EASA AD 26-123
Fuselage – Forward Fuselage Skin Panels – Inspection
EASA Airworthiness Directive PAD No. 26-123 is a proposed directive addressing inspection requirements for forward fuselage skin panels on Airbus A319, A320, and A321 aircraft models. It applies to specific serial numbers and panel part numbers identified in the directive. The directive focuses on detecting potential structural integrity issues caused by production quality deviations and certain repair conditions affecting the fuselage panels.
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319Airbus A319-153NAirbus A320Airbus A320-251NAirbus A320-252NAirbus A320-271NAirbus A321Airbus A321-251NXAirbus A321-252NXAirbus A321-271NXAirbus A321-272NX