EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

EASA SIB 2010-25

Aug 27, 2010

Cabin Oxygen Mask Service Recommendations from Original Equipment Manufacturers, and Cabin Oxygen Masks with B/E Aerospace In-line Flow Indicators Part Number (P/N) 118023-02

EASA Safety Information Bulletin SIB No. 2010-25 provides service recommendations regarding cabin oxygen masks equipped with B/E Aerospace in-line flow indicators part number 118023-02. The bulletin applies to CS1-23 and CS-25 category aeroplanes, including Airbus A318, A319, A320, A321, Boeing 737, 747, 757, 767, 777, and Fokker F28 models. It addresses failures of the in-line flow indicators that can cause oxygen flow interruption during use.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Fokker F28

EASA SIB CE-10-38R1

Aug 23, 2010

Honeywell Avionics - GPS Non-Precision Approach (NPA) caused by GPS Receiver Software Defect

The Special Airworthiness Information Bulletin SAIB CE-10-38R1 issued by the FAA provides information about a GPS Non-Precision Approach (NPA) issue caused by a software defect in Honeywell GPS receivers. This concern affects multiple Honeywell avionics products including Flight Management Systems, GPS Navigators, TAWS, GNSS units, and the VIDL-G receiver, notably installed on aircraft such as the Dassault F7X. The bulletin highlights a temporary loss of GPS navigation during extended flights when no backup navigation system is available.

Safety Information Bulletin
  • Dassault F7X

EASA SIB SW-10-42R1

Aug 17, 2010

Apical Industries, Inc. Emergency Float Kits (STC-installed) for Bell 206 and 407 series Helicopters

Special Airworthiness Information Bulletin SAIB: SW-10-42R1 is a revised FAA information bulletin addressing uneven deployment issues with Apical Industries, Inc. Emergency Float Kits installed on Bell 206 and Bell 407 series helicopters. The affected kits include specific part and serial numbers under STC SR01535LA. This bulletin informs operators about a deployment problem caused by incorrect installation of float inflation hoses.

Safety Information Bulletin
  • Bell 206
  • Bell 407

EASA SIB 2010-24

Aug 13, 2010

Airbus A340 Exhaust — Thrust Reverser (TR) Actuation System Doors — Recommended installation of warning placards

EASA Safety Information Bulletin 2010-24 is an informational bulletin addressing the Airbus A340 exhaust thrust reverser (TR) actuation system doors. It applies to Airbus A340 models -211, -212, -213, -311, -312, and -313 across all manufacturer serial numbers. The bulletin recommends installing warning placards on certain thrust reverser cowls to support previous modifications mandated by EASA Airworthiness Directive 2010-0044.

Safety Information Bulletin
  • Airbus A340

EASA SIB CE-10-44

Aug 10, 2010

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.

Safety Information Bulletin
  • Cessna 402C

EASA SIB SW-10-41

Aug 9, 2010

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.

Safety Information Bulletin
All aircraft

EASA SIB CE-10-39

Aug 4, 2010

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.

Safety Information Bulletin
  • American Champion 7ECA
  • American Champion 7GCAA
  • American Champion 7GCBC
  • American Champion 7KCAB
  • American Champion 8KCAB
  • American Champion 8GCBC

EASA SIB CE-10-40R1

Aug 2, 2010

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.

Safety Information Bulletin
  • Cessna 100 Series
  • Cessna 200 Series
  • Cessna 300 Series

EASA SIB NE-10-37

Aug 2, 2010

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.

Safety Information Bulletin
  • Boeing 747
  • Boeing 767
  • Airbus A300
  • McDonnell Douglas MD-11

EASA SIB 2010-22

Jul 30, 2010

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.

Safety Information Bulletin
  • Airbus Helicopters EC155 B1
  • Airbus Helicopters EC225 LP
  • Airbus Helicopters AS332 L1
  • Airbus Helicopters AS332 L2
  • Airbus Helicopters AS365 N2
  • Airbus Helicopters AS365 N3
  • Airbus Helicopters EC135
  • AgustaWestland A109
  • AgustaWestland AB139
  • AgustaWestland AW139
  • Sikorsky S-61N
  • Sikorsky S-76
  • Sikorsky S-92A

EASA SIB SAFO10013

Jul 9, 2010

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.

Safety Information Bulletin

EASA SIB 2010-18

Jun 30, 2010

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.

Safety Information Bulletin
All aircraft

EASA SIB 2010-20

Jun 18, 2010

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.

Safety Information Bulletin
  • Eurocopter SA 3180
  • Eurocopter SA 318B
  • Eurocopter SA 318C
  • Eurocopter SE 3160
  • Eurocopter SA 316B
  • Eurocopter SA 316C
  • Eurocopter SA 319B
  • Eurocopter SA 315B

EASA SIB 2010-19

Jun 2, 2010

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.

Safety Information Bulletin
All aircraft

EASA SIB CE-10-29R1

May 31, 2010

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.

Safety Information Bulletin
  • Cessna 560XL
  • Cessna 650
  • Cessna 750

EASA SIB CE-10-17

May 28, 2010

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.

Safety Information Bulletin
  • Piper PA-28
  • Piper PA-32

EASA SIB CE-10-30

May 28, 2010

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.

Safety Information Bulletin
  • Piper PA-28R(T)
  • Piper PA-44-180(T)

EASA SIB CE-10-20R1

May 21, 2010

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.

Safety Information Bulletin
  • Cessna 336
  • Cessna 337
  • Reims F337

EASA SIB NE-10-32

May 18, 2010

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.

Safety Information Bulletin

EASA SIB AV-2010-04

May 11, 2010

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.

Safety Information Bulletin
  • Bombardier Regional Jet Series
  • Bombardier Challenger 600