{"id":"F2006B11048","name":"AD/L.40/7 Amdt 1 - Landing Gear Aural Warning - Modification","slug":"ad-l-40-7-amdt-1-landing-gear-aural-warning-modification","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":56667,"registerId":"commonwealth-F2006B11048-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/L.40/7 Amdt 1 - Landing Gear Aural Warning - 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)  Meta Sokol L.40 Series Aeroplanes\n\n \n\nAD/L.40/7\n\nAmdt 1\n\n\nLanding Gear Aural Warning - Modification 11/67\n\n \n\nApplicability: All models.\n\n \n\nRequirement: Relocate the landing gear aural warning switch so that the aural warning device can only be silenced when the landing gear retract levers are locked in the overcentre position.\n\n \n\nCompliance: Before 1 July 1968.\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\n \n\n \n\n \n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":2498},"content_quality":"ok","complexity_score":1,"scope_assessment":{"changed":false,"description":"As Amendment 1 to an existing directive, the scope remains narrowly focused on the specific landing gear aural warning modification for Meta Sokol L.40 aircraft. There is no indication of expansion beyond the original technical safety requirement."},"complexity_factors":["Single, specific mechanical requirement with no sub-conditions","No interpretation section or defined terms","Straightforward applicability applying to all models of a single aircraft type","No cross-references to other legislation or nested exceptions"],"plain_english_summary":"**What this is:** An Airworthiness Directive (a mandatory safety order) issued under the Civil Aviation Regulations requiring owners of Meta Sokol L.40 aircraft to modify their landing gear warning system.\n\n**Who it affects:** All models of Meta Sokol L.40 Series Aeroplanes.\n\n**What it requires:** The landing gear aural warning switch must be relocated so that pilots can only silence the alarm when the landing gear levers are fully retracted and locked in the overcentre position (the locked-away position).\n\n**Why it matters:** This prevents pilots from accidentally turning off the warning sound when the landing gear is not properly stowed, reducing the risk of flying or landing with the gear in an unsafe position.\n\n**Compliance deadline:** Before 1 July 1968."}},"importantCases":[],"_links":{"self":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification","history":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification/history","analysis":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification/analysis","conflicts":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification/conflicts","importantCases":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification/important-cases","documents":"/api/acts/ad-l-40-7-amdt-1-landing-gear-aural-warning-modification/documents"}}