{"id":"F2006B06021","name":"AD/PA-46/14 Amdt 2 - Aileron Cable Routing","slug":"ad-pa-46-14-amdt-2-aileron-cable-routing","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":114419,"registerId":"commonwealth-F2006B06021-current","compilationNumber":null,"startDate":"2026-04-03","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/PA-46/14 Amdt 2 - Aileron Cable Routing","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)  \nPiper PA-46 (Malibu) Series Aeroplanes\n\nAD/PA-46/14\n\nAmdt 2\n\n  \nAileron Cable Routing 6/96\n\nApplicability: All Model PA-46-310P with serial numbers 46-8408001 through 46-8608067, and 4608001 through 4608066.\n\nRequirement: Action in accordance with Piper Service Bulletin 863A.\n\nCompliance: Unless already accomplished, within 100 hours time in service after 23 May 1996.\n\nThe compliance of the previous issue of this Directive is changed to reflect the alteration to applicability. This Amendment is effective from 23 May 1996.\n\nBackground: Reports were received of the aileron control cables chafing the flap track bracket.\n\nAmendment 1 required a modification to be incorporated.\n\nAmendment 2 is issued to align aircraft serial number applicability of this Directive with the Requirement Document.\n\nThe original issue of this AD became effective on 31 July 1987\\. Amendment 1 became effective on 20 April 1989.","sortOrder":0}],"analysis":{"kimi_summary":{"_metrics":{"model":"kimi-k2.5","source":"moonshot-batch","completionTokens":2081},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"Amendment 2 is administrative only, correcting the list of affected aircraft serial numbers to align with the referenced Piper Service Bulletin 863A. It does not expand the substantive safety requirement beyond the original issue addressing aileron cable chafing."},"complexity_factors":["Incorporates by reference an external technical document (Piper Service Bulletin 863A) without reproducing the actual repair instructions","Non-standard serial number formatting with two distinct alphanumeric ranges requiring careful cross-checking against aircraft logs","Conditional compliance clause ('Unless already accomplished') requiring record review"],"plain_english_summary":"Owners/operators of certain Piper PA-46-310P aircraft (serials 46-8408001–46-8608067 or 4608001–4608066) must reroute the aileron control cables per Piper Service Bulletin 863A to prevent chafing against a flap track bracket that could lead to cable failure and loss of control. If not already done, the work was required within 100 flight hours after 23 May 1996. Amendment 2 only corrects the serial-number applicability."}},"importantCases":[],"_links":{"self":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing","history":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing/history","analysis":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing/analysis","conflicts":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing/conflicts","importantCases":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing/important-cases","documents":"/api/acts/ad-pa-46-14-amdt-2-aileron-cable-routing/documents"}}