Browse 4995 EASA regulations with AI-powered summaries.
EASA AD 2019-FATA-01020A-05
SUPERSEDED BY FATA AD 2021-FATA-01020A-07 is an aviation regulatory document indicating that the current directive has been replaced by FATA AD 2021-FATA-01020A-07. The document does not provide details on specific affected aircraft, engines, or parts.
EASA AD 2019-0298-E
EASA Airworthiness Directive 2019-0298-E is an emergency directive addressing the inspection of outer wing shear bolts on Stemme AG ASP S15-1 aeroplanes, specifically serial numbers ASP-031 and ASP-034 through ASP-043. The directive mandates inspection and corrective actions for outer wing shear bolts with Part Number 365058 to prevent potential wing separation. This directive applies to affected parts installed on both outer wings of the specified aircraft.
EASA AD 2019-0295
EASA Airworthiness Directive 2019-0295 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus Helicopters AS 332 C, C1, L, and L1 models. It addresses corrosion found on the main gearbox suspension bar attachment fittings and screws, which could lead to structural failure and detachment of the suspension bars. The directive mandates inspections and corrective actions to ensure continued airworthiness.
EASA SIB 2019-18
EASA Safety Information Bulletin 2019-18 is an informational document addressing fan blade life limitations for CFM International CFM56-7B engines, which are installed on Boeing 737-600, 737-700, 737-800, and 737-900 aircraft. The bulletin discusses reported fan blade failures due to fatigue fractures and references related service bulletins and EASA Airworthiness Directive 2019-0018. It provides recommendations to enhance safety by implementing fan blade life limits but does not impose mandatory requirements.
EASA AD 2019-0293
EASA Airworthiness Directive 2019-0293 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Pilatus Aircraft Ltd PC-24 aeroplanes. It addresses the replacement of vinyl grommets used in the emergency exits, which may become rigid after exposure to low temperatures. The directive applies to all PC-24 aircraft serial numbers and mandates replacing affected grommets to ensure emergency exits function properly during evacuation.
EASA AD 2019-0292
EASA Airworthiness Directive 2019-0292 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting CEAPR DR 400 aeroplanes, including multiple DR 400 variants up to serial number 2723. The directive mandates inspection of the stabilator attachment to detect potential deformation and incorrect positioning of internal wedges in the false spar. This inspection aims to prevent possible detachment of the stabilator, which could lead to loss of control of the aircraft.
EASA AD 2019-0294
EASA Airworthiness Directive 2019-0294 is an official regulatory document addressing the inspection and removal of the vertical fin vibration absorber on Leonardo S.p.A. A109S and AW109SP helicopters. It mandates inspections and corrective actions to address cracks and damage found on the vertical fin vibration absorber and surrounding structure. This directive applies to all serial numbers of the affected helicopter models and aims to ensure continued airworthiness and structural integrity.
EASA AD CF-2018-01R2
The Airworthiness Directive CF-2018-01R2 addresses wear issues in the nose landing gear (NLG) drag strut lock link on De Havilland Aircraft of Canada Limited DHC-8-400, -401, and -402 models, serial numbers 4001 through 4585 and 4587. It mandates inspections and corrective actions to prevent NLG collapse caused by worn or loose bushings in the locking mechanism. This directive updates previous versions to clarify supersession and compliance requirements.
EASA SIB 2019-17
EASA Safety Information Bulletin No. 2019-17 is an airworthiness bulletin addressing possible improper maintenance by Xtra Aerospace, LLC. It informs the European aviation community about the FAA's revocation of Xtra Aerospace's Part 145 certificate due to systemic approval of maintenance articles not listed on their operations specifications. This bulletin applies broadly to aircraft owners, operators, manufacturers, maintenance organizations, parts suppliers, and distributors, but does not target specific aircraft or engine models.
EASA AD 2019-0290
EASA Airworthiness Directive 2019-0290 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting ATR 72 aeroplanes, excluding certain serial numbers and those with ATR modification 07988 embodied in production. The directive addresses an unsafe condition related to electrical wiring routing under panel 295CL on the left-hand side wing rear spar. It mandates a modification to the electrical harness clamp installation to prevent wire chafing and potential fire hazards.
EASA AD 2018-0095R1
EASA Airworthiness Directive 2018-0095R1 is an updated safety directive addressing inspection and operational limitations for the intermediate pressure compressor (IPC) rotor buffer seal on Rolls-Royce Trent 1000 series engines, which power Boeing 787-8 and 787-9 aircraft. The directive mandates repetitive borescope inspections and sets operational restrictions to prevent engine power loss caused by seal cracking. It also introduces an optional modification that can terminate the inspection requirements.
EASA AD 2018-0094R1
EASA Airworthiness Directive 2018-0094R1 is a regulatory update addressing inspection and de-pairing limitations for the intermediate pressure compressor rotor seal on Rolls-Royce Trent 1000 engines installed on Boeing 787-8 and 787-9 aircraft. The directive mandates repetitive borescope inspections and corrective actions for affected seals to prevent engine power loss. It also introduces optional terminating actions through specific Rolls-Royce service bulletins.
EASA AD 2019-0289
EASA Airworthiness Directive 2019-0289 is an airworthiness directive issued for Airbus Helicopters EC 175 B models. It addresses a manufacturing defect in air no fuel valves with Part Number 510396-2, which may cause fuel leakage and increase the risk of post-impact fire following a hard landing.
EASA AD 2019-0288
EASA Airworthiness Directive 2019-0288 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A350-941 and A350-1041 aeroplanes. It mandates compliance with the Airbus A350 Airworthiness Limitations Section Part 3 Revision 05 and variation 5.3, which include certification maintenance requirements essential for continued airworthiness.
EASA AD 2019-0287
EASA Airworthiness Directive 2019-0287 is an airworthiness directive addressing Airbus Helicopters EC 225 LP models equipped with emergency life rafts installed in the multi-purpose sponsons. It focuses on inspection, cleaning, lubrication, and replacement of the external life raft jettison system's inflation cylinder percussion system bellcranks to prevent jamming issues. The directive applies to specific bellcrank part numbers and mandates corrective actions to ensure safe release of life rafts during emergencies.
EASA AD US-2019-23-10
Airworthiness Directive 2019-23-10 is a final rule issued by the FAA addressing Textron Aviation Inc. airplanes, specifically models E33, E33A, E33C, F33, G33, 35-C33, 35-C33A, S35, V35, V35A, 36, and certain serial numbers of F33A, F33C, V35B, and A36. The directive mandates inspection and replacement of the right aileron flight control cable end fittings to prevent failure and potential loss of roll control.
EASA AD US-2019-21-51
[Final Rule] Engine - High-Pressure Turbine Interstage Seal - Removal from Service is a Federal Aviation Administration (FAA) airworthiness directive addressing certain General Electric Company GE90-115B model turbofan engines. It mandates the removal from service of the Interstage Seal, part number 2505M72P01, installed on specific engine serial numbers due to a recent uncontained high-pressure turbine failure event. This directive aims to prevent potential engine and aircraft damage caused by high-energy debris release.
EASA AD 2019-0285
EASA Airworthiness Directive 2019-0285 is an airworthiness directive issued for Airbus Helicopters EC 175 B models. It mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the Airbus Helicopters EC 175 B Airworthiness Limitations Section Revision 014. The directive addresses recalculation of service life limits and replacement of certain parts to ensure continued airworthiness.
EASA AD 2019-0283
EASA Airworthiness Directive 2019-0283 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates inspections of the wing trailing edge and trailing edge devices to detect cracks and provides optional modification instructions to prevent potential in-flight loss of parts. The directive applies to specific manufacturer serial numbers as identified in the applicable Airbus Service Bulletins.
EASA AD 2019-0281
The document titled 'Fuselage — ADF Antenna / Fuel Tank Protection' pertains to the AIRBUS HELICOPTERS EC175 model. It addresses specific considerations related to the aircraft's fuselage, focusing on the Automatic Direction Finder (ADF) antenna and measures to protect the fuel tank. The directive aims to ensure continued airworthiness and safety of the affected helicopter model.