{"id":"F2006B09921","name":"AD/FA-200/1 - Battery Leads - Identification and Relocation","slug":"ad-fa-200-1-battery-leads-identification-and-relocation","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":55140,"registerId":"commonwealth-F2006B09921-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/FA-200/1 - Battery Leads - Identification and Relocation","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)  Fuji FA-200 Series Aeroplanes\n\n \n\nAD/FA-200/1 Battery Leads - Identification and Relocation NK\n\nApplicability: All models FA-200-160 and FA-200-180.\n\n \n\nRequirement: 1. Reposition the negative battery lead on FA200-160 aircraft so that it cannot be connected to the positive terminal.\n\n \n\n2. Clearly identify both the positive and negative lead terminals on FA200-160 and FA200-180 aircraft.\n\n \n\nCompliance: Within 100 hours time in service after 28 November 1968.\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\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":1388},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"The directive maintains its original narrow technical scope addressing a specific wiring safety defect in two aircraft models. There is no expansion beyond the original purpose of preventing battery misconnection hazards."},"complexity_factors":["Single-page instrument with only two operative requirements","No defined terms, interpretation sections, or legal jargon","Single, unconditional compliance deadline with no exceptions","No cross-references to other legislation or regulations","Clear applicability limited to two specific aircraft models"],"plain_english_summary":"This safety directive requires owners/operators of Fuji FA-200-160 and FA-200-180 aircraft to make two simple electrical safety fixes: relocate the FA-200-160 negative battery lead so it cannot reach the positive terminal, and clearly mark positive and negative battery terminals on both models. Compliance is required within 100 flight hours after 28 November 1968. The changes prevent reversed connections that can cause sparks, fires, electrical damage, or engine-start failures."}},"importantCases":[],"_links":{"self":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation","history":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation/history","analysis":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation/analysis","conflicts":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation/conflicts","importantCases":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation/important-cases","documents":"/api/acts/ad-fa-200-1-battery-leads-identification-and-relocation/documents"}}