeller HC-C3Y
  • Hartzell Propeller HC-D2V, HC-D2MV
  • Hartzell Propeller HC-D2X
  • Hartzell Propeller HC-D3V, HC-D3MV
  • Hartzell Propeller HC-D4
  • Hartzell Propeller HC-E2Y
  • Hartzell Propeller HC-E3YR
  • Hartzell Propeller HC-E4
  • Hartzell Propeller HC-E5
  • Hartzell Propeller HC-F2Y
  • Hartzell Propeller HC-F3Y
  • Hartzell Propeller HC-G2Y
  • Hartzell Propeller HC-G3Y
  • Hartzell Propeller HC-H3Y
  • Hartzell Propeller HC-I2Y
  • Hartzell Propeller HC-I3YR
  • Hartzell Propeller HC-J2Y
  • Hartzell Propeller HC-J3Y
  • Hartzell Propeller HC-L2Y
  • Hartzell Propeller HC-L3YF
  • Hartzell Propeller HC-M2YR
  • Hartzell Propeller HC-M3Y
  • Hartzell Propeller HD-E6C
  • Mccauley Propeller Systems 1A100
  • Mccauley Propeller Systems 1A101
  • Mccauley Propeller Systems 1A102
  • Mccauley Propeller Systems 1A103
  • Mccauley Propeller Systems TCM
  • Mccauley Propeller Systems 1A135
  • Mccauley Propeller Systems 1A170
  • Mccauley Propeller Systems 1A175
  • Mccauley Propeller Systems 1A90
  • Mccauley Propeller Systems 1B175
  • Mccauley Propeller Systems 1B90
  • Mccauley Propeller Systems 1C160
  • Mccauley Propeller Systems 1C172
  • Mccauley Propeller Systems 1C235
  • Mccauley Propeller Systems 1C90
  • Mccauley Propeller Systems 2A34C
  • Mccauley Propeller Systems 2A36C
  • Mccauley Propeller Systems 2A37C
  • Mccauley Propeller Systems 2AF31C10
  • Mccauley Propeller Systems 2AF34C
  • Mccauley Propeller Systems 2AF36C
  • Mccauley Propeller Systems 2D34C
  • Mccauley Propeller Systems 2D37C
  • Mccauley Propeller Systems 3A32C
  • Mccauley Propeller Systems 3A32C4(XX)
  • Mccauley Propeller Systems 3A34C4(XX)
  • Mccauley Propeller Systems 3A36C4(XX)
  • Mccauley Propeller Systems 3A37C34(XX)
  • Mccauley Propeller Systems 3AF32C
  • Mccauley Propeller Systems 3AF32C5(XX)
  • Mccauley Propeller Systems 3AF34C
  • Mccauley Propeller Systems 3AF34C5(XX)
  • Mccauley Propeller Systems 3AF36C5(XX)
  • Mccauley Propeller Systems 3AF37C5(XX)
  • Mccauley Propeller Systems 3D32C4(XX)
  • Mccauley Propeller Systems 3D34C4(XX)
  • Mccauley Propeller Systems 3D36C4(XX)
  • Mccauley Propeller Systems 3DF36C5(XX)
  • Mccauley Propeller Systems 3FF32C
  • Mccauley Propeller Systems 3FF34C
  • Mccauley Propeller Systems 3GFR34C6(XX)
  • Mccauley Propeller Systems 3GFR34C7(XX)
  • Mccauley Propeller Systems 4HFR34C
  • Mccauley Propeller Systems 4JFR34C
  • Mccauley Propeller Systems 5HFR34C
  • Mccauley Propeller Systems 5JFR36C

EASA AD 2023-0059

Mar 16, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2023-0059 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Fan Jet Falcon aeroplanes equipped with the Supplemental Structural Inspection Program (SSIP). It mandates updated maintenance tasks and life limits as specified in the Dassault Fan Jet Falcon Aircraft Maintenance Manual Chapter 5-40 Revision 11. This directive ensures continued structural integrity and airworthiness of these aircraft.

Airworthiness DirectiveSuperseded
  • Dassault Fan Jet Falcon

EASA AD 2023-0060

Mar 16, 2023

Time Limits / Maintenance Checks – Airworthiness Limitations Section Chapter 5-40 – Amendment

EASA Airworthiness Directive 2023-0060 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Fan Jet Falcon aeroplanes. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Dassault FJF Aircraft Maintenance Manual Airworthiness Limitations Section Chapter 5-40 Revision 19. This directive applies to all Fan Jet Falcon aircraft except those that have incorporated the Supplemental Structural Inspection Program via Service Bulletin 730.

Airworthiness DirectiveSuperseded
  • Dassault Fan Jet Falcon

EASA AD US-2023-05-16

Mar 15, 2023

Engine - Crankshaft Counterweight Retaining Rings - Inspection

Airworthiness Directive 2023-05-16 is a final rule issued by the FAA addressing Continental Aerospace Technologies, Inc. reciprocating engines, including models such as GTSIO-520 series, IO-360 series, IO-470 series, IO-520 series, IO-550 series, LTSIO-360 series, O-470 series, TSIO-360 series, TSIO-520 series, TSIO-550 series, TSIOF-550-K, and TSIOL-550 series. This directive mandates inspection of the crankshaft assembly for proper installation of the counterweight retaining rings in the counterweight groove and requires corrective actions if improper installation is found.

Airworthiness Directive
  • Continental Aerospace Technologies, GTSIO-520
  • Continental Aerospace Technologies, IO-360
  • Continental Aerospace Technologies, IO-470
  • Continental Aerospace Technologies, IO-520
  • Continental Aerospace Technologies, IO-550
  • Continental Aerospace Technologies, LTSIO-360
  • Continental Aerospace Technologies, LTSIO-520
  • Continental Aerospace Technologies, O-470
  • Continental Aerospace Technologies, TSIO-360
  • Continental Aerospace Technologies, TSIO-520
  • Continental Aerospace Technologies, TSIO-550
  • Continental Aerospace Technologies, TSIOF-550
  • Continental Aerospace Technologies, TSIOL-550

EASA AD US-2023-02-17

Mar 15, 2023

Wings - Carry-thru Spar - Inspection

The Federal Aviation Administration's Airworthiness Directive 2023-02-17 is a final rule addressing Textron Aviation Inc. (formerly Cessna Aircraft Company) Model 210N, 210R, P210N, P210R, T210N, T210R, 177, 177A, 177B, 177RG, and F177RG airplanes. It mandates inspections and corrective actions for the carry-thru spar lower cap due to identified corrosion and fatigue cracking risks. This directive aims to prevent potential wing separation and loss of control caused by structural failure.

Airworthiness Directive
  • Textron Aviation 177 (Cardinal)
  • Textron Aviation 177RG (Cardinal RG)
  • Textron Aviation 210 (Centurion)
  • Textron Aviation F177RG
  • Textron Aviation 210N
  • Textron Aviation 210R
  • Textron Aviation P210N
  • Textron Aviation P210R
  • Textron Aviation T210N
  • Textron Aviation T210R
  • Textron Aviation 177
  • Textron Aviation 177A
  • Textron Aviation 177B
  • Textron Aviation 177RG

EASA AD 2023-0053

Mar 14, 2023

Fuselage — Rear Fuselage — Modification

EASA Airworthiness Directive 2023-0053 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330-223F and A330-243F aeroplanes. It addresses a structural modification to the rear fuselage, specifically the circumferential joint at Frame 58, to prevent widespread fatigue damage. The directive mandates reinforcement of this area to maintain the structural integrity of the affected aircraft models.

Airworthiness Directive
  • Airbus A330223F243F

EASA AD 2023-0054

Mar 14, 2023

Fuselage — Rear Fuselage — Modification

EASA Airworthiness Directive 2023-0054 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330-202, A330-203, A330-223, A330-243, and A330-841 aeroplanes. The directive addresses a modification to the rear fuselage, specifically the circumferential joint at Frame 58, to ensure structural integrity. It applies to specific manufacturer serial numbers of these aircraft models.

Airworthiness Directive
  • Airbus A330202203223243841

EASA AD CF-2023-19

Mar 14, 2023

Pneumatic – 14th Stage Bleed Duct Missing Insulation

Canadian Airworthiness Directive CF-2023-19 addresses missing insulation on the 14th stage bleed ducts of Mitsubishi Heavy Industries RJ Aviation ULC model CL-600-2B19 aircraft. This directive mandates inspections of the engine pylon structure and introduces a new certification maintenance requirement to ensure the integrity of the bleed duct insulation. The AD applies to all serial numbers of the CL-600-2B19 model.

Airworthiness DirectiveSuperseded
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Mitsubishi Heavy Industries RJ Aviation ULC CL-600-2B19

EASA AD US-2023-03-15

Mar 13, 2023

Air Conditioning - Trim Air Diffuser Ducts - Inspection / Replacement

Airworthiness Directive 2023-03-15 is a final rule issued by the Federal Aviation Administration addressing all Boeing Model 747 series airplanes including 747-100, 747-200, 747-300, 747-400, 747SR, and 747SP variants. This directive focuses on the inspection and replacement of trim air diffuser ducts (TADDs) to prevent damage that could lead to fuel leakage and potential fire or explosion hazards. It supersedes previous requirements and updates inspection and replacement protocols for these critical air conditioning components.

Airworthiness Directive
  • Boeing 747