Sign in Create account

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 2009-27

EUROCOPTER - Magnetic Particles Contamination in the Oil System of Power Transmission Assemblies

EASA Safety Information Bulletin SIB No: 2009-27 addresses magnetic particles contamination in the oil system of power transmission assemblies, specifically affecting Eurocopter AS332 L2 and EC225LP helicopters. The bulletin follows an accident investigation and updates maintenance procedures to improve gearbox debris identification and response. It recommends operators incorporate Eurocopter Safety Information Notice 2075-S-63 Revision 0 into their maintenance manuals.

Safety Information Bulletin

Eurocopter AS332 L2
Eurocopter EC225LP

EASA SIB 2009-08

ZODIAC Monogram Systems (formerly Weber) Coffeemaker CM121 — Electrical Burning Smell

EASA Safety Information Bulletin SIB No: 2009-08 addresses an electrical burning smell issue reported in ZODIAC Monogram Systems (formerly Weber) CM121 coffeemakers installed on Boeing 737 series aeroplanes. The bulletin provides safety recommendations based on the manufacturer's Service Bulletin 870130-25-2151 Revision 1 for wire terminal replacement to mitigate the problem. This information bulletin is intended to enhance safety by advising operators of affected aircraft to follow the corrective actions.

Safety Information Bulletin

Boeing 737

EASA SIB 2009-26

Lifesaving Systems Corporation (LSC) D-Lok Hook installed on Rescue Hoists — Inspection / Replacement

EASA Safety Information Bulletin 2009-26 addresses the inspection and replacement of Lifesaving Systems Corporation (LSC) D-Lok Hooks installed on rescue hoists, specifically those with Part Numbers 410-A and 410-F. These hooks, used on various helicopters including installations by Goodrich and Breeze-Eastern, were found to have material irregularities due to a manufacturing change from forged to cast material. The bulletin informs operators about the associated Airworthiness Directives and the need for compliance.

Safety Information Bulletin

EASA SIB CE-09-46

Cirrus SR20 and SR22 Aeroplanes - Nose Landing Gear Cracking

The Special Airworthiness Information Bulletin SAIB: CE-09-46 is an FAA informational bulletin addressing nose landing gear cracking concerns on Cirrus Design Corporation Models SR20 and SR22 airplanes. It highlights observed cracking and nose gear collapses in SR20 training aircraft and cracking in SR22 models, although no collapses have occurred on the latter. The bulletin is intended to alert owners and installers but does not mandate regulatory action.

Safety Information Bulletin

Cirrus SR20
Cirrus SR22

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.

Safety Information Bulletin

Embraer EMB-135
Embraer 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.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin

Hawker 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.

Safety Information Bulletin

Cessna U206F
Cessna U206G
Cessna TU206F
Cessna TU206G

EASA SIB 2009-23

LPT Disk 1 failure on CFM56-5-A1 engine

EASA Safety Information Bulletin SIB No. 2009-23 addresses a Low Pressure Turbine (LPT) Disk 1 failure on the CFM56-5-A1 engine. The bulletin reports an incident on 30 June 2009 involving a CFM56-5A engine that experienced a stall during take-off, leading to LPT damage and disk fracture. The document is relevant to operators and maintenance organizations using CFM56-5-A1 engines.

Safety Information Bulletin

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.

Safety Information Bulletin

Cessna 310
Cessna 320
Cessna 335
Cessna 340
Cessna 401
Cessna 402
Cessna 411
Cessna 414
Cessna 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.

Safety Information Bulletin

Cessna 100
Cessna 200
Cessna 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.

Safety Information Bulletin

Hawker Beechcraft 60
Hawker Beechcraft 60A
Hawker 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.

Safety Information Bulletin

Mooney M20B
Mooney M20C
Mooney M20D
Mooney M20E
Mooney M20F
Mooney M20J
Mooney 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.

Safety Information Bulletin

Grumman AA-5A
Grumman AA-5B
Grumman AG-5B
American General AA-5A
American General AA-5B
American General AG-5B
Tiger AA-5A
Tiger AA-5B
Tiger 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.

Safety Information Bulletin

Robinson 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.

Safety Information Bulletin

Cirrus SR20
Cirrus 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.

Safety Information Bulletin

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.

Safety Information Bulletin

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.

Safety Information Bulletin