{"id":"F2006B08187","name":"AD/CESSNA 310/8 - Main Landing Gear Side Brace Link - Inspection","slug":"ad-cessna-310-8-main-landing-gear-side-brace-link-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":115394,"registerId":"commonwealth-F2006B08187-current","compilationNumber":null,"startDate":"2026-04-03","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/CESSNA 310/8 - Main Landing Gear Side Brace Link - 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)  Cessna 310 Series Aeroplanes\n\n \n\nAD/CESSNA 310/8 Main Landing Gear Side NK\n\nBrace Link - Inspection Applicability: All model 310 and 310B prior to S/No. 35550 fitted with early style link. Document:              Cessna SL No. 310-34.\n\nCompliance: At intervals not exceeding 100 hours time in service.\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":1798},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"The directive maintains its original narrow technical scope. It addresses only the specific airworthiness issue of main landing gear side brace link integrity on early-model Cessna 310 aircraft, without expansion into broader operational or maintenance requirements."},"complexity_factors":["Single operative requirement (inspection only)","No definitions section or interpretation provisions","Narrow applicability limited to specific aircraft models and serial number ranges","Simple periodic compliance trigger (100 hours time in service) with no conditional exceptions","No cross-references to other legislative instruments beyond the enabling regulations"],"plain_english_summary":"This AD mandates recurring inspections of the main landing gear side brace link on Cessna 310/310B aircraft (serial numbers below 35550 fitted with the early-style link). Owners and operators must inspect the link every 100 hours’ time-in-service using the procedures in Cessna Service Letter No. 310-34.  \n\nThe requirement reduces the risk of side brace failure and potential landing gear collapse during takeoff or landing, protecting aircraft integrity and occupant safety."}},"importantCases":[],"_links":{"self":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection","history":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection/history","analysis":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection/analysis","conflicts":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection/conflicts","importantCases":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection/important-cases","documents":"/api/acts/ad-cessna-310-8-main-landing-gear-side-brace-link-inspection/documents"}}