{"id":"F2006B04396","name":"AD/BELL 205/6 - Cyclic Control Supports - Inspection","slug":"ad-bell-205-6-cyclic-control-supports-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":44221,"registerId":"commonwealth-F2006B04396-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BELL 205/6 - Cyclic Control Supports - Inspection","content":"---\nmeta-content-style-type: text/css\nmeta-content-type: application/xhtml+xml; charset=utf-8\nmeta-generator: Aspose.Words for .NET 22.10.0\n---\n\n?xml version=\"1.0\" encoding=\"utf-8\" standalone=\"no\"?>\n\nCOMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\n \n\nBell Helicopter Textron 205 Series Helicopters\n\n \n\nAD/BELL 205/6 Cyclic Control Supports - Inspection 2/70 Applicability:              All 205A and 205A-1 models not modified to a standard acceptable to the Secretary. Document:               Bell SL No. 205A-43.\n\nCompliance: Within 100 hours time in service after 20 February 1970 and thereafter at intervals not exceeding 100 hours time in service.\n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":1658},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This directive maintains its original narrow scope mandating inspection of cyclic control supports for specific Bell helicopter models. There is no indication the scope has expanded beyond this original safety engineering purpose."},"complexity_factors":["Single mechanical component scope (cyclic control supports only)","Only one applicability condition (unmodified aircraft)","Simple recurring compliance interval (100 hours time in service)","Reference to only one external technical document","No cross-references to other legislation sections or nested conditional logic"],"plain_english_summary":"Owners/operators of Bell 205A and 205A‑1 helicopters (unless modified to approved standards) must perform recurring inspections of the cyclic control supports to detect wear or cracks. The first check is within 100 flight hours after 20 February 1970 and then every 100 hours, using the procedures in Bell Service Letter No. 205A‑43. This prevents loss of control from failed control‑stick supports."}},"importantCases":[],"_links":{"self":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection","history":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection/history","analysis":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection/analysis","conflicts":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection/conflicts","importantCases":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection/important-cases","documents":"/api/acts/ad-bell-205-6-cyclic-control-supports-inspection/documents"}}