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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 2011-02

ATR Main Landing Gear (MLG) Shock Absorbers — Cross Locking Bolt of the Attachment Pin

EASA Safety Information Bulletin 2011-02 is an informational document addressing the ATR 42 and ATR 72 aeroplanes' main landing gear (MLG) shock absorbers, specifically the cross locking bolt of the attachment pin. It highlights the risk of migration and rupture of the shock absorber attachment pin due to missing locking bolts, referencing previous maintenance manuals and service bulletins.

Safety Information Bulletin

ATR 42
ATR 72

EASA SIB 2010-26R1

Potential Performance Degradation of Anti-icing Fluids — Reduced Holdover Times

EASA Safety Information Bulletin 2010-26R1 is an informational document addressing potential performance degradation of aircraft anti-icing fluids due to contamination by runway de-icing fluids. It applies to all aeroplanes operating in winter conditions and highlights that mixing thickened anti-icing fluids with small amounts of formate or acetate-based runway de-icing fluids can reduce holdover times. The bulletin does not target specific aircraft or engine models but provides guidance relevant to ground operations involving de-icing and anti-icing procedures.

Safety Information Bulletin

EASA SIB CE-11-21

Hawker Beechcraft 33, 35 and 36 (Bonanza), 55, 56, 58 and 95 (Baron), and 60 (Duke) aeroplanes - Trailing Edge Flap Nose Rib P/N 35-165050-84 Cracking

The Special Airworthiness Information Bulletin SAIB: CE-11-21 is an FAA informational bulletin addressing potential cracking in the trailing edge flap nose rib part number 35-165050-84 on Hawker Beechcraft Bonanza Model Series 33, 35, and 36; Baron Model Series 55, 56, 58, and 95; and Duke Model Series 60 aircraft. This bulletin informs owners, operators, and maintenance personnel about the airworthiness concern but does not mandate any regulatory action. The cracking issue has been observed on both left-hand and right-hand flap nose ribs, with no current determination that it warrants an airworthiness directive.

Safety Information Bulletin

Hawker Beechcraft Bonanza 33
Hawker Beechcraft Bonanza 35
Hawker Beechcraft Bonanza 36
Hawker Beechcraft Baron 55
Hawker Beechcraft Baron 56
Hawker Beechcraft Baron 58
Hawker Beechcraft Baron 95
Hawker Beechcraft Duke 60

EASA SIB SAFO11002

Hawker Beechcraft Model 60 (Duke) - Flap Pre-flight Check

SAFO 11002 is a Safety Alert for Operators issued by the U.S. Federal Aviation Administration concerning the Beechcraft Duke (BE-60) aircraft. It highlights the critical need for proper flap operation checks before takeoff to ensure flight safety. The alert is based on an accident investigation where improper flap actuator maintenance contributed to a fatal crash.

Safety Information Bulletin

Beechcraft Duke 60

EASA SIB CE-11-16

Garmin International - Integrated Flight Deck Systems

The Garmin International - Integrated Flight Deck Systems Special Airworthiness Information Bulletin (SAIB) CE-11-16 addresses an issue with incorrect LNAV/VNAV and LNAV+V full scale deflection on SBAS (WAAS) enabled Garmin Integrated Flight Decks, including G1000, Cirrus Perspective, Embraer Prodigy, G900X, G950, GNS 400W/500W-series, and GNS 480/CNX80 units. This bulletin informs operators of a scaling error affecting certain approaches with long final approach segments, which may cause the aircraft to fly outside allowed lateral limits. The issue does not currently warrant an Airworthiness Directive under 14 CFR part 39.

Safety Information Bulletin

EASA SIB CE-11-09

Avidyne Corporation - Flight Management Computing Software System [Piper PA-46R-350T / Cirrus SR20, SR22]

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-09 informs operators and maintenance personnel about a software issue in the Avidyne Corporation Flight Management Computing Software System installed on Piper PA-46R-350T and Cirrus SR20/SR22 aircraft. The bulletin highlights a faulty transition logic causing incorrect altitude limits to be displayed on the Flight Management System. This issue affects aircraft equipped with the Avidyne Entegra Integrated Flight Display system, part number 700-00083-( ), across any software release.

Safety Information Bulletin

Piper PA-46R-350T
Cirrus SR20
Cirrus SR22

EASA SIB CE-11-14

Piper PA-28, PA-32 and PA-34 - Vertical Stabilizer Forward Attachment Point Corrosion

The Special Airworthiness Information Bulletin CE-11-14 issued by the FAA on January 5, 2011, addresses potential corrosion on the vertical stabilizer forward attachment point of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks on specific parts, including steel fitting 62453-00 and aluminum bulkhead/frame assembly 62444-xx, based on service data from routine maintenance inspections. The bulletin provides inspection guidance from Piper service manuals and reminds operators to focus on corrosion prevention and detection.

Safety Information Bulletin

Piper PA-28
Piper PA-32
Piper PA-34

EASA SIB CE-11-13

Piper PA-34 aeroplanes - Forward Wing Spar Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-13 is an informational bulletin addressing potential corrosion on the forward wing spar of Piper PA-28, PA-32, and PA-34 aircraft. It highlights corrosion risks at the fuselage attach fitting, landing gear attach point, and behind the leading edge fuel tank, and recommends incorporating Piper Service Bulletin 1006 to mitigate these issues. This bulletin does not mandate regulatory action but serves as guidance for owners and operators of the affected Piper models.

Safety Information Bulletin

Piper PA-28
Piper PA-32
Piper PA-34

EASA SIB CE-11-11

Piper PA-28, PA-32, and PA-34 - Aileron Hinge Fitting Corrosion

The FAA Special Airworthiness Information Bulletin CE-11-11 provides information regarding potential corrosion on the aileron hinge fittings of Piper PA-28, PA-32, and PA-34 aircraft. This bulletin is informational only and does not mandate any regulatory action but highlights the importance of inspections as outlined in the aircraft service manuals.

Safety Information Bulletin

Piper PA-28
Piper PA-32
Piper PA-34

EASA SIB CE-11-10

Piper PA-28, PA-32, PA-34, and PA-44 - Corrosion on Flap Hinges, Brackets, and Ribs

The Special Airworthiness Information Bulletin FAA SAIB CE-11-10 is an informational bulletin addressing potential corrosion issues on flap hinges, brackets, and ribs of Piper Aircraft models PA-28, PA-32, PA-34, and PA-44. It highlights corrosion found on specific parts including hinges (part numbers 62324-xx), ribs (62328-xx), and brackets (62323-00 and 65899-00). The bulletin provides guidance to operators to focus on inspections outlined in the aircraft service manuals to mitigate corrosion risks.

Safety Information Bulletin

Piper PA-28
Piper PA-32
Piper PA-34
Piper PA-44

EASA SIB SW-11-15

Robinson R22 and R44 series Helicopters - Carbon Monoxide Detectors

The Special Airworthiness Information Bulletin SAIB: SW-11-15 is an FAA informational bulletin addressing Robinson Helicopter Company Model R22 and R44 series helicopters. It specifically targets R22 helicopters with serial numbers 0001 through 4037 and R44 helicopters with serial numbers 0001 through 1590 that are equipped with cabin heaters. The bulletin recommends the installation of carbon monoxide detectors to enhance safety.

Safety Information Bulletin

Robinson R22
Robinson R44

EASA SIB 2007-01R1

Use of Automotive Gasoline (Mogas) containing Bio-Ethanol

EASA Safety Information Bulletin SIB No. 2007-01R1 provides guidance on the use of automotive gasoline (Mogas) containing bio-ethanol in piston-engine aircraft certificated under CS-VLA, CS-22, CS-23, or CS-27 and approved for Mogas operation. It addresses concerns related to the presence of low-molecular weight alcohols such as methanol and ethanol in Mogas fuels and their potential effects on engine performance and fuel system integrity. The bulletin is relevant for aircraft with spark-ignited piston engines approved by type certificate holders or through Supplemental Type Certificates (STC).

Safety Information Bulletin

EASA SIB CE-10-49R1

Cessna Citation Series — Galley Heated Drain Mast

The Special Airworthiness Information Bulletin SAIB CE-10-49 R1 is an FAA informational bulletin addressing an airworthiness concern with heated drain masts (P/N 105881) installed on various Cessna Citation models including the 510 Mustang, 525 series (CJ, CJ1, CJ2, CJ3, CJ4), 550 series, 560 series, 650 series, and 750 X. The bulletin informs owners, operators, and maintenance personnel about overheating and fire risks associated with these galley heated drain masts. It provides guidance to prevent such issues but does not mandate regulatory action.

Safety Information Bulletin

Cessna Citation 510 Mustang
Cessna Citation 525 CJ
Cessna Citation 525 CJ1
Cessna Citation 525 CJ2
Cessna Citation 525 CJ3
Cessna Citation 525 CJ4
Cessna Citation 550 series
Cessna Citation 560 series
Cessna Citation 650 series
Cessna Citation 750 X

EASA SIB CE-11-08

Cessna 206/207 aeroplanes - Sierra Industries STC SA3634SW and SA3853SW

The Special Airworthiness Information Bulletin SAIB: CE-11-08 is an FAA informational bulletin addressing fuel storage concerns on Cessna Models 206 and 207 aircraft equipped with Sierra Industries STC SA3634SW or SA3853SW auxiliary fuel tank bladders. It highlights a potential issue where operators may misjudge actual fuel quantity due to insufficient settling time of fuel in the auxiliary bladders after refueling. The bulletin does not mandate regulatory action but provides safety recommendations.

Safety Information Bulletin

Cessna 206
Cessna 207

EASA SIB CE-11-06

Small Aeroplanes - Main Landing Gear (Tundra) Tires and Wheels

The FAA Special Airworthiness Information Bulletin SAIB: CE-11-06 provides guidance on the use of oversized main landing gear tires, commonly known as tundra tires, on small airplanes including the Allied Ag Cat Productions, Inc. Model G-164B. It highlights safety concerns related to modifications involving larger tires such as the 29x11-10 size on the original Cleveland Wheel and Brake wheel part number 40-101. The bulletin emphasizes the need for FAA-approved data and inspections when installing these tires to ensure continued airworthiness.

Safety Information Bulletin

Allied Ag Cat Productions, Inc. G-164B

EASA SIB 2010-34

CANCELLED - REPLACED BY EASA AD 2011-0076

EASA Safety Information Bulletin 2010-34 is an informational bulletin concerning CEAPR (Robin) DR400 series aircraft manufactured between 1980 and 1988 equipped with engine air filter part number 56-23-02-000. It addresses an accident involving a DR400/160 where the engine air filter was incorrectly installed, leading to engine performance issues. The bulletin highlights the risk of improper air filter installation causing significant engine RPM loss.

Safety Information Bulletin

CEAPR DR400

EASA SIB 2010-36

Embraer EMB-505 aeroplanes - Terrain Awareness Warning System (TAWS)

EASA Safety Information Bulletin SIB No. 2010-36 is an advisory document concerning Embraer EMB-505 aeroplanes. It addresses an airworthiness concern related to the Terrain Awareness Warning System (TAWS) information in the original airplane flight manual, which does not fully meet certification requirements. The bulletin aligns with a similar FAA advisory and aims to inform European operators and owners of the recommended updates.

Safety Information Bulletin

Embraer EMB-505

EASA SIB 2010-35

M7 Aerospace (Fairchild/Swearingen) SA226 and SA227 aeroplanes — Wing Skin Cracking

EASA Safety Information Bulletin 2010-35 addresses wing skin cracking issues on M7 Aerospace (formerly Fairchild/Swwearingen) SA226 and SA227 aeroplanes. The bulletin informs operators about detected cracks in the upper leading edge skin and doubler at Wing Station 81. It aims to raise awareness among European operators regarding this structural concern.

Safety Information Bulletin

M7 Aerospace SA226
M7 Aerospace SA227

EASA SIB CE-11-05

Taylorcraft - Main Landing Gear Tie Strut P/N B-A51

The Special Airworthiness Information Bulletin SAIB: CE-11-05 is an FAA informational bulletin addressing corrosion concerns in the main landing gear tie strut part number B-A51 installed on Taylorcraft airplanes, including models under type certificate data sheets 1A9, 1A11, TG-6, A-643, A-696, A-699, A-700, A-746, and TG-6. It provides guidance to owners and operators on inspecting and mitigating corrosion risks to prevent tie strut failure. This bulletin is not a mandatory directive but offers important safety recommendations.

Safety Information Bulletin

Taylorcraft 1A9
Taylorcraft 1A11
Taylorcraft TG-6
Taylorcraft A-643
Taylorcraft A-696
Taylorcraft A-699
Taylorcraft A-700
Taylorcraft A-746

EASA SIB SAFO10007

Tundra Tire Installation/Approval for Aeroplanes Equipped with Leaf Spring Type Main Landing Gear

The Safety Alert for Operators (SAFO) 10007 titled 'Tundra Tire Installation/Approval for Aeroplanes Equipped with Leaf Spring Type Main Landing Gear' provides safety information regarding the use of oversize tundra tires, skis, and wheel/ski configurations on aircraft with leaf spring type main landing gear. It highlights the increased risk of structural failures, particularly near the axle attachment holes, with at least 32 documented accidents primarily involving aircraft such as the Piper PA-18. The document offers guidance on inspection and maintenance practices to mitigate these risks.

Safety Information Bulletin

Piper PA-18