RegNotify

EASA Regulations & Airworthiness Directives

Browse 4771 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320262Airbus A321257Airbus A319229Airbus A350206Airbus A330197All177Airbus A318172Boeing 737164Airbus A380162Airbus A340136Airbus A350-941119Airbus Helicopters AS 332110Airbus Helicopters EC 225107Airbus Helicopters SA 330107Boeing 787106Show all...

EASA AD 18-139

WITHDRAWN - EXPLANATORY STATEMENT ATTACHED

EASA Withdrawal Statement for Proposed AD 18-139 announces the withdrawal of the proposed airworthiness directive concerning Airbus Helicopters BK117 D-2 and D-2m models equipped with Helionix Step 2 avionics. The withdrawal follows Airbus Helicopters' publication of Temporary Revision 3 to the Rotorcraft Flight Manual, which amended night operation procedures and restored an acceptable safety level. A modification application submitted by Airbus Helicopters is expected to provide a final fix for the identified unsafe condition.

Dec 13, 2018
Agency DecisionSafety MgmtFlight OpsAirbus Helicopters MBB-BK 117Airbus Helicopters BK117 D-2Airbus Helicopters BK117 D-2m

EASA AD US-2018-23-09

Stabilizers - Horizontal Stabilizers - Inspection

Airworthiness Directive 2018-23-09 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 horizontal stabilizers to detect cracks in the rear spar upper chord caused by galvanic corrosion due to a manufacturing oversight involving missing protective finishes on certain bushings.

Dec 12, 2018
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-600Boeing 737-700Boeing 737-700CBoeing 737-800Boeing 737-900Boeing 737-900ER

EASA AD 2018-0271

SUPERSEDED BY EASA AD 2019-0115

EASA Airworthiness Directive 2018-0271 is an airworthiness directive issued for Airbus A350-941 aeroplanes with specific manufacturer serial numbers. It addresses the issue of baby bassinet inserts installed on stowages and partitions that were found loose due to missing application of a self-securing fixation device. The directive mandates repetitive inspections to ensure the tightness of these inserts to prevent potential detachment and injury.

Dec 12, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941

EASA AD US-2018-23-51

SUPERSEDED BY FAA AD 2020-24-02

FAA Airworthiness Directive 2018-23-51 is a final rule affecting all Boeing 737-8 and 737-9 airplanes. It requires revising the airplane flight manual to include procedures for flight crews to handle runaway horizontal stabilizer trim caused by erroneous high angle of attack sensor inputs. This directive addresses a safety risk identified by the manufacturer that could lead to loss of control and potential terrain impact.

Dec 12, 2018
Airworthiness DirectiveFlight OpsSafety MgmtBoeing 737Boeing 737-8Boeing 737-9

EASA AD 2018-0270

Windows — Passenger Windows — Repair

EASA Airworthiness Directive 2018-0270 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. AW119MKII helicopters. It addresses an issue with passenger windows that were improperly installed during production on certain serial-numbered helicopters. The directive mandates corrective actions to ensure the windows can be safely jettisoned in emergencies.

Dec 12, 2018
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters A109Leonardo S.P.A. Helicopters A119Leonardo AW119MKII

EASA AD CF-2018-31

Landing Gear System — Alternate Extension System — Introduction of New Airworthiness Limitation

Canadian Airworthiness Directive CF-2018-31 mandates a new airworthiness limitation for the landing gear system's alternate extension system on Bombardier Inc. model CL-600-2C10, CL-600-2D15, and CL-600-2D24 aircraft. This directive introduces a new maintenance requirement to ensure the operational reliability of the alternate extension system. It applies to these specific Bombardier regional jets and aims to enhance safety through updated inspection intervals.

Dec 11, 2018
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2C10Bombardier CL-600-2D15Bombardier CL-600-2D24

EASA AD 2018-0266

SUPERSEDED BY EASA AD 2023-0117

EASA Airworthiness Directive 2018-0266 is an airworthiness directive issued for Airbus A300F4-605R and A300F4-622R aeroplanes equipped with Airbus modification 12046. It addresses the inspection and maintenance of aft cargo door frame forks to detect cracks and prevent structural integrity issues. The directive mandates specific inspections and corrective actions to ensure continued airworthiness of affected aircraft.

Dec 11, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600Airbus A300F4-605RAirbus A300F4-622R

EASA SIB 2018-18R1

Use of Restraint Systems and Pilot Back Protection during Parachute Operations

EASA Safety Information Bulletin 2018-18R1 provides updated guidance on the use of restraint systems and pilot back protection during parachute operations in Part 23 certificated aeroplanes. It addresses the design and operational requirements for modifications to aircraft used in parachuting activities, emphasizing risk assessments for installing restraint systems or alternative means to hold on, as well as pilot back protection. This bulletin applies to operators conducting parachute operations and Design Organization Approval holders involved in aircraft modifications for such operations.

Dec 11, 2018
Safety Information BulletinFlight OpsSafety Mgmt

EASA AD 2018-0269

Wings — Center Wing Ribs — Inspection / Modification

EASA Airworthiness Directive 2018-0269 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Vulcanair P.68 series aeroplanes, specifically the AP68TP-300 "Spartacus" and AP68TP-600 "Viator" models with certain serial numbers. The directive addresses inspection and modification requirements for the center wing ribs, specifically ribs #3 and #4 on both left and right wings, to ensure structural integrity.

Dec 11, 2018
Airworthiness DirectiveMaintenanceSafety MgmtVulcanair AP.68TPVulcanair P.68 AP68TP-300Vulcanair P.68 AP68TP-600

EASA AD 2018-0267

Wings — Movable Flap Track Fairing #2 U-Frame Bolt-Nut Couples — Inspection

EASA Airworthiness Directive 2018-0267 is an airworthiness directive applicable to Airbus A380-841, A380-842, and A380-861 aeroplanes with manufacturer serial numbers 0222 to 0233 inclusive, excluding 0229 and 0232. It addresses inspection requirements for the movable flap track fairing number 2 U-frame bolt-nut couples on both left-hand and right-hand sides. The directive mandates inspection, replacement, and re-torqueing of these components to ensure continued airworthiness.

Dec 11, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A380

EASA AD US-2018-22-01

Engine - Second Stage Turbine Rotors - Removal

The Federal Aviation Administration's Airworthiness Directive 2018-22-01 addresses Honeywell International Inc. TPE331 turboprop engines, specifically models TPE331-8, -10, -10N, -10R, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, and -11U equipped with certain second stage turbine rotor assemblies. This directive mandates the removal of specific second stage turbine rotors at reduced life limits to prevent unsafe conditions. It was issued following reports of uncontained rotor separation and discovery of cracks in the turbine rotors.

Dec 10, 2018
Airworthiness DirectiveMaintenanceSafety MgmtHoneywell International TPE331

EASA AD 2018-0263

Time Limits / Maintenance Checks — Main Gearbox Magnetic Plugs — Inspection Main Rotor Drive — Planet Gear Assemblies — Replacement

EASA Airworthiness Directive 2018-0263 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters EC 155 B and EC 155 B1 models. It addresses inspection and replacement requirements for main gearbox magnetic plugs and planet gear assemblies to ensure continued airworthiness and safety. The directive mandates inspections and potential replacement of affected planet gear assemblies identified by specific part and serial numbers.

Dec 7, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SAAirbus Helicopters AS 365Airbus Helicopters EC 155Airbus Helicopters EC 155 BAirbus Helicopters EC 155 B1

EASA AD 2018-0262

SUPERSEDED BY CAA UK AD G-2022-0011

EASA Airworthiness Directive 2018-0262 is an airworthiness directive addressing safety concerns with IPECO HOLDING Ltd Type 3A063 pilot and co-pilot seats installed on ATR 42 and ATR 72 aircraft. It mandates modifications and inspections to prevent unexpected rearward movement of flight crew seats caused by worn or defective track lock springs and guide blocks. The directive applies to specific seat part numbers listed in the document.

Dec 6, 2018
Airworthiness DirectiveMaintenanceSafety MgmtATR 42ATR 72

EASA AD 2017-0151R1

Engine — Exhaust System — Modification

EASA Airworthiness Directive 2017-0151R1 is a regulatory document addressing modification requirements for the exhaust system of GE Aviation Czech M601, H75, H80, and H85 series engines. These engines are commonly installed on aircraft such as Thrush Aircraft Inc. S-2R, PZL-106 Kruk, Air Tractor AT-300/400/500 series, Allied Ag Cat G-164 series, RUAG Do 28, and Aircraft Industries L-410. The directive mandates modifications to prevent potential power turbine or quill shaft spline failures that could lead to engine overspeed and subsequent safety hazards.

Dec 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtGe Aviation Czech H75, H80, H85Ge Aviation Czech M601Thrush Aircraft Inc. S-2RPZL-106 KrukAir Tractor AT-300Air Tractor AT-400Air Tractor AT-500Allied Ag Cat G-164RUAG Do 28Aircraft Industries L-410

EASA AD US-2018-21-12

Engine Fuel & Control - Fuel Manifold - Removal / Replacement

The document titled "Engine Fuel & Control - Fuel Manifold - Removal / Replacement" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2018-21-12) addressing certain General Electric Company GEnx-2B67, -2B67B, and -2B67/P turbofan engines. It mandates the removal and replacement of specific top main and lower fuel manifolds due to low-cycle fatigue cracking that could lead to engine fires. This AD affects engines installed on U.S. registered aircraft and aims to enhance engine safety.

Dec 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric GEnx

EASA AD 2018-0245R1

SUPERSEDED BY EASA AD 2019-0168

EASA Airworthiness Directive 2018-0245R1 is an amendment addressing safety concerns on Airbus A350-941 and A350-1041 aeroplanes related to the crew oxygen cylinder assemblies with part number 4441227-058-000. The directive mandates operational checks and replacement of affected oxygen cylinder assemblies to prevent potential ignition or fire during ground operational testing. This directive applies to all manufacturer serial numbers of the specified Airbus A350 models.

Dec 5, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A350Airbus A350-941Airbus A350-1041

EASA AD 2013-0184R2

Fuselage — Frame 47 Splice Fitting Holes Between Stringers 24 and 26 — Inspection

EASA Airworthiness Directive 2013-0184R2 is a regulatory document addressing inspection requirements for the fuselage frame 47 splice fitting holes between stringers 24 and 26 on Airbus A300 and A300-600 aeroplanes. It mandates high frequency eddy current inspections to detect cracks that could compromise structural integrity. The directive applies to all manufacturer serial numbers of the specified Airbus models and includes detailed inspection thresholds and intervals.

Dec 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300Airbus A300-600

EASA AD 2018-0261-E

SUPERSEDED BY EASA AD 2019-0023

EASA Airworthiness Directive 2018-0261-E is an emergency directive addressing safety concerns on Leonardo S.p.A. AW169 and AW189 helicopters. It mandates repetitive inspections of the tail rotor servo actuator's castellated nut and the tail rotor duplex bearing to detect potential issues that could lead to loss of yaw control. This directive applies to all serial numbers of AW169 and AW189 helicopters.

Dec 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AW169Leonardo S.P.A. Helicopters AW189Leonardo AW169Leonardo AW189

EASA AD 2018-0260

SUPERSEDED BY EASA AD 2023-0194

EASA Airworthiness Directive 2018-0260 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters AS 332 C, C1, L, and L1 models. It addresses the life limits and replacement requirements for main gearbox suspension bar fittings and screws to ensure continued airworthiness. The directive applies to specific part numbers related to the main gearbox suspension bar attachment fittings and screws.

Dec 3, 2018
Airworthiness DirectiveMaintenanceSafety MgmtAirbus Helicopters SA 330Airbus Helicopters AS 332Airbus Helicopters EC 225Airbus Helicopters AS 332 CAirbus Helicopters AS 332 C1Airbus Helicopters AS 332 LAirbus Helicopters AS 332 L1

EASA SIB CE-18-32

Textron Aviation Model 208B Aeroplanes - Engine Oil System (Airframe Furnished) - Flapper Check Valve Failure

The Special Airworthiness Information Bulletin SAIB: CE-18-32 is an FAA informational bulletin addressing the failure of the engine oil system flapper check valve on Textron Aviation Model 208B airplanes equipped with the PT6A-140 engine. It alerts owners, operators, and maintenance personnel about failures of check valve part number C100490-1 on certain serial numbers of the 208B EX model. The bulletin provides details on the issue without mandating regulatory action.

Dec 3, 2018
Safety Information BulletinMaintenanceSafety Mgmt