{"id":"F2006B11057","name":"AD/L200/7 - Main Undercarriage Breakstrut Hinges - Inspection","slug":"ad-l200-7-main-undercarriage-breakstrut-hinges-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":56683,"registerId":"commonwealth-F2006B11057-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/L200/7 - Main Undercarriage Breakstrut Hinges - 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\n![](image.001.png)  Morava L200 Series Aeroplanes\n\n \n\nAD/L200/7 Main Undercarriage Breakstrut Hinges - Inspection 11/78\n\nApplicability: All models.\n\n \n\nDocument: Omnipol SB No. L200/111.\n\n \n\nCompliance: Before issue of Certificate of Airworthiness.\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\n \n\n \n\n \n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":1589},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"This is a targeted safety directive addressing a specific mechanical component on a specific aircraft type. The scope remains exactly as intended—mandating inspection of undercarriage hinges prior to airworthiness certification."},"complexity_factors":["Single operational requirement with no exceptions or conditions","No defined terms or interpretation section","Only one external reference (to manufacturer Service Bulletin L200/111)","No procedural steps, delegation provisions, or penalty clauses"],"plain_english_summary":"This Airworthiness Directive mandates a safety inspection of the **main landing gear breakstrut hinges** on **Morava L200 series aircraft** (Czech-built aeroplanes).\n\n**What it requires:**\n- Operators must inspect the breakstrut hinges (critical components that help absorb landing forces) on the main undercarriage before the aircraft can be issued a Certificate of Airworthiness (the official document allowing it to fly legally).\n\n**Who it affects:**\n- Owners and operators of all Morava L200 model aircraft.\n\n**Why it matters:**\n- The directive addresses potential structural failures in the landing gear. The reference to \"Omnipol SB No. L200/111\" suggests this follows a manufacturer's Service Bulletin indicating possible defects that could cause landing gear collapse."}},"importantCases":[],"_links":{"self":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection","history":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection/history","analysis":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection/analysis","conflicts":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection/conflicts","importantCases":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection/important-cases","documents":"/api/acts/ad-l200-7-main-undercarriage-breakstrut-hinges-inspection/documents"}}