{"id":"F2006B04132","name":"AD/BEECH 65/35 Amdt 1 - Port Inner Wing Electrical Wiring","slug":"ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43840,"registerId":"commonwealth-F2006B04132-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 65/35 Amdt 1 - Port Inner Wing Electrical Wiring","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 65/35\n\nAmdt 1\n\n\nPort Inner Wing Electrical Wiring 3/89\n\n \n\nApplicability: All models Queen Air 65 and 70.\n\n \n\nRequirement: 1. Inspect electrical loom in port inner wing for chafing where the loom passes stiffener LH P/No. 50-120006-6 (See Beechcraft A65, 70 and B80 parts catalogue Figure 66).\n\n \n\n2. Support loom to avoid further chafing.\n\n \n\nCompliance: Within 100 hours’ time in service after 28 February 1973.\n\n \n\nBackground: Amendment 1 includes model 70 in applicability and consolidates Queen Air series 65 and 70 aircraft.\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":1523},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":true,"description":"Amendment 1 expanded the applicability from the original Model 65 only to include Model 70 aircraft, consolidating both Queen Air series variants under a single directive."},"complexity_factors":["Extremely short text (under 150 words)","Single, specific technical requirement with only two sub-steps","Minimal defined terms (only aircraft models and one part number reference)","Simple compliance trigger (100 hours 'time in service' after fixed date)","No nested conditional logic or cross-references to other legislative provisions"],"plain_english_summary":"**What it does:** This directive mandates a safety inspection for specific Beechcraft aircraft to prevent electrical failures.\n\n**Who it affects:** Owners and operators of Beechcraft Queen Air Model 65 and Model 70 series aeroplanes.\n\n**What must be done:**\n1. **Inspect** the electrical wiring bundle (called a \"loom\") located in the left (port) inner wing for damage caused by rubbing (chafing) where it passes a specific metal support bracket (stiffener part number 50-120006-6).\n2. **Secure** the wiring to prevent future rubbing against the aircraft structure.\n\n**Deadline:** The work must be completed within 100 hours of flight time after 28 February 1973.\n\n**Why it matters:** Chafing can damage electrical insulation, potentially causing short circuits, electrical system failures, or fire hazards. The amendment updates the original directive to include Model 70 aircraft, ensuring both variants meet the same safety standard."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring","history":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring/history","analysis":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring/analysis","conflicts":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring/conflicts","importantCases":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring/important-cases","documents":"/api/acts/ad-beech-65-35-amdt-1-port-inner-wing-electrical-wiring/documents"}}