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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA SIB CE-12-19

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.

Mar 2, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 500Cessna 501Cessna 550

EASA SIB FA-02-2012

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.

Feb 14, 2012
Safety Information BulletinFlight OpsSafety MgmtEmbraer EMB-500

EASA SIB SW-12-10R1

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.

Feb 10, 2012
Safety Information BulletinSafety MgmtMaintenanceEnstrom F-28AEnstrom F-28CEnstrom F-28FEnstrom 280Enstrom 280CEnstrom 280FEnstrom 280FX

EASA SIB CE-12-18

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.

Feb 10, 2012
Safety Information BulletinMaintenanceSafety MgmtHawker Beechcraft 33 BonanzaHawker Beechcraft 35 BonanzaHawker Beechcraft 36 Bonanza

EASA SIB NM-12-11

[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.

Feb 8, 2012
Safety Information BulletinMaintenanceSafety MgmtBoeing 737

EASA SIB CE-12-16

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.

Feb 3, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 510

EASA SIB CE-12-15

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.

Feb 1, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172SCessna 182TCessna T182TCessna 206HCessna T206H

EASA SIB CE-11-47R1

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.

Jan 31, 2012
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-12-14

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.

Jan 26, 2012
Safety Information BulletinMaintenanceSafety MgmtCessna 150Cessna 152Cessna 170Cessna 172Cessna 175Cessna 177Cessna 180Cessna 182Cessna 185Cessna 188Cessna 190Cessna 195Cessna 206Cessna 207Cessna 210Cessna T303Cessna 336Cessna 337

EASA SIB CE-12-13

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.

Jan 25, 2012
Safety Information BulletinMaintenanceSafety MgmtEclipse Aerospace EA500

EASA SIB 2012-01

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.

Jan 20, 2012
Safety Information BulletinSafety MgmtMaintenanceEurocopter AS 350Eurocopter AS 355

EASA SIB 2012-02

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.

Jan 5, 2012
Safety Information BulletinMaintenanceSafety MgmtMooney M20KPiper PA28-201TPiper PA34-220TPiper PA-28R-201T

EASA SIB 2011-30

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.

Dec 22, 2011
Safety Information BulletinSafety MgmtFlight OpsEurocopter EC 120 BEurocopter EC 130 B4

EASA SIB CASA-2011-07

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.

Dec 19, 2011
Safety Information BulletinMaintenanceSafety MgmtDiamond Canada DA20

EASA SIB 2011-29

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.

Dec 6, 2011
Safety Information BulletinFlight OpsTrainingSafety MgmtBombardier CRJ 100Bombardier CRJ 200Bombardier CRJ 440Bombardier Challenger 850Bombardier Challenger 600

EASA SIB CASA-2011-08

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.

Nov 21, 2011
Safety Information BulletinMaintenanceSafety MgmtBell 206L

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.

Nov 21, 2011
Safety Information BulletinMaintenanceSafety MgmtLearjet 31Learjet 31ALearjet 35Learjet 35ALearjet 36Learjet 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.

Nov 10, 2011
Safety Information BulletinMaintenanceSafety Mgmt

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.

Nov 9, 2011
Safety Information BulletinMaintenanceSafety MgmtM7 Aerospace SA226M7 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.

Nov 2, 2011
Safety Information BulletinMaintenanceSafety MgmtCessna 172RCessna 172S