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 2011-14

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE. Topic addressed by EASA SIB 2011-15R3

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE is an EASA Safety Information Bulletin (SIB) originally issued as SIB 2011-14 addressing the incorrect setting of ICAO 24-bit aircraft addresses in Mode S transponders. It applies to all aircraft equipped with SSR Mode S transponders, including those certificated under FAR, JAR, and CS Parts 22, 23, 25, 27, 29, 31HB, VLA, or VLR. The bulletin highlights risks associated with duplicate or incorrect ICAO addresses affecting air traffic control identification and ACAS II performance.

Jul 4, 2011
Safety Information BulletinSafety Mgmt

EASA SIB CE-11-42

Piper PA-28, PA-32, PA-34 and PA-44 Series - Flight Control Cable/Pulley Inspections

The Special Airworthiness Information Bulletin SAIB: CE-11-42 is an FAA informational bulletin addressing a potential airworthiness issue with flight control cables and pulleys on Piper PA-28, PA-32, PA-34, and PA-44 series airplanes. It highlights a manufacturing flaw in pulleys that can cause aileron control cables to fail, potentially resulting in loss of aileron control. The bulletin applies to all serial numbers of the specified Piper models and provides inspection guidance but does not mandate regulatory action.

Jun 30, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32Piper PA-34Piper PA-44

EASA SIB 2011-19

WITHDRAWN - AmSafe Restraint Systems - Jammed Connector in a Rotary Buckle

EASA Safety Information Bulletin 2011-19 is an informational bulletin addressing a reported issue with the AmSafe Restraint Systems rotary buckle, part number 504928-405, used in various AmSafe restraint system part numbers installed on helicopters and fixed-wing aircraft. The bulletin highlights a case where a passenger could not release the pelvic connector on an AS.365 N3 Dauphin helicopter during a non-emergency landing. Although the cause of the jammed connector has not been determined, EASA does not consider this an unsafe condition requiring an Airworthiness Directive.

Jun 17, 2011
Safety Information BulletinSafety MgmtEurocopter AS365 N3 Dauphin

EASA SIB CE-11-40

Allied Ag Cat Productions, Inc. (formerly Grumman, Schweizer) G-164 series — Potential Cracking in the Rudder

The Special Airworthiness Information Bulletin SAIB: CE-11-40 informs owners, operators, and maintenance personnel of Allied Ag Cat Productions, Inc. G-164 series airplanes about potential cracking in the rudder main spar tube. This bulletin covers models G-164, G-164A, G-164B (including variants with 73” wing gap and turbocharged versions), G-164C, and G-164D under Type Certificate Data Sheet 1A16. The FAA does not consider this an unsafe condition requiring mandatory Airworthiness Directive action at this time.

Jun 16, 2011
Safety Information BulletinMaintenanceSafety MgmtAllied Ag Cat G-164

EASA SIB 2011-18

Techtest Ltd. Emergency Locator Transmitter (ELT) — Marking and Training Considerations

EASA Safety Information Bulletin SIB No. 2011-18 titled Techtest Ltd. Emergency Locator Transmitter (ELT) — Marking and Training Considerations addresses the use of Techtest Ltd. Type 500-12, 500-16, and 500-27 ELTs installed or carried on all aircraft categories. The bulletin highlights specific operational characteristics and training needs related to these ELTs, which may be classified as either ELT-S or Personal Locator Beacons (PLBs).

Jun 15, 2011
Safety Information BulletinTrainingSafety Mgmt

EASA SIB SW-11-39

FreeFlight Systems (formerly Trimble) 2000 and 2101 Approach (series) GPS navigation units

The Special Airworthiness Information Bulletin SAIB: SW-11-39 is an FAA advisory concerning FreeFlight Systems (formerly Trimble) 2000 and 2101 Approach series GPS navigation units. It addresses service difficulties related to software version 24xM, which causes long computational delays during flight planning operations in affected GPS units. This bulletin does not apply to specific aircraft or engine models but focuses on the GPS navigation equipment used in various aircraft.

Jun 8, 2011
Safety Information BulletinFlight OpsMaintenanceSafety Mgmt

EASA SIB 2011-16

Teledyne Continental Ignition Systems (formerly Bendix) Magneto Capacitor Installation

EASA Safety Information Bulletin SIB No: 2011-16 addresses the installation of magneto capacitors on piston engine aircraft equipped with Teledyne Continental Ignition Systems (formerly Bendix) D-2000 or D-3000 series magnetos. The bulletin references a safety recommendation following an incident investigation involving a SOCTA TB-10 'Tobago' aircraft. It provides guidance for owners and operators to review and implement revised capacitor installation instructions as outlined in Teledyne Continental Ignition Systems Service Bulletin SB651.

Jun 8, 2011
Safety Information BulletinMaintenanceSafety MgmtSOCATA TB-10

EASA SIB CE-11-37

Piper PA-44-180 & Cessna 172R and S Aeroplanes - Engine Oil Filter Interference

The Special Airworthiness Information Bulletin SAIB: CE-11-37 is an FAA informational bulletin addressing engine oil filter interference issues in Piper PA-44-180 aircraft with Lycoming O-360-A1H6 and LO-360-A1H6 engines, and Cessna 172R and S aircraft with Lycoming IO-360-L2A engines. The bulletin highlights potential interference between oil cooler hose fittings and the oil filter that could lead to improper installation and oil system problems. Other engines and aircraft models may also be affected.

Jun 6, 2011
Safety Information BulletinMaintenanceSafety MgmtPiper PA-44-180Cessna 172RCessna 172S

EASA SIB CE-11-36

Cessna 172S Aeroplanes- Frayed Aileron Cables

The Special Airworthiness Information Bulletin SAIB: CE-11-36 is an FAA advisory addressing the potential issue of frayed aileron cables on Cessna Model 172S airplanes. It informs owners, operators, and maintenance personnel about observed wear in the aileron control system cables found during routine inspections. This bulletin does not mandate corrective action but provides important information on inspection and maintenance.

Jun 1, 2011
Safety Information BulletinMaintenanceSafety MgmtCessna 172S

EASA SIB 2011-12

Bombardier BD-700 — Possible Failure of Exit Door Actuator Tensator Springs

EASA Safety Information Bulletin SIB No: 2011-12 is an advisory document concerning Bombardier BD-700-1A10 and BD-700-1A11 aircraft. It highlights a possible failure of one or more Tensator springs in the exit door actuator, which may cause uncontrolled opening and closing of the exit doors. The bulletin supports the FAA's recommendations to address this issue and informs European operators accordingly.

May 26, 2011
Safety Information BulletinMaintenanceSafety MgmtBombardier BD-700

EASA SIB 2011-11

A reliable approach to rigging a sailplane

EASA Safety Information Bulletin SIB No: 2011-11 provides guidance on a reliable approach to rigging certain sailplanes, specifically the SZD-24C “Foka”, SZD-24-4A “Foka 4”, SZD-32A “Foka 5”, and SZD-36A “Cobra 15”. The bulletin addresses issues related to the wing attachment rigging mechanism, particularly the engagement of bevel bolts in the lug stack during rigging. It references findings from the UK Air Accidents Investigation Branch following an accident involving a SZD-24-4A “Foka 4”.

May 25, 2011
Safety Information BulletinMaintenanceSafety MgmtSZD SZD-24C FokaSZD SZD-24-4A Foka 4SZD SZD-32A Foka 5SZD SZD-36A Cobra 15

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 2011-08

Exterior Exit Markings on All-cargo Transport Aeroplanes

EASA Safety Information Bulletin SIB No. 2011-08 provides guidance on exterior exit markings for all-cargo transport aeroplanes. It applies to all transport category aeroplanes operated in an all-cargo configuration and references FAA Special Airworthiness Information Bulletin NM-10-23. The bulletin addresses the need for clear exterior markings on emergency exits accessible from inside the aircraft when fully loaded.

May 17, 2011
Safety Information BulletinSafety Mgmt

EASA SIB 2011-10

Loose Equipment in the Flight Compartment and on Glare Shields

EASA Safety Information Bulletin SIB No: 2011-10 addresses the hazards of loose equipment in the flight compartment and on glare shields for all aircraft. It endorses the FAA Special Airworthiness Information Bulletin CE-10-35 and highlights the risk of flight control jams caused by loose objects such as pens, coins, or tools. This bulletin aims to raise awareness among aircraft owners and operators about these safety concerns.

May 17, 2011
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2011-09

Pilot Response to Propeller Overspeed in Piston Engine Aeroplanes

EASA Safety Information Bulletin 2011-09 is an advisory document addressing pilot response to propeller overspeed in piston engine aeroplanes equipped with variable pitch propellers. It supports FAA Special Airworthiness Information Bulletin CE-10-21 and applies to all piston engine aircraft with variable pitch propellers registered in EU Member States or associated countries. The bulletin highlights the importance of adjusting airspeed below published best glide speed to maintain level flight during propeller overspeed events.

May 17, 2011
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB CE-11-32

M7 Aerospace LP (formerly Fairchild, Swearingen) SA226 aeroplanes - Engine Mount Section

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-32 addresses an airworthiness concern for M7 Aerospace LP SA226-T, SA226-AT, and SA226-TC model airplanes regarding potential cracks in the engine mount lower truss assemblies, part number 27-62010. This bulletin provides guidance on inspection and modification procedures for the left and right engine mount lower truss assemblies to detect and address cracking issues. The bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

May 13, 2011
Safety Information BulletinMaintenanceSafety MgmtM7 Aerospace SA226

EASA SIB 2009-18R1

Inspection of Main Rotor Blade Retention Bolts

EASA Safety Information Bulletin 2009-18R1 is an advisory document addressing the inspection of main rotor blade retention bolts on MD Helicopters MD900 models fitted with part number 900R3100001-105 bolts. It provides updated guidance following previous inspections related to bolts with part number 900R3100001-103 and references MD Helicopters Service Bulletin SB900-116R1 dated 9 April 2010. The bulletin aims to enhance safety by recommending repetitive gap checks and inspections of these critical components.

May 12, 2011
Safety Information BulletinMaintenanceSafety MgmtMD Helicopters MD900

EASA SIB CE-11-30

Air Tractor, Inc. (all types & models) - Airframe Structure Corrosion

The Special Airworthiness Information Bulletin SAIB: CE-11-30 is an informational document issued by the FAA addressing airframe structure corrosion in all Air Tractor, Inc. model series AT-250, AT-300, AT-400, AT-500, AT-600, and AT-800 aircraft. It highlights the susceptibility of these aircraft to severe corrosion due to their operation in harsh environments such as chemical dispersal and firebomber missions. The bulletin provides guidance on inspection and repair procedures but does not mandate regulatory action.

May 11, 2011
Safety Information BulletinMaintenanceSafety MgmtAir Tractor AT-250Air Tractor AT-300Air Tractor AT-400Air Tractor AT-500Air Tractor AT-600Air Tractor AT-800

EASA SIB CE-08-12R1

Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes - Possible Failure of a Transient Voltage Suppressor (TVS)

The Special Airworthiness Information Bulletin SAIB: CE-08-12R1 addresses a potential failure of a transient voltage suppressor (TVS) in Cirrus Design Corporation Models SR20 and SR22 airplanes. This failure may cause loss of NAV/COMM 1 functionality and produce short-term smoke and fumes in the cockpit, increasing pilot workload. The bulletin provides updated service information from Cirrus Design Corporation to mitigate this issue.

May 11, 2011
Safety Information BulletinMaintenanceSafety MgmtCirrus Design Corporation SR20Cirrus Design Corporation SR22

EASA SIB CE-08-14

Diamond Models DA 40 and DA 40F airplanes equipped with Garmin G1000 installations per Garmin Supplemental Type Certificate (STC) SA01254WI and STC SA01389WI - Possible Failure of a Transient Voltage Suppressor (TVS)

Special Airworthiness Information Bulletin SAIB: CE-08-14 is an FAA informational bulletin addressing a potential airworthiness concern for Diamond Models DA 40 and DA 40F airplanes equipped with Garmin G1000 installations under Garmin Supplemental Type Certificates SA01254WI and SA01389WI. The bulletin highlights possible failure of transient voltage suppressors (TVS) that may cause cockpit smoke, loud popping sounds, and loss of standby attitude indicator and audio panel functionality. This bulletin does not mandate corrective action but provides important safety information for operators of these aircraft.

May 11, 2011
Safety Information BulletinMaintenanceSafety MgmtDiamond DA 40Diamond DA 40F