{"id":"F2006B05212","name":"AD/CESSNA 205/8 Amdt 1 - Aileron Mass Balance Weight Attachment Rivets","slug":"ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":45450,"registerId":"commonwealth-F2006B05212-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/CESSNA 205/8 Amdt 1 - Aileron Mass Balance Weight Attachment Rivets","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 205 (210-5) Series Aeroplanes\n\n \n\nAD/CESSNA 205/8\n\nAmdt 1\n\nApplicability: All models.\n\n\nAileron Mass Balance Weight Attachment Rivets\n\n\n9/72\n\n \n\nRequirement: Inspect the rivets attaching the lower aileron skin to the balance weight for corrosion.\n\nWhere corrosion is suspected under the rivet heads attempts should be made to remove the rivet heads by a light sharp sideways blow with a screwdriver. All damaged or corroded rivets must be replaced.\n\n \n\nCompliance: Within 100 hours time in service after 29 September 1972 and thereafter at intervals not exceeding 100 hours time in service.\n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":3212},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"The amendment maintains the original targeted scope of ensuring structural integrity of aileron components through periodic inspection, without expanding into new operational areas or aircraft systems."},"complexity_factors":["Single maintenance task with no nested exceptions or conditional logic","Zero defined terms within the instrument text","No cross-references to other legislative provisions in the operative clauses","Simple periodic compliance framework based solely on flight hours"],"plain_english_summary":"This AD requires owners/operators of Cessna 205 (210-5) series aircraft to inspect for corrosion under the rivet heads that secure the aileron balance weight to the lower aileron skin. Suspect rivets must be lightly tapped to check for looseness and replaced if corroded or damaged. Inspections are required within 100 flight hours after 29 Sept 1972 and every 100 hours thereafter. It prevents balance-weight detachment that could impair roll control."}},"importantCases":[],"_links":{"self":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets","history":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets/history","analysis":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets/analysis","conflicts":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets/conflicts","importantCases":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets/important-cases","documents":"/api/acts/ad-cessna-205-8-amdt-1-aileron-mass-balance-weight-attachment-rivets/documents"}}