{"id":"F2006B04007","name":"AD/BEECH 55/63 Amdt 1 - Elevators","slug":"ad-beech-55-63-amdt-1-elevators","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43616,"registerId":"commonwealth-F2006B04007-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 55/63 Amdt 1 - Elevators","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)  Beechcraft 55, 58 and 95-55 (Baron) Series Aeroplanes\n\n \n\nAD/BEECH 55/63\n\nAmdt 1\n\n\nElevators 12/84\n\n \n\nApplicability: All models with S/Nos referenced in Beechcraft Service Bulletin No. 2030. Requirement:               Action in accordance with Beechcraft S.B. No. 2030.\n\nCompliance: Unless already accomplished in accordance with Beechcraft SI No. 1207, within 100 hours’ time in service after 31 December 1984.\n\nBackground:  Elevators on certain aeroplanes or aeroplanes fitted with replacement elevators may have improperly bonded honeycomb stiffener strips installed. S.B. No. 2030 extends compliance to other models, corrects part number errors and supersedes and cancels Service Instruction No. 1207.\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":2462},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":true,"description":"This amendment expands the original directive's applicability to include additional Beechcraft models not covered in the initial version, corrects part number errors in the referenced technical documentation, and formally supersedes the previous Service Instruction No. 1207."},"complexity_factors":["Requires reference to external technical document (Beechcraft Service Bulletin No. 2030) not contained within the instrument","Conditional compliance exemption ('unless already accomplished')","Applicability depends on cross-referencing aircraft serial numbers against manufacturer documentation","Technical aviation terminology requiring specialized knowledge ('time in service', 'honeycomb stiffener strips', 'elevators')"],"plain_english_summary":"This Airworthiness Directive requires owners/operators of specified Beechcraft 55, 58 and 95-55 (Baron) serials to inspect and repair elevator honeycomb stiffener bonding per Beechcraft Service Bulletin No. 2030 within 100 flight hours after 31 Dec 1984. The fixation addresses a potential weakening that could lead to loss of control. It expands coverage, corrects part-number errors from earlier guidance, and formally replaces Service Instruction No. 1207."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-55-63-amdt-1-elevators","history":"/api/acts/ad-beech-55-63-amdt-1-elevators/history","analysis":"/api/acts/ad-beech-55-63-amdt-1-elevators/analysis","conflicts":"/api/acts/ad-beech-55-63-amdt-1-elevators/conflicts","importantCases":"/api/acts/ad-beech-55-63-amdt-1-elevators/important-cases","documents":"/api/acts/ad-beech-55-63-amdt-1-elevators/documents"}}