{"id":"F2006B05143","name":"AD/CESSNA 185/9 Amdt 1 - Rudder Bellcrank Bracket","slug":"ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":45216,"registerId":"commonwealth-F2006B05143-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/CESSNA 185/9 Amdt 1 - Rudder Bellcrank Bracket","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)  Cessna 185 Series Aeroplanes\n\n \n\nAD/CESSNA 185/9\n\nAmdt 1\n\n\nRudder Bellcrank Bracket 5/95\n\n \n\nApplicability: All models fitted with rudder bellcrank bracket P/N 0712309-4. Requirement:  Inspect rudder bellcrank bracket top edge for cracks.\n\nCompliance: Within 100 hours time in service after the last inspection completed in accordance with the initial issue of this Directive, thereafter at intervals not exceeding 100 hours time in service.\n\n \n\nThe effective date for the initial issue of this Directive was 31 December 1964. This amendment is effective 27 April 1995.\n\nBackground: Amendment 1 is issued to reflect the aircraft model changes and manufacturers production modifications since 1964.\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":1186},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This amendment maintains the original 1964 safety inspection scope. It merely updates the applicability section to reflect current aircraft models and production modifications, without expanding the directive's reach beyond the rudder bellcrank bracket inspection."},"complexity_factors":["Single specific component identified by exact part number (P/N 0712309-4)","Uniform compliance interval with no exceptions (100 hours time in service)","Single inspection method (visual check for cracks)","No conditional provisions, exemptions, or nested requirements","Extremely short length (single page, one operative requirement)"],"plain_english_summary":"This AD requires owners/operators of Cessna 185 aircraft fitted with rudder bellcrank bracket P/N 0712309-4 to inspect the bracket’s top edge for cracks. Initial inspection is within 100 flight hours (counting from the last 1964-rule inspection) and must be repeated every 100 hours. It prevents rudder failure and potential loss of control."}},"importantCases":[],"_links":{"self":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket","history":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket/history","analysis":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket/analysis","conflicts":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket/conflicts","importantCases":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket/important-cases","documents":"/api/acts/ad-cessna-185-9-amdt-1-rudder-bellcrank-bracket/documents"}}