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EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

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EASA SIB CE-10-44

Cessna 402C Hydraulic Power Indicating - Temporary Revisions (TRs) to Pilot—s Operating Handbook (POH)

The Special Airworthiness Information Bulletin SAIB: CE-10-44 is a non-mandatory FAA information bulletin addressing hydraulic power indication issues on Cessna Model 402C airplanes. It highlights the meaning of the "HYD PRESS" light and the potential consequences if the hydraulic pressure indication is not properly addressed during flight operations.

Aug 10, 2010
Safety Information BulletinFlight OpsSafety MgmtCessna 402C

EASA SIB SW-10-41

Honeywell MK XXII Enhanced Ground Proximity Warning System (EGPWS) Software Problem

The Special Airworthiness Information Bulletin SAIB: SW-10-41 addresses a software problem in the Honeywell MK XXII Enhanced Ground Proximity Warning System (EGPWS) installed in helicopters. This issue involves a potential unannunciated failure of the Terrain Awareness Warning System (TAWS) aural alerting function when the radio altimeter is in a no computed data (NCD) or invalid state at takeoff. The bulletin informs operators that while the terrain display remains accurate, the aural alerts may not function properly until valid radio altimeter data is received.

Aug 9, 2010
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-10-39

American Champion (formerly Bellanca) - Possible Interference between the Front Seat Lap Belt and the Rear Rudder Pedals

The Special Airworthiness Information Bulletin SAIB: CE-10-39 is an FAA informational bulletin addressing a potential interference issue between the front seat lap belt and the rear rudder pedals on American Champion Aircraft Corporation models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC. The bulletin highlights a concern discovered after an incident involving an 8KCAB Decathlon where the rear rudder pedal caught on the front seat aerobatic harness. This bulletin provides guidance but does not mandate regulatory action.

Aug 4, 2010
Safety Information BulletinSafety MgmtAmerican Champion 7ECAAmerican Champion 7GCAAAmerican Champion 7GCBCAmerican Champion 7KCABAmerican Champion 8KCABAmerican Champion 8GCBC

EASA SIB CE-10-40R1

Cessna (incl. Reims Aviation) - Water Contamination of Fuel Tank Systems

The Special Airworthiness Information Bulletin SAIB CE-10-40R1 addresses water contamination issues in the fuel tank systems of Cessna single-engine airplanes, including models from the 100, 200, and 300 series manufactured by Cessna Aircraft Company and formerly Reims Aviation S.A. This bulletin informs pilots, owners, operators, and maintenance personnel about the hazards of water in fuel systems and provides guidance on inspection and prevention. It is an informational document and does not mandate regulatory action.

Aug 2, 2010
Safety Information BulletinMaintenanceSafety MgmtCessna 100 SeriesCessna 200 SeriesCessna 300 Series

EASA SIB NE-10-37

General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults

The General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults Special Airworthiness Information Bulletin (SAIB NE-10-37) informs operators of airplanes equipped with GE CF6-80C2 series turbofan engines about potential engine in-flight shutdowns caused by fuel metering valve feedback faults. This bulletin applies to engines on Boeing 747, 767, Airbus A300, and McDonnell Douglas MD-11 aircraft, except Boeing 747 and 767 airplanes with FADEC software version 8.2.R or later. The bulletin provides guidance to prevent dual-channel faults that can lead to uncommanded engine shutdowns.

Aug 2, 2010
Safety Information BulletinMaintenanceSafety MgmtBoeing 747Boeing 767Airbus A300McDonnell Douglas MD-11

EASA SIB 2010-22

Crash Position Indicator CPI 503 series Emergency Locator Transmitter (ELT) - Limited Deployment Altitude

EASA Safety Information Bulletin SIB No. 2010-22 addresses the limited deployment altitude of the Crash Position Indicator CPI 503 series Emergency Locator Transmitters (ELTs) installed on various helicopter models including Eurocopter EC 155 B1, EC 225 LP, AS 332 L1/L2, AS 365 N2/N3, Eurocopter Deutschland EC 135 series, Agusta Westland A109 series, AB139, AW139, and Sikorsky S-61N, S-76 series, and S-92A helicopters. The bulletin highlights that these ELTs meet UK CAA specifications but do not fully comply with the JTSO/ETSO-2C126 EUROCAE ED-62 impact test criteria when deployed from high altitudes. A new model, P/N 503-16HT, has been developed to address this limitation.

Jul 30, 2010
Safety Information BulletinSafety MgmtAirbus Helicopters EC155 B1Airbus Helicopters EC225 LPAirbus Helicopters AS332 L1Airbus Helicopters AS332 L2Airbus Helicopters AS365 N2Airbus Helicopters AS365 N3Airbus Helicopters EC135AgustaWestland A109AgustaWestland AB139AgustaWestland AW139Sikorsky S-61NSikorsky S-76Sikorsky S-92A

EASA SIB SAFO10013

Possible Misidentification of TCM Ignition Systems (formerly Bendix) D-2000/D-2200 Dual Magnetos

The Safety Alert for Operators (SAFO) titled "Possible Misidentification of TCM Ignition Systems (formerly Bendix) D-2000/D-2200 Dual Magnetos" addresses the issue of certain TCM/Bendix D-2000 and D-2200 dual magnetos being misidentified as D-3000 magnetos. This misidentification involves the magneto housing and data plates, which may affect compliance with applicable airworthiness directives (ADs). The document is relevant to operators and maintenance personnel working with aircraft engines equipped with these specific magnetos.

Jul 9, 2010
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB 2010-18

Go-Around Callout and Immediate Response

EASA Safety Information Bulletin SIB No: 2010-18 is an advisory document addressing go-around callout and immediate response procedures for all aeroplanes and helicopters with a two-pilot flight crew. It supports the FAA Safety Alert for Operators SAFO 10005, emphasizing that either pilot may initiate a go-around callout and that the pilot flying must immediately execute a missed approach. The bulletin aims to enhance flight safety during approach and landing phases by promoting clear and immediate go-around actions.

Jun 30, 2010
Safety Information BulletinFlight OpsSafety Mgmt

EASA SIB 2010-20

EUROCOPTER helicopters - Main Gear Box - Monitoring of lubricating oils

EASA Safety Information Bulletin 2010-20 is a safety information bulletin addressing the monitoring of lubricating oils in the Main Gear Box (MGB) of Eurocopter helicopters, specifically models SA 3180, SA 318B, SA 318C, SE 3160, SA 316B, SA 316C, SA 319B, and SA 315B. The bulletin endorses Eurocopter's recommendations for daily visual and sensory checks of MGB oil and periodic testing for water content to detect early signs of wear or damage. It references Eurocopter Safety Information Notice 2173-S-05 and Service Bulletins 05.101 and 05.43 for detailed procedures.

Jun 18, 2010
Safety Information BulletinMaintenanceSafety MgmtEurocopter SA 3180Eurocopter SA 318BEurocopter SA 318CEurocopter SE 3160Eurocopter SA 316BEurocopter SA 316CEurocopter SA 319BEurocopter SA 315B

EASA SIB 2010-19

Exhaust Mufflers Inspection for piston engine Helicopters and Aeroplanes

EASA Safety Information Bulletin 2010-19 is an informational document addressing the inspection of exhaust mufflers on piston engine helicopters and aeroplanes. It highlights safety concerns related to exhaust system component failures, including mufflers and heat exchangers, which can cause carbon monoxide poisoning, engine power loss, or fire. The bulletin applies broadly to piston engine powered helicopters and aeroplanes and references related FAA SAIBs for further information.

Jun 2, 2010
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB CE-10-29R1

Cessna Aircraft Company 560XL, 650 and 750 - Aft Side Ledger Divider Light

The Special Airworthiness Information Bulletin SAIB CE-10-29R1 is an FAA informational bulletin addressing an airworthiness concern related to the aft left and right side ledge divider lights on Cessna Model 560XL, 650, and 750 airplanes. It informs owners, operators, and maintenance personnel about the potential hazard caused by the installation of higher wattage bulbs than recommended in these aircraft models.

May 31, 2010
Safety Information BulletinMaintenanceSafety MgmtCessna 560XLCessna 650Cessna 750

EASA SIB CE-10-17

Piper PA-28 and PA-32 Main Landing Gear Torque Link Inspection Interval

The Special Airworthiness Information Bulletin (SAIB) CE-10-17 is an FAA informational bulletin addressing the inspection interval for the main landing gear torque link on Piper PA-28 and PA-32 aircraft models. It specifically concerns certain serial numbers of PA-28-140, PA-28-150/-160/-180, PA-28-235, PA-32-260, and PA-32-300 aircraft. The bulletin recommends incorporating Piper Service Bulletin 1199 to enhance inspection frequency and replacement times for the main landing gear torque link assemblies.

May 28, 2010
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28Piper PA-32

EASA SIB CE-10-30

Piper PA-28R(T) and PA-44-180(T) - Nose Landing Gear Drag Link Bolt

The FAA Special Airworthiness Information Bulletin SAIB: CE-10-30 addresses a potential airworthiness concern involving the nose landing gear drag link bolt on Piper PA-28R(T) and PA-44-180(T) aircraft models. The bulletin highlights the risk of nose gear collapse due to fatigue cracking of the drag link bolt, which has been observed in several Piper aircraft models. This information bulletin provides guidance to owners and operators to mitigate this issue but does not mandate regulatory action.

May 28, 2010
Safety Information BulletinMaintenanceSafety MgmtPiper PA-28R(T)Piper PA-44-180(T)

EASA SIB CE-10-20R1

Cessna Aircraft Company 336, 337 and (Reims) F337 aeroplanes - Wingtip Extensions

The Cessna Aircraft Company 336, 337 and (Reims) F337 aeroplanes - Wingtip Extensions Special Airworthiness Information Bulletin (SAIB: CE-10-20 R1) is an FAA advisory bulletin addressing safety concerns related to wingtip extensions on Cessna Models 336, 337, and F337 (Reims) series airplanes. It highlights potential structural issues such as wrinkled skins, cracks, and loose wing tips following modifications with Supplemental Type Certificates (STCs) for extended wingtips and winglets. The bulletin provides guidance to enhance safety but does not mandate regulatory action.

May 21, 2010
Safety Information BulletinMaintenanceSafety MgmtCessna 336Cessna 337Reims F337

EASA SIB NE-10-32

Pratt & Whitney JT8D Series Turbine Engine Accessory Drive

The Special Airworthiness Information Bulletin SAIB: NE-10-32 is an FAA informational bulletin addressing potential accessory gearbox bevel gear fractures in all Pratt & Whitney JT8D series turbine engines. It highlights issues caused by forward movement of the constant speed drive (CSD) bearing bushing that can lead to gear misalignment and fractures. The bulletin is intended for owners, operators, and certificated repair facilities operating JT8D engines.

May 18, 2010
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB AV-2010-04

Bombardier (formerly Canadair) - Core Cowl Stay Support Strut/Rod

Transport Canada Service Difficulty Advisory AV-2010-04 addresses a potential issue with the engine core cowl stay support strut/rod on Bombardier Regional Jet Series (CL-600-2B19) and Challenger 600 (CL-600-2A12/2B16) aircraft equipped with CF34-1 and CF34-3 engines. The advisory highlights the risk of in-flight engine shutdowns caused by incorrect stowage of the upper core cowl door stay support strut/rod, which can interfere with the throttle control mechanism.

May 11, 2010
Safety Information BulletinMaintenanceSafety MgmtBombardier Regional Jet SeriesBombardier Challenger 600

EASA SIB NE-10-27

Lycoming Engines - Superior Air Parts (SAP) Oil Filter Adapter P/N SL2157.

The FAA Special Airworthiness Information Bulletin SAIB: NE-10-27 provides information regarding the use of Superior Air Parts (SAP) oil filter adapter part number SL2157 installed on certain Lycoming Engines reciprocating engines. It alerts operators and maintenance personnel about potential issues when incorrect oil filters without internal oil pressure by-pass valves are installed on this adapter. The bulletin clarifies that only specific Champion and Tempest oil filters with internal by-pass valves are eligible for use with the SAP oil filter adapter SL2157.

Apr 23, 2010
Safety Information BulletinMaintenanceSafety Mgmt

EASA SIB AV-2010-02

Bombardier Inc. - Aft Nose Landing Gear Door Upper Attachment Hinge Assemblies

Transport Canada Civil Aviation Service Difficulty Advisory AV-2010-02 addresses a potential issue with the aft nose landing gear door upper attachment hinge assemblies on Bombardier Inc. CL-600-2C10, CL-600-2D15, and CL-600-2D24 aircraft. The advisory highlights incidents where a self-locking nut backing out caused hinge pin disengagement, leading to door binding and damage during landing gear extension. Bombardier has issued temporary maintenance manual revisions to mitigate this issue.

Apr 22, 2010
Safety Information BulletinMaintenanceSafety MgmtBombardier CL-600-2C10Bombardier CL-600-2D15Bombardier CL-600-2D24

EASA SIB 2010-16

Baby Bassinet Detachment

EASA Safety Information Bulletin 2010-16 addresses the detachment incident of the Innovint 7250 series baby bassinet from cabin partition walls on Airbus A318/A319/A320/A321 aircraft. The bulletin provides safety information following a reported event where the bassinet detached and caused minor injuries to a baby occupant. It includes updated installation instructions and maintenance requirements to ensure secure attachment during flight.

Apr 19, 2010
Safety Information BulletinMaintenanceSafety MgmtAirbus A318Airbus A319Airbus A320Airbus A321

EASA SIB CE-10-22

Honeywell GNS Series Navigation Systems

The FAA Special Airworthiness Information Bulletin SAIB: CE-10-22 addresses a software anomaly in Honeywell GNS Series Navigation Systems, specifically the GNS_XLS PRNAV (P/N 17960-0103-XXX), GNS_XLS Enhanced PRNAV (P/N 17960-0204-XXX), and GNS_XL PRNAV (P/N 18355-0102-0XXX). This anomaly affects RNAV procedures containing Radius-to-a-Fix (RF) legs, potentially causing the system to fail to capture and fly the curved RF path. The bulletin clarifies that this issue does not currently warrant an airworthiness directive under 14 CFR part 39.

Apr 19, 2010
Safety Information BulletinFlight OpsSafety Mgmt