RegNotify

EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA SIB 2008-02

FAA SAIB CE-08-11 - Piper PA-23, PA-31 and PA-42 Aeroplanes - Hydraulic Hose P/N 17766-02 (465-138) Potential Failure

FAA Special Airworthiness Information Bulletin CE-08-11 is an informational bulletin addressing a potential failure of hydraulic hose part number 17766-02 (465-138) on New Piper Aircraft models PA-23, PA-31, and PA-42. The hydraulic hose failure may cause loss of pressure needed to extend the landing gear, affecting all serial numbers of the listed Piper aircraft. This bulletin alerts operators and maintenance personnel to inspect and monitor this specific hydraulic hose for deterioration.

Jan 11, 2008
Safety Information BulletinMaintenanceSafety MgmtPiper PA-23Piper PA-31Piper PA-42

EASA SIB 2008-01

LINDSTRAND Hot Air Balloons (LHAB) - Replacement of defective fuel hoses.

EASA Safety Information Notice No. 2008-01 is a safety information notice regarding the replacement of defective fuel hoses on LINDSTRAND Hot Air Balloons (LHAB). It references the United Kingdom CAA Emergency Airworthiness Directive G-2008-0001, which applies to all LINDSTRAND hot air balloons equipped with burner hoses manufactured by Flexquip as identified in LHAB Service Bulletin No. 11. The notice highlights a serious safety issue related to defective burner hoses that may develop leaks.

Jan 11, 2008
Safety Information BulletinMaintenanceSafety MgmtLINDSTRAND Hot Air Balloons

EASA SIB 2007-52

Rolls-Royce RB211-524 and -535E4, RB211 Trent 500, 700 and 800 series engines - Group A Parts - Non-compliance with required Magnetic Particle Inspection (MPI) instructions

EASA Safety Information Notice 2007-52 addresses non-compliance with Magnetic Particle Inspection (MPI) instructions on Rolls-Royce RB211-524, RB211-535E4, and RB211 Trent 500, 700, and 800 series engines. The notice informs that some Group A parts were inspected without removing corrosion protective coatings, which reduces MPI effectiveness. This issue does not affect the engine type design or require additional in-service action.

Dec 21, 2007
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2007-47

WITHDRAWN - CORRECTIVE ACTIONS TAKEN

EASA Safety Information Notice No. 2007-47 is an interim communication regarding certain products and components released under EASA Approval number 145.0004. It highlights concerns about maintenance compliance for parts including main landing gear assemblies, brace struts, lock link assemblies, HPT rotor assemblies, NGV support EMUs, and CF6 engine models supplied to customers such as MNG, Patriot Aviation, and Air Universal. The notice does not confirm full compliance with EASA Part 145 requirements and awaits further investigation results.

Dec 20, 2007
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2007-51

PARACHUTES DE FRANCE reserve canopies

The EASA Safety Information Notice No. 2007-51 addresses DGAC France Airworthiness Directives F-2007-025 and F-2007-026 concerning PARACHUTES DE FRANCE reserve canopies. These directives focus on safety issues related to reserve parachutes manufactured by PARACHUTES DE FRANCE between 1987 and 1989, and the TECHNO 240-B reserve parachute model. The directives include mandatory inspections, modifications, and grounding measures to ensure parachute reliability and compliance.

Dec 19, 2007
Airworthiness DirectiveMaintenanceSafety Mgmt

EASA SIB 2007-49

Eurocopter AS 332 and EC 225 helicopters - Tail Gearbox (TGB) Attachment Fittings Manufacturing Defect

EASA Safety Information Notice No. 2007-49, issued on 2007-12-10, addresses a manufacturing defect in the tail gearbox (TGB) attachment fittings of Eurocopter AS332 C, C1, L, L1, L2 and EC225 LP helicopters with specific serial numbers. The defect involves interference caused by a missing blind hole in the structure fitting, affecting proper bolt tightening. This notice informs operators and maintenance organizations about the issue and references the DGAC France Emergency Airworthiness Directive UF-2007-027 for mandatory corrective actions.

Dec 10, 2007
Safety Information BulletinMaintenanceSafety MgmtEurocopter AS 332Eurocopter EC 225

EASA SIB 2007-48

Luftfahrt-Bundesamt (LBA) Airworthiness Directives D-2007-350 and D-2007-353 for the RUAG Aerospace GmbH Dornier 228 series aircraft.

The Luftfahrt-Bundesamt (LBA) Airworthiness Directives D-2007-350 and D-2007-353 address safety issues for the RUAG Aerospace GmbH Dornier 228 series aircraft. AD D-2007-350 concerns partial de-bonding of surface protection on rudders and elevators due to an unapproved paint stripping process. AD D-2007-353 deals with cracks in rudder control cable terminals caused by production errors in cables delivered after January 1, 2006.

Dec 10, 2007
Airworthiness DirectiveMaintenanceSafety MgmtRUAG Aerospace Dornier 228

EASA SIB 2007-46

Eurocopter EC 225 LP helicopters - Main Servo Control Check

EASA Safety Information Notice No. 2007-46 addresses a manufacturing defect in the main servo control units of Eurocopter EC 225 LP helicopters. The defect involves incorrectly positioned retaining rings on the coupling tube of the servo control distributors, potentially causing untimely piston rod movement during hydraulic pressurization. This notice informs operators and maintenance personnel about the issue and references the French DGAC Emergency Airworthiness Directive UF-2007-022 for mandatory checks and replacements.

Nov 14, 2007
Safety Information BulletinMaintenanceSafety MgmtAirbus Helicopters EC 225 LP

EASA SIB 2007-45

Rolls-Royce Deutschland (RRD) - Reverse Wired Independent Overspeed Protection Coils in BR700 series engines

EASA Safety Information Notice No. 2007-45 is an informational document addressing reverse wired Independent Overspeed Protection (IOP) coils in Rolls-Royce Deutschland BR700 series engines. The affected engine models include BR700-710A1-10, BR700-710A2-20, BR700-710C4-11, BR700-715A1-30, BR700-715B1-30, and BR700-715C1-30, which are installed on aircraft such as Bombardier BD-700-1A10 and BD-700-1A11, Gulfstream Aerospace GV and GV-SP, and McDonnell Douglas 717-200 series. The notice highlights a wiring issue that could disable the Fuel Metering Unit shutoff during an overspeed event.

Nov 14, 2007
Safety Information BulletinMaintenanceSafety MgmtBombardier BD-700-1A10Bombardier BD-700-1A11Gulfstream Aerospace GVGulfstream Aerospace GV-SPMcDonnell Douglas 717-200

EASA SIB 2007-40

FAA SAIB CE-08-02 - Cessna 180, 182 and 185 Aeroplanes - Horizontal Stabiliser Trim Freeze-up In-Flight

FAA Special Airworthiness Information Bulletin CE-08-02 is an informational bulletin addressing an airworthiness concern affecting Cessna 180, 182, and 185 series aircraft. The bulletin highlights issues with horizontal stabilizer trim freeze-up in flight caused by excessive wear in the pitch trim actuator screw-jack threads, specifically involving parts with Cessna part numbers 0712500-13 and 0712500-11. This condition may impair pitch trim control and aircraft handling.

Nov 12, 2007
Safety Information BulletinMaintenanceSafety MgmtCessna 180Cessna 182Cessna 185

EASA SIB 2007-39R1

Fokker F27 Mark 050/060 series aircraft - Main Landing Gear Sliding Member End-Stop Installation

EASA Safety Information Notice No. 2007-39 Revision 1 and Civil Aviation Authority Netherlands Airworthiness Directive NL-2007-002 address the main landing gear sliding member end-stop installation on Fokker F27 Mark 050, Mark 0502, and Mark 0604 series aircraft. The documents highlight a safety concern due to improper installation leading to potential overextension of the main landing gear sliding member. These publications provide inspection and corrective action requirements to ensure proper lockwiring and prevent structural damage.

Nov 12, 2007
Airworthiness DirectiveMaintenanceSafety MgmtFokker F27

EASA SIB 2007-41

Transport Canada Advisory AV-2007-05 - Pratt & Whitney Canada PT6A engines - Electrical Discharge Damage (EDD)

Transport Canada Advisory AV-2007-05 is a service difficulty advisory concerning Pratt & Whitney Canada PT6A series engines, addressing the issue of Electrical Discharge Damage (EDD) to the No.1 bearing. This advisory applies to any aircraft equipped with these engines and highlights the risk of in-flight shutdowns and costly component replacements due to electrical arcing damage. The advisory is supported by EASA Safety Information Notice 2007-41 and provides information on the nature and causes of EDD in these engines.

Nov 12, 2007
OtherMaintenanceSafety Mgmt

EASA SIB 2007-42

Transport Canada Advisory AV-2007-06 - Pratt & Whitney Canada PT6A-114 and -114A engines - Compressor Turbine Blade Failures

Transport Canada Advisory AV-2007-06 is a service difficulty advisory addressing compressor turbine blade failures in Pratt & Whitney Canada PT6A-114 and -114A engines. The advisory highlights inflight shutdowns and damage caused by blade failures, emphasizing the importance of proper engine maintenance and power management. It applies to any aircraft equipped with these engine models.

Nov 12, 2007
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2007-43

WITHDRAWN - SEE FAA AD 2012-06-25

EASA Safety Information Notice No. 2007-43 is an informational document regarding the FAA Airworthiness Directive 2007-23-01, which addresses issues with Goodrich Evacuation Systems installed on Airbus A330 and A340 series aircraft. The affected evacuation systems, qualified under TSO-C69b, have experienced pressure relief valve leakage that impacts raft mode functionality. This notice informs stakeholders that EASA has not adopted the FAA AD but considers it an interim solution.

Nov 12, 2007
Safety Information BulletinSafety MgmtMaintenanceAirbus A330Airbus A340

EASA SIB 2007-38R1

Viking Air Ltd. (Bombardier, De Havilland Canada) DHC-6 Aeroplanes - Inspections of Elevator Control Cables

EASA Safety Information Notice No. 2007-38 Revision 1 addresses inspections of elevator control cables on Viking Air Ltd. (formerly Bombardier and De Havilland Canada) DHC-6 series Twin Otter airplanes. The notice follows a fatal accident involving a DHC-6 in French Polynesia where worn stainless steel elevator control cables were found. It highlights the need for thorough inspections of elevator control cables to detect wear and chafing that may not be visible during routine checks.

Oct 15, 2007
Safety Information BulletinMaintenanceSafety MgmtViking Air DHC-6

EASA SIB 2007-37

WITHDRAWN — SEE FAA SAIB NE-07-49R1

EASA Safety Information Notice 2007-37 is an informational notice regarding Lycoming 4-, 6-, and 8-cylinder reciprocating engines equipped with stainless steel fuel injector tube assemblies and support clamps. It alerts aircraft owners, operators, and repair facilities about a potential issue that could cause fuel leaks, fires, and engine failures. This notice references FAA Special Airworthiness Information Bulletin NE-07-49 for further details.

Oct 9, 2007
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2007-36

FAA SAIB CE-01-41R2 - Cessna 150, 172, P172, 175, 180, 182, 185, 205, 206, 210, 336 and 337 Aeroplanes - Possible Cracks in Plastic or Non-Metallic Control Wheels

FAA Special Airworthiness Information Bulletin CE-01-41R2 addresses the potential for cracks in plastic or non-metallic control wheels installed on Cessna 150, 172, P172, 175, 180, 182, 185, 205, 206, 210, 336, and 337 series airplanes manufactured between 1960 and 1964. The bulletin informs owners, operators, and maintenance personnel about this issue and provides guidance on inspection and replacement procedures. This information is also referenced in EASA Safety Information Notice 2007-36.

Oct 5, 2007
Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 172Cessna P172Cessna 175Cessna 180Cessna 182Cessna 185Cessna 205Cessna 206Cessna 210Cessna 336Cessna 337

EASA SIB 2007-15R1

Transport Canada Alert AL-2007-02 - Bombardier CL-600-2B19 "Regional Jet" aeroplanes - Thrust Reverser Access Cowls Separation

Transport Canada Alert AL-2007-02 is a Service Difficulty Alert concerning the Bombardier CL-600-2B19 "Regional Jet" aircraft. It addresses the issue of thrust reverser access cowls separating during flight due to defective or improperly engaged Camloc fasteners. The alert references related Bombardier service letters and bulletins to highlight the safety concern and maintenance implications.

Oct 5, 2007
Safety Information BulletinMaintenanceSafety MgmtBombardier CL-600-2B19

EASA SIB 2007-35

FAA SAIB CE-07-46 - Installation of Bulkhead Universal Fittings in a Hydraulic Pump Port

FAA Special Airworthiness Information Bulletin CE-07-46 is an informational bulletin addressing an airworthiness concern related to the installation of bulkhead universal fittings in hydraulic pump ports. It highlights issues with improper installation causing hydraulic fluid leaks due to o-ring damage. This bulletin applies to any aircraft equipped with these bulkhead universal fittings and references standards for proper installation.

Oct 4, 2007
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2007-34

Use of Non-Approved Gearbox Oil in TAE 125 series engines

EASA Safety Information Notice No. 2007-34 addresses the use of non-approved gearbox oils in Thielert Aircraft Engines (TAE) 125-01 and 125-02 series engines, which are installed on various single- and twin-engine aircraft certified under US, Canadian, and European Part 23 airworthiness standards. The notice highlights that only Shell EP 75W-90 API GL-4 or Shell Spirax GSX 75W-80 oils are approved for these gearboxes. Using non-approved oils, especially GL-5 types, can cause gearbox damage and propeller control failures, potentially leading to engine overspeed or in-flight shutdown.

Sep 27, 2007
Safety Information BulletinMaintenanceSafety Mgmt