EASA Regulations for Airbus A319

253 airworthiness directives and regulations affecting Airbus A319.

EASA AD 2024-0105

May 30, 2024

Fuselage — Potable and Waste Water Service Panels — Modification

EASA Airworthiness Directive 2024-0105 is issued for Airbus A319 aeroplanes, specifically models A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, and A319-133, excluding those with certain Airbus modifications already embodied. The directive addresses modifications to the fuselage potable and waste water service panels to ensure structural integrity. It mandates compliance with Airbus Service Bulletin A320-53-1517 to correct identified fatigue issues.

Airworthiness Directive
  • Airbus A319

EASA AD 2024-0077

Apr 25, 2024

[Correction] Fuselage — Pressure Panel Longitudinal Beams — Inspection / Repair / Modification

EASA Airworthiness Directive 2024-0077 is a regulatory document addressing inspection, repair, and modification requirements for the pressure panel longitudinal beams on Airbus A318, A319, A320, and A321 aircraft. It targets all manufacturer serial numbers except those with Airbus modification 151574 embodied in production. The directive aims to ensure structural integrity by mandating inspections and corrective actions related to fatigue cracks found around fasteners connecting the pressure panel to the flexible bracket at fuselage frame 36.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0093

Apr 22, 2024

Engine — Non-Synchronous Vibration During Engine Operation — Monitoring

EASA Airworthiness Directive 2024-0093 addresses non-synchronous vibration (NSV) issues during operation of CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts, notably bearing No. 3 spring finger housings with certain part numbers and serial numbers, to ensure ongoing engine safety and airworthiness. It mandates monitoring and corrective actions to prevent potential engine stalls and turbine failures.

Airworthiness Directive
  • CFM International LEAP-1A
  • CFM International LEAP-1C
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0089

Apr 15, 2024

Fuselage — Main Landing Gear Bay Rear Panel — Inspections

EASA Airworthiness Directive 2024-0089 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes. It mandates repetitive special detailed inspections of the main landing gear bay rear panel at specific stringer and frame locations to detect cracks. This directive applies to various models except those with certain Airbus modifications or service bulletins already embodied.

Airworthiness Directive
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2022-0096R2

Apr 12, 2024

Auto Flight – New flight Guidance Standard – Modification

EASA Airworthiness Directive 2022-0096R2 is an amendment addressing flight guidance system issues on Airbus A319, A320, and A321 aeroplanes equipped with certain Flight Guidance (FG) 2G and 3G standards. It mandates modifications to the aircraft flight manual and installation of updated FG software to prevent pitch-up attitudes and autopilot disconnections during go-around maneuvers, particularly when operating with high aft center of gravity and specific thrust configurations.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0068

Mar 11, 2024

Fuselage — Lateral Cockpit Window Frame Upper Stiffener — Inspection

EASA Airworthiness Directive 2024-0068 is an inspection directive affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates special detailed inspections of the lateral cockpit window frame upper stiffener at fuselage frame 4 to detect cracks that could compromise structural integrity. The directive applies to specific aircraft configurations excluding those with certain Airbus modifications embodied in production or service.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0067-E

Mar 9, 2024

Engine — Life Limited Parts — Replacement

EASA Airworthiness Directive 2024-0067-E is an emergency directive addressing life limited parts replacement for CFM International CFM56 series engines, including models CFM56-2, -3, -5, -5B, -5C, and -7B. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737 series aircraft from the 300 to 900ER variants. The directive targets specific compressor discharge pressure seals, high-pressure compressor stage 3 disks, and high-pressure turbine rear shafts identified as affected parts due to potential damage from improper maintenance.

Airworthiness Directive
  • CFM International CFM56-2
  • CFM International CFM56-3
  • CFM International CFM56-5
  • CFM International CFM56-5B
  • CFM International CFM56-5C
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737

EASA AD 2024-0066

Mar 8, 2024

Time Limits / Maintenance Checks — Safe Life Airworthiness Limitations Items — ALS Part 1 — Amendment

EASA Airworthiness Directive 2024-0066 is an amendment concerning the Airbus A318, A319, A320, and A321 aircraft models. It updates the Safe Life Airworthiness Limitations Items in the Airworthiness Limitations Section Part 1, Revision 09, to ensure continued airworthiness through mandatory maintenance tasks and life limits. This directive applies to all serial numbers of the specified Airbus A320 family aircraft.

Airworthiness Directive
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0046

Feb 19, 2024

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 4 – System Equipment Maintenance Requirements – Amendment

EASA Airworthiness Directive 2024-0046 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the Airbus A318/A319/A320/A321 Airworthiness Limitations Section Part 4 Revision 09, which includes system equipment maintenance requirements and life limits for components. This directive ensures continued airworthiness by requiring operators to follow updated maintenance tasks and replacement schedules.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0047

Feb 19, 2024

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 5 – Fuel Airworthiness Limitations – Amendment

EASA Airworthiness Directive 2024-0047 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated fuel airworthiness limitations specified in Airbus Airworthiness Limitations Section Part 5 Revision 08. The directive ensures continued airworthiness by requiring maintenance tasks and life limit replacements as per the latest approved maintenance program.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0038

Feb 5, 2024

Equipment / Furnishings – Galleys – Inspection

EASA Airworthiness Directive 2024-0038 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It addresses inspection and modification requirements for forward-facing galley parts with specific part numbers to prevent damage that could lead to trolley detachment during emergency landings. This directive applies to all manufacturer serial numbers of the listed aircraft models.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0031

Feb 1, 2024

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitations Items – Amendment

EASA Airworthiness Directive 2024-0031 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with updated Damage Tolerance Airworthiness Limitations Items specified in the Airbus Airworthiness Limitations Section Part 2 Revision 10. This directive ensures continued airworthiness by requiring operators to follow new and/or more restrictive maintenance tasks.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0030

Jan 31, 2024

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 3 – Certification Maintenance Requirements – Amendment

EASA Airworthiness Directive 2024-0030 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A318, A319, A320, and A321 aeroplanes. It mandates compliance with the updated Airbus Airworthiness Limitations Section (ALS) Part 3 Revision 09, which contains certification maintenance requirements essential for continued airworthiness. This directive applies to all manufacturer serial numbers of the specified Airbus A320 family models.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0027

Jan 25, 2024

Wings – Bottom Wing Skin Panel 2 – Inspection

EASA Airworthiness Directive 2024-0027 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A319, A320, and A321 aeroplanes, including both Current Engine Option (CEO) and New Engine Option (NEO) models. It addresses potential fatigue cracking in the bottom wing skin manhole access panel attachment holes between Rib 13 and Rib 26 on both left and right wings. The directive mandates inspections and corrective actions to ensure structural integrity of the wings.

Airworthiness DirectiveSuperseded
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0026

Jan 24, 2024

Engine — High Pressure Turbine — Rotor Interstage Seal — Replacement

EASA Airworthiness Directive 2024-0026 is an airworthiness directive addressing the replacement of the High Pressure Turbine Rotor Interstage Seal on CFM International LEAP-1A engines installed on certain Airbus A319, A320, and A321 aircraft. The directive targets specific affected parts identified by part number 2466M68P02 and certain serial numbers. It mandates replacement of these parts to ensure continued safe operation of the engines.

Airworthiness Directive
  • CFM International LEAP-1A
  • CFM International LEAP-1C
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0022

Jan 23, 2024

Landing Gear — Nose Landing Gear — Repair Assessment

Landing Gear — Nose Landing Gear — Repair Assessment is a regulatory document concerning the Airbus S.A.S. A319, A320, and A321 aircraft types. It addresses the assessment procedures for repairs related to the nose landing gear to ensure continued airworthiness and safety. The document provides guidance on evaluating repair conditions and standards for these specific aircraft models.

Other
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA SIB 2024-02

Jan 22, 2024

Emergency Exit Safety Barriers Modification / Models Selection

EASA Safety Information Bulletin 2024-02 is an airworthiness bulletin addressing emergency exit safety barriers on Airbus A318, A319, A320, and A321 aircraft. It provides information on the different part numbers of safety barriers used during maintenance to prevent personnel from falling through open doors. The bulletin highlights concerns about the retention forces of certain upgraded barrier designs and introduces improved versions with enhanced nozzle ends.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2024-0002

Jan 4, 2024

Engine — High-Pressure Turbine Inner Stationary Seal — Inspection

EASA Airworthiness Directive 2024-0002 is an airworthiness directive addressing the inspection of the high-pressure turbine (HPT) inner stationary seal on CFM International CFM56-5B, CFM56-5C, and CFM56-7B engines. These engines are commonly installed on Airbus A318, A319, A320, A321, A340, and Boeing 737-600 through 737-900ER series aircraft. The directive mandates inspections and corrective actions to prevent potential damage caused by cracks and honeycomb separation in the affected seals.

Airworthiness Directive
  • CFM International CFM56-5B
  • CFM International CFM56-5C
  • CFM International CFM56-7B
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A340
  • Boeing 737-600
  • Boeing 737-700
  • Boeing 737-800
  • Boeing 737-900ER

EASA AD 2023-0212

Dec 6, 2023

Fuselage – Double Joggle Area at Frame 16 and Frame 20 – Inspection

EASA Airworthiness Directive 2023-0212 is issued for Airbus A318, A319, A320, and A321 aeroplanes to address potential cracks in the fuselage double joggle areas at frames 16 and 20 on both right-hand and left-hand sides. The directive applies to both Current Engine Option (CEO) and New Engine Option (NEO) models, requiring special detailed inspections and optional modifications to reinforce affected areas. This directive ensures continued structural integrity and airworthiness of the affected Airbus aircraft models.

Airworthiness DirectiveSuperseded
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321

EASA AD 2023-0209

Nov 22, 2023

Oxygen – Chemical Oxygen Generators – Replacement

EASA Airworthiness Directive 2023-0209 is an airworthiness directive issued by the European Union Aviation Safety Agency addressing chemical oxygen generators installed on various Airbus aircraft models including A310, A300, A318, A319, A320, A321, A330, and A340 series. The directive targets specific part numbers of chemical oxygen generators that have shown failures to activate, potentially reducing oxygen availability in emergencies. It mandates replacement of affected oxygen generators to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded
  • Airbus A310
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • Airbus A300600600ST (Beluga)