EASA Regulations for Airbus A300-600

62 airworthiness directives and regulations affecting Airbus A300-600.

EASA AD 2021-0190

Aug 17, 2021

Wings – Main Landing Gear Support Rib 5 – Inspection

EASA Airworthiness Directive 2021-0190 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A300, A300-600, and A300-600ST aeroplanes. It addresses the detection of cracks in the main landing gear support Rib 5 lower flange area on both right and left sides of the aircraft. The directive mandates inspections to ensure the structural integrity of these aircraft models.

Airworthiness DirectiveSuperseded
  • Airbus A300600600ST (Beluga)600ST

EASA AD 2021-0106

Apr 15, 2021

Hydraulic Power — Fire Shut-Off Valves — Inspection

EASA Airworthiness Directive 2021-0106 is an official safety directive addressing hydraulic power fire shut-off valves on Airbus A300, A310, A300-600, and A300-600ST aeroplanes. It mandates inspection of fire shut-off valves installed on the wings to detect incorrect actuator installation that could cause valve failure. The directive applies to all certified models and manufacturer serial numbers of these aircraft types.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)600ST
  • Airbus A310

EASA AD 2021-0093

Mar 30, 2021

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

EASA Airworthiness Directive 2021-0093 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models and serial numbers of Airbus A300-600 aeroplanes. It mandates updates to the airworthiness limitations section, specifically Part 2 related to damage tolerant airworthiness limitation items. The directive ensures operators comply with the latest maintenance tasks and thresholds to maintain continued airworthiness.

Airworthiness DirectiveSuperseded
  • Airbus A300-600

EASA AD 2020-0145

Jul 1, 2020

Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification

The document titled 'Landing Gear — Main Landing Gear Hinge Arm / Barrel — Pin Replacement / Inspection / Spacer Modification' is an airworthiness directive applicable to Airbus S.A.S. aircraft models A300, A300-600, and A300-600ST (Beluga). It addresses maintenance procedures related to the main landing gear hinge arm and barrel, focusing on pin replacement, inspection, and spacer modification to ensure continued airworthiness and safety.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)600ST

EASA AD 2020-0111R2

Jun 16, 2020

Superseded by EASA AD 2024-0009

EASA Airworthiness Directive 2020-0111R2 is an updated safety directive affecting all certified Airbus A300-600 aeroplanes. It mandates repetitive special detailed inspections of specific structural areas including the outer wing bottom skin and fuselage internal structure to detect cracks that could compromise structural integrity. The directive ensures continued airworthiness by requiring compliance with Airbus Airworthiness Limitations Section tasks.

Airworthiness DirectiveSuperseded
  • Airbus A300-600

EASA AD 2020-0108

May 14, 2020

Equipment / Furnishings — Emergency Locator Transmitter — Modification

EASA Airworthiness Directive 2020-0108 is an official regulatory document addressing a safety issue on Airbus A300-600 and A310 aeroplanes. It specifically targets Emergency Locator Transmitters (ELTs) with Part Number 01N65900 installed on these aircraft models. The directive mandates modifications to improve protection against electrical current injection that could cause battery fires.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A310

EASA AD 2020-0050

Mar 11, 2020

[Correction] Fuselage — Main Deck Cargo Crossbeams — Inspection / Repair

EASA Airworthiness Directive 2020-0050 is a corrective directive addressing inspection and repair of the main deck cargo crossbeams on Airbus A300-600 aeroplanes, specifically models A300 F4-605R and A300 F4-622R with manufacturer serial numbers 805 to 872 inclusive. The directive mandates repetitive detailed inspections and corrective actions for damage found between frame 48 and frame 54 on the right-hand side of the fuselage. An optional modification is provided to terminate the need for repetitive inspections.

Airworthiness Directive
  • Airbus A300-600

EASA AD 2019-0188

Jul 31, 2019

Hydraulic Power — Hydraulic Reservoir Air Pressurization System Lines — Functional Tests

EASA Airworthiness Directive 2019-0188 is an airworthiness directive affecting Airbus A300-600, A300-600ST, and A310 aeroplanes. It mandates functional tests of the hydraulic reservoir air pressurization system lines to detect pipe ruptures and air leaks. The directive ensures continued airworthiness by requiring specific maintenance tasks related to hydraulic power systems.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A300-600ST (Beluga)
  • Airbus A310
  • Airbus A300-600ST

EASA AD 2019-0090

Apr 26, 2019

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

EASA Airworthiness Directive 2019-0090 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all certified models and serial numbers of Airbus A300-600 aeroplanes. It mandates compliance with the Damage Tolerant Airworthiness Limitation Items as specified in the Airbus A300-600 Airworthiness Limitations Section Part 2, Revision 03. This directive ensures continued airworthiness by updating maintenance tasks and intervals.

Airworthiness DirectiveSuperseded
  • Airbus A300-600

EASA AD 2019-0085

Apr 18, 2019

Oxygen – Crew and Passenger Oxygen Cylinders – Inspection /; Replacement

EASA Airworthiness Directive 2019-0085 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting various Airbus aeroplanes including the A300, A310, A318, A319, A320, A321, A330 (except A330-223F and A330-243F), and A340 models. The directive addresses inspection and replacement requirements for specific oxygen cylinders with part numbers 89794077, 89794015, and 891511-14 due to a manufacturing defect. This AD mandates inspection of the hand valve assembly on affected oxygen cylinders to prevent oxygen leakage and potential safety hazards.

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

EASA AD 2019-0078

Mar 29, 2019

Flight Controls — Trimmable Horizontal Stabilizer Actuator Ball Nut Trunnion Lower Attachment — Inspection of Right-Hand Bearing Installation

EASA Airworthiness Directive 2019-0078 is an airworthiness directive addressing the inspection of the right-hand bearing installation on the trimmable horizontal stabilizer actuator ball nut trunnion lower attachment for Airbus A300, A300-600, A300-600ST, and A310 aeroplanes. It mandates a one-time detailed inspection of the affected parts to ensure proper installation and prevent potential actuator failure. The directive applies to all certified models and serial numbers of these Airbus aircraft.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)600ST
  • Airbus A310

EASA AD 2019-0014

Jan 29, 2019

Electrical Power — Wing Electrical Installation — Modification

EASA Airworthiness Directive 2019-0014 is an official regulatory document addressing electrical power wing installation modifications for Airbus A300-600, A300-600ST, and A310 aeroplanes. It mandates modifications to the wing electrical installations to prevent damage caused by insufficient clearance and potential chafing of electrical harnesses. The directive applies to all certified models and serial numbers of these aircraft types.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A300-600ST (Beluga)
  • Airbus A310
  • Airbus A300-600ST

EASA AD 2019-0017

Jan 29, 2019

Flight Controls / Stabilizers — Rudder Servo Control — Inspection

Flight Controls / Stabilizers — Rudder Servo Control — Inspection is a regulatory document applicable to AIRBUS S.A.S. aircraft models A300, A300-600, A300-600ST (Beluga), and A310. This document outlines inspection requirements for the rudder servo control systems on these aircraft types to ensure continued airworthiness and flight safety. It provides guidance for maintenance and inspection procedures specific to these Airbus models.

Airworthiness Directive
  • Airbus A300600600ST (Beluga)600ST
  • Airbus A310

EASA AD 2019-0006

Jan 17, 2019

Stabilizers — Composite Vertical Tailplane Attachment Fittings — Inspection

EASA Airworthiness Directive 2019-0006 is an airworthiness directive addressing inspection requirements for composite vertical tailplane attachment fittings on Airbus A310, A300-600, and A300-600ST aircraft. It mandates review and inspection of affected parts to detect potential delamination that could compromise the vertical tailplane attachment fittings. The directive applies to all certified models with Airbus modification 04886 embodied in production.

Airworthiness Directive
  • Airbus A300-600
  • Airbus A300-600ST (Beluga)
  • Airbus A310
  • Airbus A300-600ST

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 2013-0184R2

Dec 3, 2018

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.

Airworthiness Directive
  • Airbus A300600

EASA AD 2018-0170

Aug 6, 2018

Landing Gear – Main Landing Gear Hinge Arm / Barrel Pin – Inspection

EASA Airworthiness Directive 2018-0170 is an airworthiness directive issued for Airbus A300, A300-600, and A300-600ST aeroplanes. It addresses the inspection of main landing gear hinge arms and barrel pins, specifically parts with Part Numbers C66441-(X) and C65543-(X), to detect cracks that could lead to landing gear collapse. The directive mandates detailed visual inspections to ensure continued airworthiness and safety.

Airworthiness DirectiveSuperseded
  • Airbus A300600600ST (Beluga)600ST

EASA AD 2018-0161

Jul 25, 2018

Fuselage — Trimmable Horizontal Stabilizer Support Struts — Inspection

EASA Airworthiness Directive 2018-0161 is an airworthiness directive addressing inspection requirements for the trimmable horizontal stabilizer (THS) support struts on Airbus A300, A300-600, and A310 aeroplanes. It applies to all certified models and serial numbers of these aircraft and focuses on detecting cracks caused by stress corrosion in the aluminium THS support struts. The directive mandates repetitive inspections and corrective actions to ensure continued airworthiness and prevent potential structural failure of the horizontal tailplane.

Airworthiness Directive
  • Airbus A300600
  • Airbus A310

EASA SIB 2012-07

May 9, 2012

Diehl Comfort Modules (formerly DASELL) Baby Nursing Tables - Hinge Replacement

EASA Safety Information Bulletin 2012-07 addresses the replacement of pivot-type hinges with piano-type hinges on Diehl Comfort Modules (formerly DASELL) baby nursing tables installed on Airbus A319, A320, A321, A300-600, A310, and A330 aircraft. The bulletin informs operators about reported incidents of finger injuries and infant entrapment caused by the folding mechanism of these nursing tables. It provides references to Airbus service bulletins and operator information telexes related to design improvements and safety measures.

Safety Information Bulletin
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A300-600
  • Airbus A310
  • Airbus A330