{"id":"F2006B06617","name":"AD/ROBIN/2 - Flap Control Mechanism Dented Plate - Inspection","slug":"ad-robin-2-flap-control-mechanism-dented-plate-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":48473,"registerId":"commonwealth-F2006B06617-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/ROBIN/2 - Flap Control Mechanism Dented Plate - 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)  Robin Aviation Series Aeroplanes\n\n \n\nAD/ROBIN/2 Flap Control Mechanism Dented Plate - Inspection 8/81\n\nApplicability: All models R1000.\n\n \n\nDocument: Avions Pierre Robin SB No. 88.\n\n \n\nCompliance: Within 100 hours time in service after 31 August, 1981.\n\n \n\nBackground: The manufacturer advises that some cracks have been found around the axle of the flap control dented plate.\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":1886},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"This directive remains confined to its original 1981 scope: a specific one-time inspection requirement for cracks in the flap control dented plate on Robin R1000 aircraft. It has not expanded to cover additional components, aircraft models, or ongoing maintenance requirements."},"complexity_factors":["Addresses only one specific mechanical component on one aircraft model","No defined terms or interpretation section","Single compliance deadline with simple calculation (100 hours after fixed date)","No exceptions, exemptions, or conditional provisions","References only one external technical document"],"plain_english_summary":"**What this requires:** If you own or operate a Robin R1000 aircraft, you must inspect the flap control mechanism's \"dented plate\" for cracks around its axle.\n\n**Who must comply:** Owners and operators of all Robin R1000 model aeroplanes.\n\n**What you need to do:**\n- Follow the inspection instructions in Avions Pierre Robin Service Bulletin No. 88 (the manufacturer's technical guide)\n- Complete the inspection within 100 hours of flight time after 31 August 1981\n\n**Why it matters:** The manufacturer discovered cracks forming around the axle of this component. If left unchecked, this could compromise the safety and operation of the aircraft's flaps."}},"importantCases":[],"_links":{"self":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection","history":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection/history","analysis":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection/analysis","conflicts":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection/conflicts","importantCases":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection/important-cases","documents":"/api/acts/ad-robin-2-flap-control-mechanism-dented-plate-inspection/documents"}}