Browse 4771 EASA regulations with AI-powered summaries.
EASA AD 2019-0075
EASA Airworthiness Directive SUPERSEDED BY EASA AD 2019-0249 concerns Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engines. This directive has been superseded and is no longer the current regulatory requirement. It originally addressed airworthiness issues related to the Trent 1000 engine model.
EASA AD 2019-0071
EASA Airworthiness Directive 2019-0071 is an airworthiness directive addressing Rolls-Royce Trent XWB-75, XWB-79, XWB-79B, and XWB-84 engines, commonly installed on Airbus A350 aircraft. The directive mandates the replacement of certain low pressure turbine rear support seal panel assemblies identified by specific serial numbers due to manufacturing defects. This action aims to maintain engine integrity and aircraft safety.
EASA AD RU-2017-322-05
EASA Decision not to adopt FATA AD 2017-322-05 is a regulatory decision concerning Sukhoi Civil Aircraft JSC RRJ-95 aeroplanes. The decision addresses the requirement for repetitive inspections of fuselage Frame 58 to detect cracks and the associated corrective actions. EASA concluded that the risk of undetected cracking is extremely low due to existing inspections and repair instructions provided by Sukhoi Civil Aircraft JSC.
EASA AD 2018-0212R1
EASA Airworthiness Directive 2018-0212R1 is a regulatory document addressing the life limitation and replacement requirements for the forward engine mount titanium crossbeam, part number 238-0204-501, installed on Airbus A319-113, A319-114, A320-211, and A320-212 aeroplanes equipped with CFM56-5A engines. The directive mandates tracking the accumulated flight cycles of these crossbeams and replacing them before exceeding a life limit of 64,000 flight cycles to prevent potential failure and engine detachment in flight.
EASA AD 2019-0070
EASA Airworthiness Directive 2019-0070 is an official regulatory document addressing inspection and modification requirements for the vertical stabilizer attachment fittings on DAHER AEROSPACE TBM 700 aeroplanes, specifically serial numbers 001 through 308 inclusive and 310. The directive mandates inspections for cracks caused by corrosion and provides instructions for optional modification using improved corrosion-resistant fittings. It applies to specific part numbers of vertical stabilizer attachment fittings and aims to maintain the structural integrity of the vertical stabilizer.
EASA AD 2019-0072
EASA Airworthiness Directive 2019-0072 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the Airbus A380 Airworthiness Limitations Section Part 2 Revision 07, which includes damage tolerant airworthiness limitation items. This directive ensures the continued airworthiness of these aircraft by requiring updated maintenance tasks and intervals.
EASA AD US-2019-06-06
FAA Airworthiness Directive 2019-06-06 is a final rule addressing all International Aero Engines AG V2500 turbofan engine models. It mandates initial and repetitive borescope inspections of the diffuser case M-flange and requires replacement of the diffuser case if cracks are detected. This directive aims to prevent uncontained diffuser case rupture that could damage the engine and aircraft.
EASA AD 2019-0073
EASA Airworthiness Directive 2019-0073 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. AB139 and AW139 helicopters equipped with the Full Ice Protection System (FIPS). It addresses inspection and replacement requirements for specific tail rotor blades with part numbers 4G6410A00131, 4G6410A00132, and 4G6410A00133. The directive aims to ensure the continued airworthiness of these helicopters by mitigating risks related to tail rotor blade damage.
EASA AD 2019-0065
EASA Airworthiness Directive 2019-0065 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It mandates the replacement of rear fuselage cone diagonal struts with new serviceable parts to ensure structural integrity. This directive applies to all serial numbers except those with Airbus modification 108588 incorporated during production.
EASA AD 2019-0066
EASA Airworthiness Directive 2019-0066 is an airworthiness directive addressing the nose landing gear leg assembly inspection for Diamond Aircraft Industries GmbH DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG aeroplanes. It mandates repetitive inspections of the nose landing gear actuator attachment lever to detect cracks that could lead to restricted rudder control. The directive applies to all serial numbers, including those converted via specific service bulletins.
EASA AD 2019-0068
EASA Airworthiness Directive 2019-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus A320-251N and A321-253N aeroplanes. It addresses cracks found in pylon block seals, specifically part numbers D0003167600000 and D0003167600100, which could compromise firewall integrity between the pylon and nacelle. The directive mandates inspection and replacement of these seals to ensure continued airworthiness.
EASA AD 2019-0063
EASA Airworthiness Directive SUPERSEDED BY EASA AD 2019-0164 pertains to Airbus S.A.S. aircraft models A330 and A340. This directive has been officially replaced by EASA AD 2019-0164 and no longer applies as the active regulatory requirement. It originally addressed airworthiness concerns specific to these Airbus wide-body aircraft types.
EASA AD 2019-0062
EASA Airworthiness Directive 2019-0062 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of PZL SW-4 helicopters. It mandates compliance with updated airworthiness limitations as specified in the PZL SW-4 Instructions for Continued Airworthiness - Maintenance Manual, Revision 14 dated November 2018. This directive ensures the continued airworthiness of these helicopters by enforcing maintenance tasks and life limits.
EASA AD US-2019-05-07
The Federal Register document titled "Engine - Compressor Fan Disks - Removal / Replacement" is a final rule Airworthiness Directive (AD 2019-05-07) issued by the FAA affecting certain Honeywell International Inc. TFE731 turbofan engines, specifically models TFE731-20R, -20AR, -20BR, -40AR, -40BR, and -40R. It addresses unsafe conditions related to fan disks with surface rollovers in the dovetail slot area. The AD mandates removal and replacement of affected fan disks to ensure continued airworthiness.
EASA AD 2019-0061
EASA Airworthiness Directive 2019-0061 is an airworthiness directive addressing certain GE Aviation Czech M601 series engines installed on various aircraft including the Aircraft Industries L-410 series, Air Tractor AT series, Allied Ag Cat G-164 series, PZL-106 Kruk, RUAG Do 28 series, and Thrush S-2R series. The directive mandates inspection and potential replacement of power turbine discs with specific part numbers and serial numbers to prevent failure due to damage or non-conforming geometry.
EASA AD 2019-0051R1
EASA Airworthiness Directive 2019-0051R1 is an interim safety directive affecting all Boeing 737-8 and 737-9 MAX aircraft. It suspends normal flight operations of these models due to safety concerns following two fatal accidents and allows only limited ferry flights under strict conditions. The directive aims to ensure continued airworthiness pending further investigation and corrective actions.
EASA AD US-2019-03-06
FAA Airworthiness Directive 2019-03-06 is a final rule addressing certain Boeing 737-300, -400, and -500 series airplanes. It requires the installation of lanyard assemblies on passenger service units (PSUs) and, for some airplanes, on the life vest panels to prevent PSUs from detaching during survivable accidents. This directive aims to enhance cabin safety by reducing the risk of injury and obstruction during evacuations.
EASA AD US-2019-03-07
Airworthiness Directive 2019-03-07 is a final rule issued by the Federal Aviation Administration addressing The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. It mandates inspections of the Krueger flap bullnose attachment hardware to detect discrepancies and missing hardware that could cause the bullnose to detach during flight. The directive expands applicability to all airplanes with Krueger flap bullnose installations due to the rotable nature of the parts.
EASA AD 2019-0060
EASA Airworthiness Directive 2019-0060 is an official directive addressing inspection requirements for the tail rotor gearbox actuating rods on Airbus Helicopters AS 350 and AS 355 models. It mandates dye penetrant inspections and marking of specific tail rotor gearbox actuating rods to detect cracks and prevent loss of yaw control. The directive applies to all serial numbers of the affected helicopter models and includes detailed part numbers and manufacturing dates for inspection.
EASA AD 2019-0057
EASA Airworthiness Directive 2019-0057 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Leonardo S.p.A. A119 and AW119MKII helicopters. It addresses the inspection and replacement of collective stick torque tube assemblies, specifically part number 109-0011-03-105 from certain batch numbers, due to a manufacturing defect that could affect helicopter controllability.