{"id":"F2006B03882","name":"AD/BEECH 36/28 - Elevator Control Push Rods","slug":"ad-beech-36-28-elevator-control-push-rods","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43491,"registerId":"commonwealth-F2006B03882-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 36/28 - Elevator Control Push Rods","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 36 (Bonanza) Series Aeroplanes\n\n \n\nAD/BEECH 36/28 Elevator Control Push Rods 5/80\n\nApplicability: All models 36 and A36 with S/Nos. E-1 to E-1335. Requirement:  Action in accordance with Beechcraft SI No. 1019. Compliance:               Within 100 hours time in service after 31 May 1980.\n\nBackground: Corrosion has been found in the elevator pushrods of other models of Beech aircraft which have pushrods of similar manufacture.\n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":1630},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This is an original airworthiness directive issued to address a specific corrosion defect in defined aircraft models. The scope remains tightly focused on the original safety concern without expansion into unrelated operational areas."},"complexity_factors":["Single, unambiguous requirement referencing one external technical document","No defined terms, subsections, or nested conditional logic","Minimal cross-referencing (only to Beechcraft SI No. 1019)","Requires basic familiarity with aviation terminology ('time in service')"],"plain_english_summary":"**What this directive does**\nThis airworthiness directive mandates a safety inspection and repair for the elevator control push rods—the metal rods that transmit the pilot’s control inputs to the tail surfaces that make the aircraft climb or descend.\n\n**Who it affects**\nOwners and operators of Beechcraft 36 and A36 Bonanza aircraft with serial numbers E-1 through E-1335.\n\n**What you must do**\nCarry out the actions specified in Beechcraft Service Instruction No. 1019 to address corrosion (rust) in these push rods. This work must be completed within 100 hours of flight time accumulated after 31 May 1980.\n\n**Why it matters**\nCorrosion has been found in similar push rods on other Beechcraft models. If corrosion causes a push rod to fail, the pilot could lose control of the aircraft’s up-and-down movement, posing a serious crash risk."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-36-28-elevator-control-push-rods","history":"/api/acts/ad-beech-36-28-elevator-control-push-rods/history","analysis":"/api/acts/ad-beech-36-28-elevator-control-push-rods/analysis","conflicts":"/api/acts/ad-beech-36-28-elevator-control-push-rods/conflicts","importantCases":"/api/acts/ad-beech-36-28-elevator-control-push-rods/important-cases","documents":"/api/acts/ad-beech-36-28-elevator-control-push-rods/documents"}}