{"id":"F2006B03965","name":"AD/BEECH 55/14 - Centre Section Rear Spar Jack Pad","slug":"ad-beech-55-14-centre-section-rear-spar-jack-pad","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":43574,"registerId":"commonwealth-F2006B03965-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/BEECH 55/14 - Centre Section Rear Spar Jack Pad","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 55/14 Centre Section Rear Spar Jack Pad 5/69\n\nApplicability: Models 95-C55 and 95-D55 with S/Nos. TE-1 to TE-606. Requirement:  Action in accordance with Beechcraft SI No. 0064-067, Rev. 1.\n\nCompliance: Within 200 hours’ time in service or before 1 August 1969 whichever occurs first.\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":1391},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"This is a discrete, original airworthiness directive targeting a single mechanical component on specific aircraft models. No evidence of scope expansion beyond the original safety purpose."},"complexity_factors":["Single requirement with no exceptions or conditional logic","Minimal cross-referencing (only one external technical document)","Clear applicability limited to two specific aircraft models and defined serial number range","No defined terms, interpretation provisions, or penalty clauses","Approximately 40 words of substantive regulatory content"],"plain_english_summary":"**What this is:** A mandatory safety directive (called an Airworthiness Directive) issued by the Civil Aviation Safety Authority for specific Beechcraft Baron aircraft.\n\n**Who it affects:** Owners and operators of Beechcraft Baron models 95-C55 and 95-D55 with serial numbers TE-1 through TE-606.\n\n**What it requires:** These aircraft must undergo maintenance on the **centre section rear spar jack pad** — a reinforced structural point on the aircraft's main wing beam where jacks are placed to lift the plane. The work must strictly follow Beechcraft Service Instruction No. 0064-067, Revision 1.\n\n**Compliance deadline:** Within 200 hours of flight time or before 1 August 1969, whichever occurs first.\n\n**Why it matters:** Airworthiness Directives are legally enforceable safety orders. This addresses a specific structural integrity issue that could cause damage during routine jacking operations if left unaddressed."}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad","history":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad/history","analysis":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad/analysis","conflicts":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad/conflicts","importantCases":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad/important-cases","documents":"/api/acts/ad-beech-55-14-centre-section-rear-spar-jack-pad/documents"}}