EASA Regulations & Airworthiness Directives

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

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA SIB NM-12-20

Mar 20, 2012

[Correction] Carleton Technologies Inc. - Oxygen System Cylinder- and Valve Assemblies

The document titled '[Correction] Carleton Technologies Inc. - Oxygen System Cylinder- and Valve Assemblies' is a Special Airworthiness Information Bulletin (SAIB: NM-12-20) issued by the FAA. It addresses the correct operation of Carleton Technologies Inc. oxygen system cylinder and valve assemblies with part numbers B42365-1 and B43570-1, which are installed on various transport category airplanes. The bulletin provides guidance to ensure proper handling of the variable torque shutoff valve to maintain oxygen system effectiveness during emergencies.

Safety Information Bulletin
All aircraft

EASA SIB 2012-04

Mar 15, 2012

L´Hotellier Ball and Swivel Joints Quick Connectors — Positive Check of Control Surfaces

EASA Safety Information Bulletin SIB No. 2012-04 addresses the positive check of control surfaces for sailplanes, powered sailplanes, and other aircraft equipped with L'Hotellier ball and swivel joint quick connectors. This bulletin follows a fatal accident involving an Eiriavion PIK 20D sailplane in Belgium, highlighting the importance of ensuring proper connection of elevator controls during assembly. The bulletin references previous airworthiness directives issued by the German Civil Aviation Authority concerning these connectors but clarifies that these are not recognized by EASA as mandatory under European regulations.

Safety Information Bulletin
  • Eiriavion PIK 20D

EASA SIB HQ-12-07R1

Mar 12, 2012

Avox Systems, Inc. First Aid Kits - Contaminated Iodine Wipes

The FAA Special Airworthiness Information Bulletin SAIB: HQ-12-07R1 addresses the potential contamination of iodine wipes included in first aid kits sold by Avox Systems, Inc. These wipes, labeled as Applicator, Antiseptic or iodine/povidine prep pads, may affect aircraft required to carry emergency medical equipment under 14 CFR parts 91, 121, 125, and 135. The bulletin provides guidance for identifying affected wipes by lot number and part numbers associated with Avox first aid kits.

Safety Information Bulletin
All aircraft

EASA SIB 2012-03

Mar 7, 2012

Antonov An-26 Aeroplanes — Changes to Type Design, Airworthiness Limitations and Repairs

EASA Safety Information Bulletin 2012-03 addresses changes to the Antonov An-26 aeroplanes' type design, airworthiness limitations, and repair designs. It specifically applies to the Antonov An-26 series as listed in the Restricted Type Certificate Data Sheet EASA.IM.A.315. The bulletin informs operators about the status of life limit extensions and repair approvals related to the An-26 Instructions for Continued Airworthiness.

Safety Information Bulletin
  • Antonov An-26

EASA SIB CE-12-19

Mar 2, 2012

Cessna 500, 501 and 550 Aeroplanes — modified by Sierra Industries STC SA80RM or SA152RM

The Special Airworthiness Information Bulletin SAIB: CE-12-19 is an FAA informational bulletin concerning Cessna Aircraft Company Models 500, 501, and 550 airplanes modified with Sierra Industries Supplemental Type Certificates SA80RM or SA152RM. It addresses updated instructions for continued airworthiness related to the auxiliary fuel tank installed by these STCs. The bulletin highlights revised maintenance and inspection procedures to prevent fuel leaks in the auxiliary fuel system.

Safety Information Bulletin
  • Cessna 500
  • Cessna 501
  • Cessna 550

EASA SIB FA-02-2012

Feb 14, 2012

EMBRAER EMB-500 Aeroplanes - Static Port Heating System — Operational Checks

Flight Alert FA Nº 2/2012 – February 2, 2012 is an operational advisory for owners and operators of Embraer EMB-500 airplanes regarding the static port heating system. It addresses a hidden failure mode in the static port heaters that can cause misleading barometric altitude and airspeed readings on primary flight displays due to ice accretion. The alert provides updated procedures for operational checks to detect and correct this failure.

Safety Information Bulletin
  • Embraer EMB-500

EASA SIB SW-12-10R1

Feb 10, 2012

Enstrom 280, F-28 series Helicopters - Fuel Level Indication

The Special Airworthiness Information Bulletin SAIB: SW-12-10R1 is issued by the FAA to address fuel level indication issues in Enstrom Helicopter Corporation piston aircraft, including the F-28A, F-28C, F-28F, 280, 280C, 280F, and 280FX helicopter models. This bulletin informs operators about the risk of false fuel quantity readings that may lead to fuel exhaustion during flight. It provides safety information and recommendations to verify fuel quantity indications and maintain the fuel system properly.

Safety Information Bulletin
  • Enstrom F-28A
  • Enstrom F-28C
  • Enstrom F-28F
  • Enstrom 280
  • Enstrom 280C
  • Enstrom 280F
  • Enstrom 280FX

EASA SIB CE-12-18

Feb 10, 2012

Hawker Beechcraft 33, 35 and 36 Bonanza series Aeroplanes - Elevator Control Cable Condition

Special Airworthiness Information Bulletin SAIB: CE-12-18 is an FAA informational bulletin addressing the condition of the forward elevator control cable assembly on Hawker Beechcraft 33, 35, and 36 Bonanza series airplanes. It highlights the importance of inspecting the elevator control cables, especially where they route through closely spaced pulleys forward of the instrument panel. The bulletin also applies broadly to any airplane model with cable-driven flight controls.

Safety Information Bulletin
  • Hawker Beechcraft 33 Bonanza
  • Hawker Beechcraft 35 Bonanza
  • Hawker Beechcraft 36 Bonanza

EASA SIB NM-12-11

Feb 8, 2012

[Correction] B/E Aerospace (UK) G4B galleys on Boeing 737 aeroplanes - Possible Latch Failure on Galley Cabinets

Correction B/E Aerospace (UK) G4B galleys on Boeing 737 aeroplanes - Possible Latch Failure on Galley Cabinets is a Special Airworthiness Information Bulletin issued by the FAA addressing a potential latch failure issue on B/E Aerospace G4B galley cabinets installed on Boeing 737 airplanes. The bulletin highlights concerns about galley cabinet latch plates affixed with adhesive-only fasteners that may degrade over time, posing safety risks during flight operations.

Safety Information Bulletin
  • Boeing 737

EASA SIB CE-12-16

Feb 3, 2012

Cessna 510 Aeroplanes — Elevator Trim Tab Control System

Special Airworthiness Information Bulletin SAIB: CE-12-16 is an FAA informational bulletin addressing elevator trim tab control system issues on Cessna Model 510 airplanes. It alerts operators to reports of pitch trim freezing in flight and provides guidance to reduce the likelihood of this problem. The bulletin references specific Cessna service letters aimed at improving drainage and sealing in the tailcone and vertical stabilizer areas.

Safety Information Bulletin
  • Cessna 510

EASA SIB CE-12-15

Feb 1, 2012

Cessna 172R/S, (T)182T and (T)206H Aeroplanes with Garmin G1000 Avionics - Master Switch Failure

The Special Airworthiness Information Bulletin SAIB: CE-12-15 is an FAA informational bulletin addressing a potential failure of the avionics master switch on Cessna 172R, 172S, 182T, T182T, 206H, and T206H airplanes equipped with Garmin G1000 avionics. The bulletin highlights a risk of accelerated switch failure that could lead to loss of avionics equipment, though essential flight and landing systems remain powered through alternate electrical sources.

Safety Information Bulletin
  • Cessna 172R
  • Cessna 172S
  • Cessna 182T
  • Cessna T182T
  • Cessna 206H
  • Cessna T206H

EASA SIB CE-11-47R1

Jan 31, 2012

Goodyear Aviation Tires - Butyl Rubber Inner Tube Failure

The Special Airworthiness Information Bulletin (SAIB) CE-11-47R1 titled 'Goodyear Aviation Tires - Butyl Rubber Inner Tube Failure' informs operators, pilots, and manufacturers about potential failures of Goodyear butyl rubber inner tubes used in aviation tires sized 7.00-8.00-6. The bulletin highlights that these failures are not limited to cold weather operations and currently do not warrant mandatory airworthiness directives under 14 CFR part 39.

Safety Information Bulletin
All aircraft

EASA SIB CE-12-14

Jan 26, 2012

Cessna Aeroplanes - Alternative Methods of Compliance (AMOC) for FAA AD 2011-10-09

The document titled 'Cessna Aeroplanes - Alternative Methods of Compliance (AMOC) for FAA AD 2011-10-09' is a Special Airworthiness Information Bulletin (SAIB CE-12-14) issued by the FAA. It addresses three alternative methods of compliance for FAA Airworthiness Directive 2011-10-09, which affects multiple Cessna airplane models including the 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190, 195, 206, 207, 210, T303, 336, and 337 series. The AMOCs provide more efficient and cost-effective procedures for seat track inspections and repairs while maintaining safety standards.

Safety Information Bulletin
  • Cessna 150
  • Cessna 152
  • Cessna 170
  • Cessna 172
  • Cessna 175
  • Cessna 177
  • Cessna 180
  • Cessna 182
  • Cessna 185
  • Cessna 188
  • Cessna 190
  • Cessna 195
  • Cessna 206
  • Cessna 207
  • Cessna 210
  • Cessna T303
  • Cessna 336
  • Cessna 337

EASA SIB CE-12-13

Jan 25, 2012

Eclipse Aerospace, Inc. EA500 aeroplanes - Aileron Joints Inspection / Replacement

The Special Airworthiness Information Bulletin SAIB: CE-12-13 is an FAA informational bulletin addressing the inspection and replacement of aileron joints on Eclipse Aerospace, Inc. EA500 model series aircraft. It provides guidance for inspecting the aileron joint assemblies and replacing parts with redesigned components to address increased lateral stick forces reported on these aircraft.

Safety Information Bulletin
  • Eclipse Aerospace EA500

EASA SIB 2012-01

Jan 20, 2012

WITHDRAWN - REPLACED BY EASA AD 2013-0281R1

EASA Safety Information Bulletin 2012-01 is an informational bulletin addressing a potential unsafe condition related to the optional position strobe light installation (modification OP0811) on Eurocopter AS 350 and AS 355 helicopters. The issue involves the power supply unit and electrical wiring located in the baggage compartment, which could cause electrical sparks and potentially lead to fire if damaged and in contact with flammable substances. This bulletin informs operators and owners about the safety concern and recommends precautionary measures.

Safety Information Bulletin
  • Eurocopter AS 350
  • Eurocopter AS 355

EASA SIB 2012-02

Jan 5, 2012

Continental (L)TSIO-360 Engines - Air Reference Tube failures

EASA Safety Information Bulletin SIB No. 2012-02 addresses air reference tube failures in Continental TSIO-360 and LTSIO-360 series engines, commonly installed on Mooney Model M20K and various Piper aircraft models including PA28-201T and PA34-220T. The bulletin reports a broken aluminium air reference tube Part Number 641082 found on a Piper PA-28R-201T and clarifies that the failed tube was not a genuine Continental Motors part. This document provides safety information and recommendations but does not mandate regulatory action.

Safety Information Bulletin
  • Mooney M20K
  • Piper PA28-201T
  • Piper PA34-220T
  • Piper PA-28R-201T

EASA SIB 2011-30

Dec 22, 2011

WITHDRAWN - RECOMMENDATIONS NOT NEEDED ANYMORE

EASA Safety Information Bulletin 2011-30 is an informational bulletin addressing a risk of flight control jamming due to lack of cyclic friction on Eurocopter EC 120 B and EC 130 B4 helicopters modified with specific SAGEM Avionics autopilot systems. It highlights a discrepancy between the Rotorcraft Flight Manual and the Rotorcraft Flight Manual Supplement regarding cyclic friction settings. The bulletin aims to alert operators and pilots of these helicopters to this safety concern without imposing mandatory recommendations.

Safety Information Bulletin
  • Eurocopter EC 120 B
  • Eurocopter EC 130 B4

EASA SIB CASA-2011-07

Dec 19, 2011

Diamond Canada DA20 aeroplanes — NLG Fork Assembly Inspection / Replacement

Transport Canada Civil Aviation Safety Alert CASA 2011-07 is a safety alert addressing a potential unsafe condition involving cracking in the nose landing gear (NLG) fork assembly, part number 20-3220-08-00, on Diamond Canada DA20-A1 and DA20-C1 aeroplanes. The alert informs owners and maintainers about the discovery of cracks above the axle hole during routine inspections and provides guidance on inspection and replacement procedures.

Safety Information Bulletin
  • Diamond Canada DA20

EASA SIB 2011-29

Dec 6, 2011

Operation of Bombardier CRJ 100/200/440 and Challenger 850 and 600 series aircraft in cold weather or icing conditions during take-off.

EASA Safety Information Bulletin 2011-29 is an informational document addressing the operation of Bombardier CRJ 100/200/440 and Challenger 850 and 600 series aircraft in cold weather or icing conditions during take-off. It highlights the importance of adhering to Aircraft Flight Manual limitations and procedures, particularly regarding wing anti-ice system use and rotation rates. The bulletin also promotes pilot training initiatives such as Bombardier's Take-Off Safety Enhancement campaign to improve safety during winter operations.

Safety Information Bulletin
  • Bombardier CRJ 100
  • Bombardier CRJ 200
  • Bombardier CRJ 440
  • Bombardier Challenger 850
  • Bombardier Challenger 600

EASA SIB CASA-2011-08

Nov 21, 2011

Bell Helicopter Textron Canada (BHTC) 206L Series Helicopters — Main Rotor Blade Separation In-Flight

Bell Helicopter Textron Canada (BHTC) 206L Series Helicopters — Main Rotor Blade Separation In-Flight is a Transport Canada Civil Aviation Safety Alert (CASA 2011-08) addressing main rotor blade failures on Bell 206L series helicopters, including models 206L-1, L-3, and L-4. The alert follows two incidents involving in-flight separation of main rotor blades, one in the United States in 2008 and another in Canada in 2011. It references Alert Service Bulletin (ASB) 206L-09-159 Rev A, which provides inspection procedures for affected main rotor blades.

Safety Information Bulletin
  • Bell 206L