EASA Regulations & Airworthiness Directives

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

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA AD 2018-0275

Dec 14, 2018

Wings — Frame 56 Vertical Cruciform Fittings — Inspection / Modification

EASA Airworthiness Directive 2018-0275 is an official regulatory document addressing inspection and modification requirements for the vertical cruciform fittings at fuselage frame 56 on Airbus A380-841, A380-842, and A380-861 aeroplanes. It applies to all serial numbers except those with Airbus modifications 75132 or 75442 incorporated during production. The directive mandates inspections and potential modifications to ensure structural integrity of the affected wing fittings.

Airworthiness Directive
  • Airbus A380841842861

EASA AD 2018-0274

Dec 13, 2018

Landing Gear — Main Landing Gear Leg — Modification

EASA Airworthiness Directive 2018-0274 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of PZL W-3A helicopters. It mandates a modification to the left-hand main landing gear leg to prevent damage to the wheel braking system pneumatic line caused by rescue hoist operations. The directive ensures continued safe operation of the affected helicopters by addressing a specific landing gear component vulnerability.

Airworthiness Directive
  • Wsk Pzl-Swidnik PZL W-3A
  • PZL W-3A

EASA AD 2018-0273

Dec 13, 2018

Time Limits / Maintenance Checks – Airworthiness Limitations Section – Amendment

EASA Airworthiness Directive 2018-0273 is an airworthiness directive issued by the European Aviation Safety Agency concerning SAFRAN Helicopter Engines ARRIEL 2D, 2E, and 2N models. It applies to these engines installed on Airbus Helicopters AS 350 B3 (H125), EC 130 T2 (H130), and MBB-BK117 D-2 (EC 145 T2 or H145) helicopters. The directive mandates compliance with updated airworthiness limitations and maintenance tasks as specified in the latest SAFRAN ARRIEL 2 Maintenance and Overhaul Manuals.

Airworthiness DirectiveSuperseded
  • Safran ARRIEL 2
  • Airbus Helicopters AS 350 B3
  • Airbus Helicopters EC 130 T2
  • MBB-BK117 D-2

EASA AD 2018-0272

Dec 13, 2018

Time Limits / Maintenance Checks – Main Gearbox / Particle Detectors – Inspection

EASA Airworthiness Directive 2018-0272 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus Helicopters SA 330 J models. It mandates inspections of the main gearbox particle detectors and bottom housing (oil sump) to detect potential failures of the second stage planet gear, which could lead to loss of helicopter control.

Airworthiness DirectiveSuperseded
  • Airbus Helicopters SA 330
  • Airbus Helicopters AS 332
  • Airbus Helicopters EC 225
  • Airbus Helicopters SA 330 J

EASA PAD 18-139

Dec 13, 2018

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.

Proposed AD
  • Airbus Helicopters MBB-BK 117
  • Airbus Helicopters BK117 D-2
  • Airbus Helicopters BK117 D-2m

EASA AD 2018-0271

Dec 12, 2018

Equipment / Furnishings – Baby Bassinet Inserts – Inspection

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.

Airworthiness DirectiveSuperseded
  • Airbus A350941

EASA AD US-2018-23-09

Dec 12, 2018

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.

Airworthiness Directive
  • Boeing 737600700700C800900900ER

EASA AD US-2018-23-51

Dec 12, 2018

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.

Airworthiness Directive
  • Boeing 73789

EASA AD 2018-0270

Dec 12, 2018

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.

Airworthiness Directive
  • Leonardo S.P.A. Helicopters A109
  • Leonardo S.P.A. Helicopters A119
  • Leonardo AW119MKII

EASA AD 2018-0266

Dec 11, 2018

Doors – Aft Cargo Door Frame Forks – Inspection

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.

Airworthiness DirectiveSuperseded
  • Airbus A300-600
  • Airbus A300F4-605R
  • Airbus A300F4-622R

EASA AD CF-2018-31

Dec 11, 2018

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.

Airworthiness Directive
  • MHI RJ Aviation CL-600 (Regional Jet)
  • Bombardier CL-600-2C10
  • Bombardier CL-600-2D15
  • Bombardier CL-600-2D24

EASA SIB 2018-18R1

Dec 11, 2018

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.

Safety Information Bulletin

EASA AD 2018-0269

Dec 11, 2018

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.

Airworthiness Directive
  • Vulcanair AP.68TP
  • Vulcanair P.68 AP68TP-300
  • Vulcanair P.68 AP68TP-600

EASA AD 2018-0267

Dec 11, 2018

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.

Airworthiness Directive
  • Airbus A380

EASA AD US-2018-22-01

Dec 10, 2018

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.

Airworthiness Directive
  • Honeywell International TPE331

EASA AD 2018-0263

Dec 7, 2018

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.

Airworthiness Directive
  • Airbus Helicopters SA
  • Airbus Helicopters AS 365
  • Airbus Helicopters EC 155
  • Airbus Helicopters EC 155 B
  • Airbus Helicopters EC 155 B1

EASA AD 2018-0262

Dec 6, 2018

Equipment / Furnishings – Pilot and Co-pilot Seats – Modification /; Inspection

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.

Airworthiness DirectiveSuperseded
  • ATR 42
  • ATR 72

EASA AD 2017-0151R1

Dec 5, 2018

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.

Airworthiness Directive
  • Ge Aviation Czech H75, H80, H85
  • Ge Aviation Czech M601
  • Thrush Aircraft Inc. S-2R
  • PZL-106 Kruk
  • Air Tractor AT-300
  • Air Tractor AT-400
  • Air Tractor AT-500
  • Allied Ag Cat G-164
  • RUAG Do 28
  • Aircraft Industries L-410

EASA AD US-2018-21-12

Dec 5, 2018

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.

Airworthiness Directive
  • General Electric GEnx

EASA AD 2018-0245R1

Dec 5, 2018

Oxygen – Crew Oxygen Cylinder Assembly – Operational Check /; Replacement

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.

Airworthiness DirectiveSuperseded
  • Airbus A3509411041