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EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:All Airbus A320286 Airbus A321285 Airbus A319253 Airbus A350224 Airbus A330221 Airbus A318189 Airbus A380182 Boeing 737175 Airbus A340141 Airbus A350-941134 Airbus BD-500 (A220 Series)123 Airbus Helicopters AS 332119 Airbus Helicopters EC 225116 Airbus Helicopters SA 330116 Boeing 787116 Show all...

EASA SIB NM-11-48

Learjet Inc. 31, 31A, 35, 35A, 36 and 36A aeroplanes - Wing Transverse Duct Assembly

The FAA Special Airworthiness Information Bulletin SAIB: NM-11-48 provides guidance for owners and operators of Learjet Inc. Model 31, 31A, 35, 35A (C-21A), 36, and 36A airplanes regarding inspection and potential replacement of the wing transverse duct assembly. This bulletin addresses possible restricted airflow through the duct that could reduce the anti-ice capability of the right wing leading edge. The document is informational and does not mandate regulatory action.

Safety Information Bulletin

Learjet 31
Learjet 31A
Learjet 35
Learjet 35A
Learjet 36
Learjet 36A

EASA SIB 2009-39R1

Contaminated Halon 1211 (BCF) and 1301 (BTM) Supplies

EASA Safety Information Bulletin SIB No: 2009-39R1 addresses the issue of contaminated Halon 1211 (BCF) and Halon 1301 (BTM) supplies used in aircraft fire extinguishers and ground fire extinguishers at airports. The contamination was linked to falsified sample test reports by a supplier, affecting handheld fire extinguishers typically found in aircraft cabins and some engine/APU systems. Several related EASA Airworthiness Directives remain valid to remove affected handheld Halon 1211 extinguishers from service, but no directives have been issued for engine or APU systems.

Safety Information Bulletin

EASA SIB CE-12-08

M7 Aerospace (formerly Fairchild, Swearingen) SA226 and SA227 aeroplanes - Elevator Control System

M7 Aerospace (formerly Fairchild, Swwearingen) SA226 and SA227 aeroplanes - Elevator Control System is a Special Airworthiness Information Bulletin (SAIB CE-12-08) issued by the FAA. It addresses corrosion concerns in the pitch trim actuator fuselage fittings, part number 27-43060, on M7 Aerospace Models LP SA226 and SA227 series airplanes. The bulletin provides inspection and repair recommendations but does not mandate regulatory action.

Safety Information Bulletin

M7 Aerospace SA226
M7 Aerospace SA227

EASA SIB CE-12-03

Cessna Model 172R and 172S Fuel Control; Engine Performance with the Throttle Control at Idle

The Special Airworthiness Information Bulletin SAIB: CE-12-03 is an informational document issued by the FAA regarding fuel control and engine performance at idle throttle settings for 1996 and later Cessna Model 172R and 172S reciprocating engine airplanes. It addresses concerns about proper engine operation when the throttle is at idle and clarifies what constitutes idle engine performance. The bulletin is not an airworthiness directive and does not impose mandatory requirements.

Safety Information Bulletin

Cessna 172R
Cessna 172S

EASA SIB CE-11-29R1

Cessna 414A and 421C, if modified by S-TEC Corporation STC - Flight Control System

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-29R1 addresses flight control system concerns for Cessna 414A and 421C aircraft modified by S-TEC Corporation Supplemental Type Certificates SA08996AC-D, SA7787SW-D, and SA7790SW-D with optional trim installed. The bulletin provides guidance on inspecting rudder trim tab blocks and phenolic blocks along the flight control system to prevent wear and ensure proper rudder travel. This information bulletin is advisory and does not mandate regulatory action.

Safety Information Bulletin

Cessna 414A
Cessna 421C

EASA SIB 2011-26

Bombardier (formerly Canadair) CL-600-2B19 - Heading Deviations

EASA Safety Information Bulletin SIB No: 2011-26 is an advisory document addressing possible heading deviations in Bombardier (formerly Canadair) CL-600-2B19 Regional Jet aircraft caused by surface magnetic anomalies. It references FAA Safety Alert for Operators SAFO 11006 and applies to all serial numbers of the CL-600-2B19. The bulletin highlights the risk of heading discrepancies during surface operations in areas with known or suspected magnetic field anomalies and supports FAA recommendations to mitigate these risks.

Safety Information Bulletin

Bombardier CL-600-2B19

EASA SIB AV-11-2011

EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes - Flap or Slat Torque Tubes Improper Installation

The document titled EMBRAER ERJ 170/175 and ERJ 190/195 Aeroplanes - Flap or Slat Torque Tubes Improper Installation is an Aviation Alert (AV Nº 11/2011) issued on October 4, 2011. It addresses the correct installation of flap and slat torque tubes on EMBRAER ERJ-170/175 and ERJ-190/195 airplanes to prevent system failures. The alert informs operators about revisions to Aircraft Maintenance Manual (AMM) tasks related to these components.

Safety Information Bulletin

Embraer ERJ 170
Embraer ERJ 175
Embraer ERJ 190
Embraer ERJ 195

EASA SIB SW-11-61

Honeywell International (formerly Bendix King) KRA 405B Radar Altimeter — Erroneous Altitude Information

The FAA Special Airworthiness Information Bulletin SAIB: SW-11-61 addresses a potential undetected failure condition in the Honeywell International (formerly Bendix King) KRA 405B Radar Altimeter. This condition may cause the radar altimeter to provide erroneous altitude information without warning, affecting aircraft systems that rely on radar altitude data. The bulletin applies to aircraft equipped with the KRA 405B Radar Altimeter system.

Safety Information Bulletin

EASA SIB NM-11-60

Hawker Beechcraft (formerly Raytheon, British Aerospace) BAe125 and Hawker Series aeroplanes — Nose Landing Gear Drag Stay Assembly

The Special Airworthiness Information Bulletin SAIB: NM-11-60 issued by the FAA addresses an airworthiness concern related to the nose landing gear drag stay assembly on certain Hawker Beechcraft Corporation BAe.125 Series 800A, 800B, 1000A, and 1000B airplanes, as well as Hawker 750, 800, 800XP, 850XP, 900XP, and 1000 models. The bulletin informs operators about issues with slow extension of the nose landing gear and provides guidance for modification to improve performance.

Safety Information Bulletin

Hawker Beechcraft BAe125 Series 800A
Hawker Beechcraft BAe125 Series 800B
Hawker Beechcraft BAe125 Series 1000A
Hawker Beechcraft BAe125 Series 1000B
Hawker Beechcraft Hawker 750
Hawker Beechcraft Hawker 800
Hawker Beechcraft Hawker 800XP
Hawker Beechcraft Hawker 850XP
Hawker Beechcraft Hawker 900XP
Hawker Beechcraft Hawker 1000

EASA SIB SAFO11008

Robinson R44 helicopters — Hydraulic Flight Control System Boost Servos

Robinson R44 helicopters — Hydraulic Flight Control System Boost Servos is a Safety Alert for Operators (SAFO 11008) issued by the Federal Aviation Administration. It addresses concerns regarding the hydraulic-boost servos on hydraulic system-equipped Robinson R44 helicopters following a fatal accident in Australia. The alert highlights the Australian Transport Safety Bureau's Safety Advisory Notice AO-2011-016-SAN-001 related to potential issues with flight control system components.

Safety Information Bulletin

Robinson R44

EASA SIB CE-11-57

Air Tractor, Inc. AT-400 and AT-402 Series Aeroplanes — Engine Mount Section

The Special Airworthiness Information Bulletin SAIB: CE-11-57 is an FAA informational bulletin addressing an airworthiness concern for Air Tractor, Inc. Models AT-400, AT-400A, AT-402, AT-402A, and AT-402B airplanes. It highlights the need for inspections of the engine mount attach tubes for fatigue cracking, particularly at the left hand firewall attach location, but does not mandate regulatory action. The bulletin provides guidance on inspection procedures and reporting for affected aircraft under Type Certificate Data Sheets A9SW and A17SW.

Safety Information Bulletin

Air Tractor AT-400
Air Tractor AT-400A
Air Tractor AT-402
Air Tractor AT-402A
Air Tractor AT-402B

EASA SIB 2011-25

Repair and/or Fabric Recovering of Rudder and Elevator

EASA Safety Information Bulletin 2011-25 addresses the repair and fabric recovering of rudders and elevators on RUAG Aerospace Dornier 228 series aeroplanes. It highlights incidents where fabric skin detached due to improper attachment not following the Structural Repair Manual and Aircraft Maintenance Manual procedures. The bulletin provides guidance to ensure repairs and fabric recoveries are performed correctly to maintain airworthiness.

Safety Information Bulletin

RUAG Aerospace Dornier 228

EASA SIB NE-11-54

Continental Motors (formerly TCM) Engines - Propeller Strikes and Hydraulic Locks

The Special Airworthiness Information Bulletin SAIB NE-11-54 is an FAA advisory regarding Continental Motors (formerly Teledyne Continental Motors) direct drive and geared reciprocating engines. It addresses recommended inspections following propeller strikes or hydraulic lock incidents to ensure engine safety and reliability. This bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

Safety Information Bulletin

EASA SIB CE-11-50

Cirrus Design Corporation SR20, SR22 and SR22T Aeroplanes — Partial Asymmetric Flap and Flap Actuator Over-Extension

The Cirrus Design Corporation SR20, SR22 and SR22T Aeroplanes — Partial Asymmetric Flap and Flap Actuator Over-Extension is a Special Airworthiness Information Bulletin issued by the FAA to alert owners and installers about a flap actuator over-extension issue affecting Cirrus SR20, SR22, and SR22T aircraft. This bulletin highlights a potential flap actuator rod end bending and partial asymmetric flap condition that could occur due to a 0-percent proximity sensor failure. The bulletin provides information and recommendations but does not mandate regulatory action.

Safety Information Bulletin

Cirrus SR20
Cirrus SR22
Cirrus SR22T

EASA SIB CE-11-49

Air Tractor, Inc. AT-802, AT-802A Elevator Tab Control System

The Special Airworthiness Information Bulletin SAIB: CE-11-49 is an FAA informational bulletin addressing the elevator tab control system on Air Tractor, Inc. Models AT-802 and AT-802A airplanes. It highlights an airworthiness concern related to the elevator trim actuator attach clamp assembly bracket and provides guidance on inspection and lubrication of the elevator trim control system. The bulletin is not mandatory and does not constitute an airworthiness directive.

Safety Information Bulletin

Air Tractor AT-802
Air Tractor AT-802A

EASA SIB AV-06-2011

Superseded by ANAC Flight Alert (FA) No. 24/2012

The ANAC Flight Alert AV Nº 06/2011, issued on August 18, 2011, addresses the risk of brake carbon disk failure on EMBRAER ERJ-170/175 and ERJ-190/195 aircraft. It informs operators about potential damage to carbon disk brakes that can lead to debris contamination on runways and possible engine ingestion or landing gear malfunction. The document provides updated inspection procedures to detect and prevent brake disintegration events.

Safety Information Bulletin

Embraer ERJ-170
Embraer ERJ-175
Embraer ERJ-190
Embraer ERJ-195

EASA SIB 2011-22

Ground and Airborne Icing

EASA Safety Information Bulletin SIB No: 2011-22 titled 'Ground and Airborne Icing' addresses safety concerns related to aircraft operations in freezing rain and freezing drizzle conditions. It applies to all aircraft certificated in any category and highlights that some aircraft certified under Appendix C to CS 25 may not be adequately protected against super-cooled large droplets (SLD) icing conditions. The bulletin provides guidance for European operators and flight crews to enhance safety during ground and airborne icing scenarios.

Safety Information Bulletin

EASA SIB 2011-21

Aircraft with Floats - Safety Best Industry Practices

EASA Safety Information Bulletin SIB No: 2011-21 is a safety advisory addressing all aircraft equipped with floats, including floatplanes and helicopters. It endorses Transport Canada Civil Aviation's Safety Alert CASA 2011-03, which promotes voluntary adoption of best industry practices to enhance floatplane safety. The bulletin highlights the importance of safety measures such as personal flotation devices and emergency egress training.

Safety Information Bulletin

EASA SIB CE-11-43

American Champion (formerly Bellanca, Aeronca) Model 7 and 8 series aeroplanes - Possible Interference with Flight Controls

Special Airworthiness Information Bulletin SAIB: CE-11-43 is an FAA informational bulletin addressing possible flight control interference in American Champion Aircraft Corporation Models 7EC, 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC airplanes. The bulletin highlights incidents where loose objects, such as emergency door jettison pins and seat belt buckle components, caused partial control jams during flight. It provides safety information and service letter references to mitigate these risks.

Safety Information Bulletin

American Champion 7EC
American Champion 7ECA
American Champion 7GCAA
American Champion 7GCBC
American Champion 7KCAB
American Champion 8KCAB
American Champion 8GCBC

EASA SIB 2011-17

Disassembly of Engines following In-Flight Shutdown with Indication of Critical Part Failure

EASA Safety Information Bulletin SIB No. 2011-17 provides guidance on the disassembly of engines following an in-flight shutdown (IFSD) when there is an indication of critical part failure. It applies to maintenance and continued airworthiness management organisations working on engines with critical parts installed on commercial air transport aircraft. The bulletin highlights the importance of a forensic teardown to investigate failures of critical engine parts, such as turbines and rotors, to ensure thorough root cause analysis and proper handling of affected components.

Safety Information Bulletin