{"id":"F2006B03688","name":"AD/BEECH 200/31 Amdt 1 - Elevator Control Horn Attachment","slug":"ad-beech-200-31-amdt-1-elevator-control-horn-attachment","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43278,"registerId":"commonwealth-F2006B03688-current","compilationNumber":null,"startDate":"2026-04-01","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 200/31 Amdt 1 - Elevator Control Horn Attachment","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\n![](image.001.png)  Beechcraft 200 (Super King Air) Series Aeroplanes\n\n \n\nAD/BEECH 200/31\n\nAmdt 1\n\n\nElevator Control Horn Attachment 5/81\n\n \n\nApplicability: All models 200 with S/Nos BB-3 to BB-674. All models 200C with S/Nos BL-1 to BL-8. All models 200T with S/Nos BT-1 to BT-16.\n\nRequirement: Action in accordance with Beechcraft SI No 1111 Rev 1.\n\n \n\nCompliance: Unless already accomplished, within 100 hours time in service after 31 May 1981.\n\n \n\nBackground:  The installation of additional rivets in the elevator control horn attachment has been found necessary under service conditions to prevent looseness developing in this control connection. This amendment adds additional aeroplanes and revises accomplishment instructions.\n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":1578},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":true,"description":"This amendment expands the original directive's coverage by adding more aircraft serial numbers to the applicability list and revising the accomplishment instructions compared to the original version."},"complexity_factors":["Single, specific mechanical requirement with no conditional exceptions","Short document with minimal defined terms (only aircraft model/serial ranges)","Relies on external technical manual (Beechcraft Service Instruction) for detailed procedures rather than complex legislative text","Simple compliance calculation (flight hours after fixed date)"],"plain_english_summary":"A mandatory airworthiness directive requiring owners/operators of certain Beechcraft Super King Airs (Model 200: BB‑3–BB‑674; 200C: BL‑1–BL‑8; 200T: BT‑1–BT‑16) to install additional rivets in the elevator control‑horn per Beechcraft Service Instruction No. 1111 Revision 1.  \n\nThis fixes a connection that can loosen in service and impair pitch control; work must be completed within 100 flight hours after 31 May 1981 if not already done."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment","history":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment/history","analysis":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment/analysis","conflicts":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment/conflicts","importantCases":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment/important-cases","documents":"/api/acts/ad-beech-200-31-amdt-1-elevator-control-horn-attachment/documents"}}