{"id":"F2006B10397","name":"AD/HS 125/119 Amdt 1 - MLG Torque Links","slug":"ad-hs-125-119-amdt-1-mlg-torque-links","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":116057,"registerId":"commonwealth-F2006B10397-current","compilationNumber":null,"startDate":"2026-04-03","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/HS 125/119 Amdt 1 - MLG Torque Links","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)  British Aerospace BAe 125 Series Aeroplanes\n\n \n\n# AD/HS 125/119\n\nAmdt 1\n\nApplicability: Series 800A and 800B.\n\n# MLG Torque Links 5/98\n\n \n\nRequirement: Action in accordance with Mandatory BAe SB 32-226-3257A.\n\n \n\nNote: UK CAA AD 002-05-91 refers.\n\n \n\nCompliance: As specified in the requirement document.\n\n \n\nThe compliance of the original issue of this directive remains unchanged. This amendment becomes effective on 23 April 1998.\n\nBackground:  This Directive requires a modification which will improve torque link resistance to vibration.\n\n \n\nAmendment 1 is issued to re-instate this directive to the series.\n\n \n\nThe original issue of this Airworthiness Directive became effective on 8 August 1991.\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":1322},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"Amendment 1 simply re-instates the directive to the active series without altering the technical requirements, aircraft applicability, or compliance actions from the original 1991 issue."},"complexity_factors":["Requires compliance with an external manufacturer document (Mandatory BAe SB 32-226-3257A) not reproduced in the directive itself","Specific and narrow applicability limited to two aircraft sub-models (BAe 125 Series 800A and 800B)","References UK CAA foreign airworthiness directive for additional context"],"plain_english_summary":"This is a safety rule for specific aircraft owners and operators. **What it does:** Requires a mandatory modification to the Main Landing Gear (MLG) torque links on British Aerospace BAe 125 Series 800A and 800B aeroplanes. Torque links are mechanical components that keep landing gear wheels properly aligned during flight. **Who it affects:** Anyone who owns, operates, or maintains these specific aircraft models. **What you must do:** Carry out the modification exactly as described in British Aerospace Service Bulletin 32-226-3257A (a technical manual from the manufacturer) to improve how the torque links handle vibration. **Why it exists:** To prevent potential failures or damage caused by vibration in the landing gear system, ensuring the aircraft remains safe to fly."}},"importantCases":[],"_links":{"self":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links","history":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links/history","analysis":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links/analysis","conflicts":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links/conflicts","importantCases":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links/important-cases","documents":"/api/acts/ad-hs-125-119-amdt-1-mlg-torque-links/documents"}}