{"id":"F2006B06637","name":"AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement","slug":"ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":48538,"registerId":"commonwealth-F2006B06637-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/ROBIN/4 - Aileron/Flap Support Brackets - Inspection and Reinforcement","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/4 Aileron/Flap Support Brackets - Inspection\n\nand Reinforcement\n\n\n10/82\n\n \n\nApplicability: All model R2000.\n\n \n\nDocument: Avions Pierre Robin SB No. 90.\n\n \n\nCompliance: Within 100 hours time in service after 31 October, 1982.\n\n \n\nBackground: The Manufacturer has reported cracking adjacent to the attachment points of the left and right aileron/flap common support brackets and corresponding wing skin areas.\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":1996},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This directive remains precisely targeted at its original purpose: addressing a specific safety defect (cracking in aileron/flap support brackets) on Robin R2000 aircraft. The scope has not expanded beyond this singular technical airworthiness issue."},"complexity_factors":["Single, specific technical requirement affecting only one aircraft component","Simple applicability criteria limited to one specific aircraft model series","Straightforward compliance deadline based on accumulated flight hours","Relies on external manufacturer technical document rather than incorporating detailed engineering procedures","No exemptions, exceptions, or conditional provisions requiring legal interpretation"],"plain_english_summary":"This Airworthiness Directive requires owners/operators of Robin R2000 aircraft to inspect and, if needed, reinforce the metal brackets attaching the ailerons and flaps to the wings per Manufacturer Service Bulletin No. 90.  \n\nInspections and any reinforcement must be completed within 100 flight hours after 31 October 1982 to address bracket cracking that could lead to control-surface failure and potential loss of aircraft control."}},"importantCases":[],"_links":{"self":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement","history":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement/history","analysis":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement/analysis","conflicts":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement/conflicts","importantCases":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement/important-cases","documents":"/api/acts/ad-robin-4-aileron-flap-support-brackets-inspection-and-reinforcement/documents"}}