{"id":"F2006B05159","name":"AD/CESSNA 188/24 - Stub Wing Front and Rear Spars","slug":"ad-cessna-188-24-stub-wing-front-and-rear-spars","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":45270,"registerId":"commonwealth-F2006B05159-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/CESSNA 188/24 - Stub Wing Front and Rear Spars","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 188 (Agwagon) Series Aeroplanes\n\n \n\nAD/CESSNA 188/24 Stub Wing Front and Rear Spars 10/74\n\nApplicability: All models.\n\n \n\nRequirement: Action in accordance with Rex Aviation Ltd. Tech. Memo No. TM- 46, Issue 3. Compliance:               Within 100 hours time in service after 31 October 1974.\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":1968},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"The directive maintains its original narrow scope: a specific structural safety requirement for wing spars on a single aircraft model series. There is no indication of expansion beyond the original technical safety intent."},"complexity_factors":["Extremely short document (approximately 100 words of substantive content)","No defined terms or interpretation section","Single, unambiguous compliance requirement","No exceptions, conditions, or nested logic","Only one external reference (to a technical memorandum)"],"plain_english_summary":"Owners and operators of Cessna 188 “Agwagon” agricultural aircraft must inspect and, if necessary, repair the stub wing front and rear spars per Rex Aviation Technical Memo TM‑46, Issue 3. The mandatory work was to be completed within 100 flight hours after October 31, 1974.\n\nThis AD targets critical wing-to-fuselage structural members to prevent spar failure and potential wing separation during heavy, low-level agricultural operations."}},"importantCases":[],"_links":{"self":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars","history":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars/history","analysis":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars/analysis","conflicts":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars/conflicts","importantCases":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars/important-cases","documents":"/api/acts/ad-cessna-188-24-stub-wing-front-and-rear-spars/documents"}}