EASA Regulations &amp; Airworthiness Directives

Oxygen — Chemical Oxygen Generators — Replacement

The document titled 'Oxygen — Chemical Oxygen Generators — Replacement' pertains to the Airbus A330 aircraft type. It addresses the replacement requirements for chemical oxygen generators installed on these aircraft to ensure continued safety and compliance with airworthiness standards. This document is relevant for operators and maintenance organizations managing Airbus A330 fleets.

Airbus A330

EASA SIB CE-19-10

Safety Information Bulletin

Rockwell Collins Pro Line 4 and Pro Line 21 Flight Management Systems

The Special Airworthiness Information Bulletin SAIB: CE-19-10 is an FAA informational bulletin addressing an issue with certain versions of the Rockwell Collins Pro Line 4 and Pro Line 21 Flight Management Systems (FMS), specifically FMC-3000, FMC-4200, FMC-5000, and FMC-6000 versions 97 through 3.2. The bulletin informs operators that deleting waypoints using the DELETE function on these FMS versions may cause the aircraft to make an incorrect turn direction during departures, STARs, or approaches. This bulletin does not apply to any specific aircraft type but relates to the affected FMS equipment installed on various aircraft.

EASA AD 2019-0137

Superseded by EASA AD 2020-0055

EASA Airworthiness Directive 2019-0137 is an airworthiness directive addressing CFM International LEAP-1B engines installed on Boeing 737-8 and 737-9 aircraft. It mandates repetitive inspections of the transfer gearbox module scavenge screens for metallic particles due to potential failure of the radial drive shaft bearing cage. The directive aims to prevent in-flight engine shutdowns caused by this failure.

CFM International LEAP-1B
Boeing 737-8
Boeing 737-9

EASA AD 2019-0139

Superseded by EASA AD 2021-0046

EASA Airworthiness Directive 2019-0139 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus Helicopters EC 120 B helicopters. It addresses the inspection and replacement requirements for main rotor hub scissors attachment bolts, specifically part number C623A21101, to prevent potential failure due to corrosion and mechanical stress. The directive mandates inspections, markings, and corrective actions to ensure continued safe operation of the affected helicopters.

Airbus Helicopters EC 120 B

EASA AD CF-2019-22

Electrical Power - Electrical Wires Chafing With Auxiliary Aft Cabin Fuel Tank Bracket

Canadian Airworthiness Directive CF-2019-22 addresses an electrical wiring issue on Bombardier Inc. CL-600-2B19 aircraft. The directive targets specific serial numbers of this model where generator power cables may chafe against the auxiliary aft cabin fuel tank bracket. This condition could lead to electrical short circuits and generator malfunctions.

MHI RJ Aviation CL-600 (Regional Jet)
Bombardier CL-600-2B19

EASA AD US-2019-11-03

Flight Controls - Main Slat Track Assemblies - Identification / Replacement

Federal Aviation Administration Airworthiness Directive 2019-11-03 is a final rule addressing certain Boeing 737-700C, -800, and -900ER series airplanes. It mandates inspection and maintenance record checks of main slat track assemblies to identify those affected by hydrogen embrittlement due to incorrect manufacturing. The directive aims to prevent potential failure of the main slat track assemblies that could lead to slat departure and compromise flight safety.

Boeing 737700C800900ER

EASA AD 2019-0136

Rotorcraft Flight Manual — Emergency Procedures Section — Amendment

EASA Airworthiness Directive 2019-0136 is an amendment to the Rotorcraft Flight Manual Emergency Procedures Section for Leonardo S.p.A. AW189 helicopters. It addresses corrections to the emergency procedure related to the "1(2) FUEL LOW" caution message in the AW189 flight manual. This directive applies to all serial numbers of AW189 helicopters and updates the emergency procedures to ensure accurate fuel consumption information.

Leonardo S.P.A. Helicopters AW189
Leonardo AW189

EASA AD 2019-0135

Superseded by EASA AD 2019-0261

EASA Airworthiness Directive 2019-0135 is an airworthiness directive addressing Rolls-Royce Trent 1000 engine models installed primarily on Boeing 787 aircraft. It mandates the removal and replacement of intermediate pressure turbine blades (IPTB) due to reported cracking caused by sulphidation corrosion, which poses a risk of engine in-flight shutdown. The directive applies to multiple Trent 1000 variants and specifies affected part numbers and serial numbers as listed in the referenced Rolls-Royce service documents.

Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000
Boeing 787

EASA AD 2019-0131

Superseded by EASA AD 2020-0113

EASA Airworthiness Directive 2019-0131 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Falcon 2000 aeroplanes. It mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 2000 Aircraft Maintenance Manual Chapter 5-40, Revision 20. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components on these aircraft.

Dassault Falcon 2000

EASA AD 2019-0132

Superseded by EASA AD 2020-0115

EASA Airworthiness Directive 2019-0132 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Dassault Aviation Mystère-Falcon 900 aeroplanes. It mandates compliance with updated airworthiness limitations published in the Dassault Mystère-Falcon 900 Aircraft Maintenance Manual Chapter 5-40, Revision 24. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

Dassault MystÃ¨re-Falcon 900
Dassault Mystère-Falcon 900

EASA AD 2019-0133

Superseded by EASA AD 2020-0116

EASA Airworthiness Directive 2019-0133 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Dassault Aviation Falcon 900EX aeroplanes, serial numbers 1 to 119 inclusive except 97. It mandates compliance with updated airworthiness limitations specified in the Dassault Falcon 900EX Aircraft Maintenance Manual Chapter 5-40, Revision 16. This directive ensures continued airworthiness by enforcing maintenance tasks and life limits for components.

Dassault Falcon 900EX

EASA AD 2019-0134

Superseded by EASA AD 2020-0117

The document titled SUPERSEDED BY EASA AD 2020-0117 is an airworthiness directive related to the Dassault Aviation Falcon 900EX aircraft. It indicates that the previous directive has been replaced by EASA AD 2020-0117, which now governs the relevant safety and maintenance requirements for this aircraft type.

Dassault Falcon 900EX

EASA AD 2019-0130-E

Jun 7, 2019

Main Landing Gear — Upper Connection — Inspection / Repair

EASA Airworthiness Directive 2019-0130-E is an emergency directive addressing the main landing gear upper connection inspection and repair for Stemme AG S12 powered sailplanes, specifically serial numbers 12-002 to 12-026 inclusive. It mandates a one-time inspection of the main landing gear installation to detect incorrect axle installation that could lead to damage or injury. The directive provides instructions for inspection and corrective actions based on findings.

Stemme Ag S12

EASA AD 2019-0128

Jun 6, 2019

Equipment / Furnishings — Seat Belt Attachment Points / Bolts — Inspection / Replacement

EASA Airworthiness Directive 2019-0128 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Pipistrel Vertical Solutions Virus SW 121 aeroplanes. It addresses the inspection and possible replacement of seat belt attachment bolts on the baggage compartment bulkhead to ensure proper thread engagement and secure attachment. The directive applies to all serial numbers of the Virus SW 121 aircraft.

Pipistrel Vertical Solutions D.O.O. Virus SW
Pipistrel Virus SW 121

EASA AD 2019-0129

Jun 6, 2019

Stabilizers — Horizontal Stabilizer Rear Attachment Bolts — Inspection / Replacement

EASA Airworthiness Directive 2019-0129 is an official regulatory document addressing the inspection and replacement of horizontal stabilizer rear attachment bolts on Pilatus PC-12 series aeroplanes, including PC-12, PC-12/45, PC-12/47, and PC-12/47E models. The directive targets bolts with specific part and production order numbers that were improperly heat treated during manufacturing. It mandates replacement of these affected bolts to ensure continued airworthiness and flight safety.

Pilatus Aircraft PC-12
Pilatus PC-12
Pilatus PC-12/45
Pilatus PC-12/47
Pilatus PC-12/47E

EASA AD 2019-0125

Equipment / Furnishing — 9G NGS XL StepX Stretcher 1120050-Series — Modification

EASA Airworthiness Directive 2019-0125 is an official regulatory document addressing the modification of the 9G NGS XL StepX Stretcher 1120050-Series installed on certain Embraer ERJ 170 and ERJ 190 series aircraft. The directive applies to all serial numbers of these aircraft modified with the affected stretcher under EASA Supplemental Type Certificate 10030758. It mandates specific modifications to the stretcher to ensure continued airworthiness and safety.

Embraer ERJ 170
Embraer ERJ 190

EASA AD 2019-0126

Fuselage — Forward Cargo Door Upper Frame Fittings and Brackets — Inspection / Modification

The document titled 'Fuselage — Forward Cargo Door Upper Frame Fittings and Brackets — Inspection / Modification' is an airworthiness directive concerning the AIRBUS S.A.S. A350 aircraft. It addresses the inspection and potential modification of the forward cargo door upper frame fittings and brackets to ensure structural integrity and safety. This directive applies specifically to the Airbus A350 model.

Airbus A350

EASA AD 2019-0124

Superseded by EASA AD 2019-0192

EASA Airworthiness Directive 2019-0124 is an airworthiness directive issued for Airbus A380 aeroplanes, specifically models A380-841, A380-842, and A380-861 with certain manufacturer serial numbers. The directive addresses an unsafe condition related to the Ram Air Turbine (RAT) gearbox, which may contain water leading to corrosion and potential failure of the RAT during flight. This AD mandates inspection and corrective actions to ensure continued safe operation of the affected RAT parts.

Airbus A380

EASA AD 2019-0127

Wings — Trailing Edge Flap Track #3 and #4 Supports — Modification

EASA Airworthiness Directive 2019-0127 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates modifications to the trailing edge flap track #3 and #4 supports on both left-hand and right-hand wings to address structural concerns. The directive applies to all serial numbers except those with Airbus modification 77208 incorporated in production.

Airbus A380

EASA AD RU-2019-322-04

Jun 4, 2019

Airworthiness / Maintenance Records Check

The Airworthiness Directive 2019-322-04 issued by the Federal Air Transport Agency of the Russian Federation mandates a one-time airworthiness inspection for RRJ-95 aircraft. This directive addresses the airworthiness and maintenance records of the RRJ-95 following an accident involving an RRJ-95B operated by Aeroflot. The directive includes a detailed inspection program covering aircraft documents, maintenance records, service life, executed works, emergency equipment, flight performance, and overall technical condition.