{"id":"F2006B04165","name":"AD/BEECH 65/8 - Control Sub-Panel Shelf - Modification","slug":"ad-beech-65-8-control-sub-panel-shelf-modification","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43900,"registerId":"commonwealth-F2006B04165-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 65/8 - Control Sub-Panel Shelf - Modification","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 65 and 70 (Queen Air) Series Aeroplanes\n\n \n\nAD/BEECH 65/8 Control Sub-Panel Shelf - Modification 11/67\n\nApplicability: Model 65 S/Nos. LC-1 to LC-239. Models 65-80, 65-A80 & 65-B80 with S/Nos. LD- 1 to LD-318.\n\n \n\nDocument: Beechcraft SB 67-5.\n\n \n\nCompliance: Within 50 hours’ time in service after 24 May 1967.\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":1893},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This standalone Airworthiness Directive maintains its original narrow scope. It addresses only the specific safety modification to the control sub-panel shelf for the identified Beechcraft 65 series aircraft and has not expanded to cover additional aircraft types, components, or operational requirements."},"complexity_factors":["Single, unambiguous mechanical modification requirement","Narrow applicability limited to specific aircraft serial number ranges","Single external technical reference (Beechcraft SB 67-5)","No conditional exceptions, defined terms, or nested legal provisions"],"plain_english_summary":"**What this is:** An Airworthiness Directive (a mandatory safety order) issued by the Civil Aviation Safety Authority (CASA) requiring a specific mechanical modification to certain Beechcraft aircraft.\n\n**What it requires:** Owners or operators must modify the **control sub-panel shelf** (a structural component near the cockpit controls) according to the manufacturer's instructions in **Beechcraft Service Bulletin 67-5**.\n\n**Who it affects:** Only specific Beechcraft Queen Air aeroplanes:\n- Model 65 with serial numbers LC-1 to LC-239\n- Models 65-80, 65-A80, and 65-B80 with serial numbers LD-1 to LD-318\n\n**Deadline:** Within 50 hours of flight time after 24 May 1967.\n\n**Why it matters:** Airworthiness Directives are legally binding. Non-compliance grounds the aircraft—you cannot fly legally until the work is done."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification","history":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification/history","analysis":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification/analysis","conflicts":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification/conflicts","importantCases":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification/important-cases","documents":"/api/acts/ad-beech-65-8-control-sub-panel-shelf-modification/documents"}}