EASA Regulations for Airbus A320-216

2 airworthiness directives and regulations affecting Airbus A320-216.

EASA AD 2023-0179

Fuselage — Cargo Door Frame Attachment Drillings — Inspection

EASA Airworthiness Directive 2023-0179 is an airworthiness directive addressing inspection requirements for the cargo door frame attachment drillings on Airbus A320-214, A320-216, A320-251N, A320-271N, and A321-253NX aeroplanes. It focuses on detecting and correcting oversized fastener holes in the fuselage skin panel assembly to maintain structural integrity. The directive provides detailed inspection and corrective action instructions based on Airbus Service Bulletins A320-53-1493 and A320-53-1494.

Oct 11, 2023

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321Airbus A320-214Airbus A320-216Airbus A320-251NAirbus A320-271NAirbus A321-253NX

EASA AD 2018-0155

Electrical and Electronic Common Installation — Harness Routing into Centre Wing Box — Modification

EASA Airworthiness Directive 2018-0155 is an official regulatory document addressing Airbus A320-214, A320-216, A320-232, and A320-233 aeroplanes that have incorporated Airbus modification 155636 but not modification 158379. This directive focuses on the electrical and electronic common installation, specifically the harness routing into the centre wing box. It mandates a modification to prevent potential safety hazards related to fuel tank ignition.

Jul 20, 2018

Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A320-214Airbus A320-216Airbus A320-232Airbus A320-233