{"id":"F2006B06639","name":"AD/ROBIN/7 Amdt 2 - Nose Landing Gear Bracket","slug":"ad-robin-7-amdt-2-nose-landing-gear-bracket","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":48545,"registerId":"commonwealth-F2006B06639-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/ROBIN/7 Amdt 2 - Nose Landing Gear Bracket","content":"COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 \\- 105 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\n![](image.001.png)  \nRobin Aviation Series Aeroplanes\n\nAD/ROBIN/7\n\nAmdt 2\n\n  \nNose Landing Gear Bracket 7/93\n\nApplicability: Models listed in Avions Pierre Robin SB No. 101 Rev. 3. Requirement: Inspect in accordance with Avions Pierre Robin SB No. 101 Rev. 3.\n\nNote: DGAC AD 83-206(A)R3 Refers.\n\nCompliance: 1. If the width of the lower plate is 84mm: At the next 500hr Inspection, and thereafter at intervals not to exceed 500hrs time in service.\n\n2. If the width of the lower plate is less than 84mm: At the next 100 hr Inspection, and thereafter at intervals not to exceed 100hrs time in service. If a crack is found in the welding area; and the crack runs along the circumference and is less than 15mm long max. and/or a radial crack is less than 8mm long max, reinspect at intervals not to exceed 25hrs time in service until repaired or replaced.\n\nBackground: The Manufacturer reports cracking of the weld securing the nose wheel steering bracket to the nose landing gear leg. Amendment 1 was issued to align this directive to the revised Country of Origin AD which required a dye penetrant inspection and a variation to the compliance.\n\nAmendment 2 is issued in response to a revision of the Country of Origin AD which alters Applicability.","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":2313},"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":true,"description":"Amendment 2 explicitly alters the applicability of the directive, changing which specific aircraft models or configurations are covered compared to previous versions, in order to align with revised French aviation safety directives."},"complexity_factors":["Conditional compliance intervals based on physical measurement threshold (84mm plate width)","Nested secondary conditions for crack dimensions triggering accelerated 25-hour inspection intervals","External referencing to French manufacturer technical documents (Service Bulletin No. 101 Rev. 3 and DGAC AD 83-206(A)R3)","Amendment history affecting scope of applicability"],"plain_english_summary":"This directive requires owners/operators of specified Robin/Avions Pierre Robin aircraft to inspect the weld attaching the nose-wheel steering bracket to the nose landing gear, using the manufacturer’s Service Bulletin procedures. Inspection frequency depends on the lower plate width, and detected small cracks trigger 25‑flight‑hour re‑inspections until repair or replacement to prevent steering failure."}},"importantCases":[],"_links":{"self":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket","history":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket/history","analysis":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket/analysis","conflicts":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket/conflicts","importantCases":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket/important-cases","documents":"/api/acts/ad-robin-7-amdt-2-nose-landing-gear-bracket/documents"}}