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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA SIB 2009-25

EMBRAER EMB-135 and EMB-145 Series Aeroplanes — WindowsTM version of Personal Computer Memory Access (PCMA) Software on the AH-800 Attitude & Heading Reference System (AHRS)

EASA Safety Information Bulletin SIB No. 2009-25 is an informational bulletin concerning EMBRAER EMB-135 and EMB-145 series aeroplanes equipped with the AH-800 Attitude & Heading Reference System (AHRS). It announces the availability of a new WindowsTM version of the Personal Computer Memory Access (PCMA) software used for ground support and configuration of the AH-800 AHRS. The bulletin highlights the risk of incorrect AHRS configuration potentially causing an inverted attitude display, which could lead to loss of control.

Aug 10, 2009
Safety Information BulletinMaintenanceSafety MgmtEmbraer EMB-135Embraer EMB-145

EASA SIB CE-09-47

Garmin G1000, Perspective—¢, Prodigy—¢ Integrated Flight Decks with Garmin GFC 700 Autopilot

Special Airworthiness Information Bulletin SAIB CE-09-47 is an FAA informational bulletin addressing an issue with Garmin G1000, Perspective™, and Prodigy™ Integrated Flight Decks installed with the Garmin GFC 700 autopilot. It informs pilots about a potential mismatch between automatically tuned VOR or LOC/ILS frequencies and those published on approach charts or NOTAMs, which can cause incorrect course indications during approaches. This bulletin applies to aircraft equipped with these specific Garmin integrated flight decks and autopilot systems.

Aug 10, 2009
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2009-24

Lycoming O-235 — Cylinder barrel — Inspection

EASA Safety Information Bulletin SIB No: 2009-24 is an informational bulletin addressing inspection of cylinder barrels on Lycoming O-235 engines used in various aircraft. It informs operators about the risk of circumferential cracks in cylinder barrels that can cause oil leaks and potential engine failure. The bulletin highlights improved cylinder designs and provides inspection recommendations to detect corrosion and cracks.

Aug 6, 2009
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-09-41

Hawker Beechcraft Model 390 aeroplanes / Goose Neck Type Latches, Replacement.

Special Airworthiness Information Bulletin SAIB CE-09-41 is an FAA information bulletin addressing an airworthiness concern on Hawker Beechcraft Model 390 airplanes. It recommends replacing the goose neck type latches on the aft baggage and maintenance doors with a redesigned rotary pin style latch as detailed in Service Bulletin SB 52-3864. This bulletin is informational and does not mandate regulatory action under 14 CFR part 39.

Aug 5, 2009
Safety Information BulletinMaintenanceSafety MgmtHawker Beechcraft 390

EASA SIB CE-09-39

Cessna (T)U206 aeroplanes with Wing Tip Tanks - STC SA4366WE

The Special Airworthiness Information Bulletin FAA Aircraft Certification Service SAIB CE-09-39 addresses the maximum landing gross weight limitation for Cessna U206F, U206G, TU206F, and TU206G series airplanes equipped with Flint Aero wing tip tanks installed under Supplemental Type Certificate SA4366WE. It clarifies the maximum landing weight as documented in Flint Aero Airplane Flight Manual Supplement Revision B. This bulletin provides safety information but does not mandate regulatory action.

Jul 31, 2009
Safety Information BulletinSafety MgmtCessna U206FCessna U206GCessna TU206FCessna TU206G

EASA SIB CE-09-16

Main Landing Gear Torque Tubes and Structural Inspection Document - Cessna Twin Engine Aeroplanes.

The Special Airworthiness Information Bulletin SAIB: CE-09-16 is an FAA informational bulletin addressing the inspection of main landing gear torque tubes on various Cessna twin engine aircraft models including the 310 series, 320 series, 335, 340 series, 401 series, 402 series, 411 series, 414, and 421 series. It highlights the importance of inspecting the torque tubes for fatigue cracks and ensuring proper landing gear rigging to maintain safe operation. This bulletin is not mandatory and does not constitute an airworthiness directive.

Jul 30, 2009
Safety Information BulletinMaintenanceSafety MgmtCessna 310Cessna 320Cessna 335Cessna 340Cessna 401Cessna 402Cessna 411Cessna 414Cessna 421

EASA SIB CE-09-42

Cessna Landing Light, Beacon Light, and Taxi Light switches on Cessna 100, 200, and 300 series aeroplanes.

Special Airworthiness Information Bulletin SAIB: CE-09-42 is an FAA information bulletin addressing the mandatory replacement intervals for Landing Light, Beacon Light, and Taxi Light switches on Cessna 100, 200, and 300 series airplanes. The bulletin highlights concerns related to switch failures causing overheating and smoke in the cockpit, referencing Cessna service bulletins MEB09-3 and SEB09-6. It provides guidance on inspection and replacement intervals to maintain airworthiness.

Jul 27, 2009
Safety Information BulletinMaintenanceSafety MgmtCessna 100Cessna 200Cessna 300

EASA SIB NE-09-31R1

Hawker Beechcraft Model 60 "Duke" aeroplanes with Lycoming TIO-541-E1C4 engines - Kelly Aerospace Energy Systems (KAES) T1879 Rebuilt Turbocharger

The Special Airworthiness Information Bulletin SAIB NE-09-31R1 provides information regarding the Hawker Beechcraft Model 60, 60A, and 60B (Duke) aircraft equipped with Lycoming TIO-541-E1C4 engines. It addresses a potential issue with the Kelly Aerospace Energy Systems (KAES) rebuilt T1879 turbocharger, part number 407540-9003, serial number JAR00401. The bulletin informs operators about a production discrepancy affecting this specific turbocharger model.

Jul 10, 2009
Safety Information BulletinMaintenanceSafety MgmtHawker Beechcraft 60Hawker Beechcraft 60AHawker Beechcraft 60B

EASA SIB CE-09-38

Mooney M20 Series - Installation (FAA STC SA4443NM) of Wing Tip Fairings

The Special Airworthiness Information Bulletin (SAIB) CE-09-38 issued by the FAA provides information regarding the installation of wing tip fairings under Supplemental Type Certificate (STC) SA4443NM on Mooney M20 series airplanes, including models M20B, M20C, M20D, M20E, M20F, M20J, and M20K. The bulletin addresses an airworthiness concern related to the lighting configuration on these aircraft when equipped with the STC wing tip fairings. It is not an airworthiness directive and does not mandate mandatory actions.

Jul 10, 2009
Safety Information BulletinMaintenanceSafety MgmtMooney M20BMooney M20CMooney M20DMooney M20EMooney M20FMooney M20JMooney M20K

EASA SIB CE-04-34

True Flight Aerospace LLC (Grumman, American General, Tiger) AA-5A, AA-5B and AG-5B - Horizontal Stabilizer Forward Spar Carry-through Support Structure

Special Airworthiness Information Bulletin No. CE-04-34 is an informational bulletin issued by the FAA regarding Tiger Aircraft LLC (American General) Model AA-5A, AA-5B, and AG-5B airplanes. It addresses a safety concern involving cracks and deformation found in the horizontal stabilizer forward spar carry-through support structure of these aircraft. The bulletin provides inspection guidance but does not mandate any regulatory action at this time.

Jul 8, 2009
Safety Information BulletinMaintenanceSafety MgmtGrumman AA-5AGrumman AA-5BGrumman AG-5BAmerican General AA-5AAmerican General AA-5BAmerican General AG-5BTiger AA-5ATiger AA-5BTiger AG-5B

EASA SIB SW-09-36

Fuel - Robinson Helicopter Company Hot Weather Operation

The Special Airworthiness Information Bulletin SAIB SW-09-36 is an FAA informational bulletin addressing fuel vapor issues during hot weather operations in Robinson Helicopter Company Model R44 II helicopters. It alerts operators to the potential for fuel vapor formation at high ambient temperatures and altitudes, which can cause engine power loss. The bulletin provides guidance based on factory testing and operational experience.

Jul 2, 2009
Safety Information BulletinFlight OpsSafety MgmtRobinson Helicopter Company R44 II

EASA SIB CE-09-32

Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount

The Special Airworthiness Information Bulletin Navigation: Cirrus Aircraft Under-Glareshield GPS/WAAS Antenna Mount is an FAA informational bulletin addressing airworthiness concerns for Cirrus Models SR20 and SR22 airplanes equipped with GPS/WAAS antennas mounted under the glareshield. It highlights potential issues with antenna mounting robustness and signal loss due to airframe shadowing that may affect GPS/WAAS navigation service. The bulletin applies specifically to Cirrus aircraft using the original under-glareshield mounting location for GPS/WAAS antennas.

Jun 30, 2009
Safety Information BulletinSafety MgmtCirrus SR20Cirrus SR22

EASA SIB 2009-20

Lifesaving Systems Corp. D-Lok Hook of the Rescue Hoist — Inspection / Replacement

EASA Safety Information Bulletin 2009-20 is an advisory document concerning the Lifesaving Systems Corp. D-Lok Hook assemblies, Part Numbers 410-A and 410-F, used on rescue hoists in various helicopters. It informs operators about detected manufacturing discrepancies in hooks from lots 208 and 1108, which may be installed on multiple helicopter types including those with Breeze Hoist installations. The bulletin supports the inspection and replacement actions outlined in Goodrich Service Bulletin 42315-489-01 Revision 1.

Jun 29, 2009
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB AV-2007-03R1

Flexible Fuel Manifolds - Pratt & Whitney Canada PW 100 Series Engines

Transport Canada Civil Aviation Service Difficulty Advisory AV-2007-03R1 addresses issues with the flexible fuel manifolds installed on Pratt & Whitney Canada PW100 series engines. The advisory highlights problems with improperly torqued manifold nuts leading to fuel leaks and engine fires. It provides guidance to ensure proper installation and maintenance of these fuel manifolds to maintain engine safety and reliability.

Jun 22, 2009
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2009-19

Standard Practices - Turbine Engines Critical Parts Cleaning

EASA Safety Information Bulletin 2009-19 is an advisory document addressing the cleaning of critical rotating parts in all turbine aircraft engines, including models such as the Pratt & Whitney PW2000 series. It highlights the risk of uncontained engine failures caused by aggressive grit blast cleaning during maintenance. The bulletin aligns with FAA Special Airworthiness Information Bulletin NE-09-34 and applies these recommendations to turbine engines installed on aircraft registered in European Union Member States and associated countries.

Jun 18, 2009
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB SW-09-30

Enstrom Helicopters - Engine Pylon Failures

The Special Airworthiness Information Bulletin SAIB: SW-09-30 issued by the FAA alerts owners and operators of Enstrom Helicopter Corporation Models F28F, 280F, and 280FX about a potential airworthiness concern involving cracks in the engine pylon near the belt tensioning assembly mounting bracket. This bulletin provides information on recent reports of cracked pylons and references previous Enstrom service communications addressing this issue. The bulletin is informational and does not mandate regulatory action.

Jun 15, 2009
Safety Information BulletinMaintenanceSafety MgmtEnstrom F28FEnstrom 280FEnstrom 280FX

EASA SIB 2009-14

Garmin Global Positioning System (GPS) Navigation Units (400W / 500W series and GNS 480) — Upgrade to main unit software and GPS software

EASA Safety Information Bulletin SIB No. 2009-14 provides information on a software upgrade for Garmin Global Positioning System (GPS) Navigation Units, specifically the 400W / 500W series and GNS 480 models. These GPS units are installed on various Part 23 certificated aeroplanes and Part 27 certificated helicopters. The bulletin addresses software improvements to enhance navigation accuracy and reliability.

Jun 15, 2009
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2009-13

WITHDRAWN - SEE FAA AD 2010-04-05

EASA Safety Information Bulletin SIB No. 2009-13 is an informational bulletin regarding the inspection of McCauley 1A103/TCM propeller hubs for cracking. It applies to all serial numbers of these propellers, commonly installed on Cessna 152/A152 and Reims Aviation F152/FA152 aircraft. The bulletin highlights findings of cracks near mounting bolt holes and references FAA AD 2003-12-05 and McCauley Service Bulletin ASB 221D for inspection and rework procedures.

Jun 15, 2009
Safety Information BulletinMaintenanceSafety MgmtCessna 152Cessna A152Reims Aviation F152Reims Aviation FA152

EASA SIB 2009-16

Misinterpretation of ACAS Resolution Advisory (RA) Aural Annunciation Messages

EASA Safety Information Bulletin SIB No: 2009-16 addresses the misinterpretation of ACAS Resolution Advisory (RA) aural annunciation messages, particularly the 'Adjust Vertical Speed, Adjust' (AVSA) message. This bulletin applies to all turbine-powered aeroplanes equipped with ACAS II (TCAS II Version 7.0) that meet specific weight or passenger seating criteria, including commercial and non-commercial operations. The document highlights the importance of correct pilot responses to RA messages to maintain safe separation from other aircraft.

Jun 9, 2009
Safety Information BulletinFlight OpsSafety Mgmt