Doors – Cargo Door Locking Mechanism – Inspection
Superseded. A newer version replaces this document.
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of EC175 B helicopters must inspect the locking mechanisms of both cargo doors within specified flight hour limits—before exceeding 440 flight hours if under 330 flight hours accumulated, or within 110 flight hours after the effective date if 330 or more flight hours are accumulated. Inspections must then be repeated every 440 flight hours. Any detected deficiencies must be corrected before the next flight.
Summary
EASA Airworthiness Directive 2019-0255 is an airworthiness directive issued for Airbus Helicopters EC175 B helicopters. It mandates repetitive inspections of the locking mechanisms on both right-hand and left-hand cargo doors to ensure proper operation and prevent potential in-flight cargo door loss. The directive applies to all serial numbers of the EC175 B model.
What changed
This directive introduces mandatory repetitive inspections of the cargo door locking mechanisms on EC175 B helicopters following a reported incident where a cargo door handle was found open and the locking mechanism inoperative. It requires corrective actions if any deficiencies are found during inspections. This AD is an interim measure and may be followed by further actions.
Why it matters
This directive is critical for aviation professionals as it addresses a safety risk that could lead to loss of a cargo door in flight, potentially causing damage or reduced helicopter control. Operators and maintenance teams must ensure compliance to maintain aircraft airworthiness and safety. Failure to comply could result in unsafe flight conditions and regulatory penalties.
More for Airbus Helicopters EC175
All 73- EASA AD 2026-0179Tail Rotor – Tail Rotor Blade – Service Life Limit Amendment / ReplacementSep 18, 2026
- EASA PAD 26-090Tail Rotor – Tail Rotor Blade – Service Life Limit Amendment / ReplacementJul 24, 2026
- EASA AD 2026-0110[Correction] Fuselage – Screws and Nuts installed on Firewalls – InspectionJun 10, 2026
- EASA AD 2026-0039Time Limits / Maintenance Checks — Airworthiness Limitations Section — AmendmentFeb 27, 2026
- EASA PAD 26-026
Get the next one by email
New ADs and bulletins for Airbus Helicopters EC175 and Helicopters EC175 B, summarized like this page, every Monday.