EASA AD 2022-0183
Fuselage — Belly Fairing Upper Wing Panel Fasteners — Inspection
Summary
EASA Airworthiness Directive 2022-0183 is an airworthiness directive issued for Airbus A350-1041 aeroplanes. It mandates inspection of the belly fairing upper wing panel fasteners, specifically on access panels 195DT, 196DT, 195ET, and 196ET, to ensure the integrity of fasteners and prevent potential in-flight detachment. The directive addresses a safety concern related to missing or inappropriate fasteners that could affect aircraft control.
What Changed
EASA Airworthiness Directive 2022-0183 introduces a new requirement for a one-time detailed inspection of the fasteners on specific belly fairing access panels of Airbus A350-1041 aircraft. It also requires corrective actions if defects are found and mandates contacting Airbus for further instructions when necessary. This directive does not supersede any previous ADs.
Why It Matters
This directive is critical for aviation professionals because it addresses a potential unsafe condition that could lead to in-flight detachment of belly fairing panels, risking damage and reduced control of the aircraft. Operators and maintenance organizations must ensure compliance to maintain airworthiness and safety. Failure to comply could result in operational restrictions or safety incidents.
What To Do
Operators of Airbus A350-1041 aeroplanes must perform a detailed inspection of the fasteners on affected belly fairing panels within 18 months of 13 September 2022. If any defects are found, corrective actions must be completed before the next flight. Additionally, if the service bulletin instructs to contact Airbus, operators must obtain and comply with approved instructions before further flight.
AI-generated summary from official EASA source document. Always verify against the original.