Equipment/Furnishings — Overhead Stowage Compartment — Handle Rod Disconnected
- Published
- Effective
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of affected ACLP BD-500-1A10 and BD-500-1A11 aircraft must install retaining clips on the latch rod assemblies of overhead stowage compartments containing emergency equipment. This must be done in accordance with ACLP Service Bulletin BD500-252065 Issue 001 or later approved revisions. Compliance is required within 9350 flight hours from the effective date of 19 February 2026.
Summary
EASA Airworthiness Directive CF-2026-08 is a regulatory document addressing a safety issue in Airbus Canada Limited Partnership (ACLP) aircraft models BD-500-1A10 and BD-500-1A11. The directive focuses on the overhead stowage compartments where the handle rod may become disconnected, potentially preventing access to emergency equipment. This AD applies to specific serial numbers of these aircraft models and mandates corrective action to ensure safety.
What changed
This new Airworthiness Directive introduces a requirement to install retaining clips on the latch rod assemblies of overhead stowage compartments containing emergency equipment. The change addresses the issue where the latch rod is not long enough to maintain engagement, which can cause the compartment to jam. The retaining clips provide positive retention to prevent the rod from disengaging from the handle or latch mechanism.
Why it matters
This directive is critical for aviation professionals because it ensures reliable access to emergency equipment stored in overhead compartments. Failure to comply could result in compartments jamming and emergency equipment being inaccessible during critical situations. Operators, maintenance organizations, and compliance teams must address this to maintain aircraft airworthiness and passenger safety.
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- EASA AD CF-2026-45Wings – Discrepant Fasteners at Wing to Fuselage Joint - AmendmentSep 11, 2026
- EASA AD CF-2026-40Time Limits/Maintenance Checks – New and Revised Airworthiness Limitations TasksSep 2, 2026
- EASA AD CF-2026-36Fuselage – Skin Assembly – Discrepant Fasteners at Air Data System Probe Doubler - Replacement
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