{"id":"F2006B06648","name":"AD/ROCK-114/2A - Aileron Hinge Supports - Inspection","slug":"ad-rock-114-2a-aileron-hinge-supports-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":48568,"registerId":"commonwealth-F2006B06648-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/ROCK-114/2A - Aileron Hinge Supports - Inspection","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)  Gulfstream (Rockwell) 114 Series Aeroplanes\n\n \n\nAD/ROCK-114/2A Aileron Hinge Supports - Inspection 7/78\n\nApplicability: All model 114 aeroplanes with S/Nos. 14000 to 14376. Document:  Rockwell International SB No. SB-114-14A.\n\nCompliance: 1. Unless already accomplished as per SB No. 114-14, initially inspect before further flight as per Part 1 of SB No. 114-14A and perform external visual inspection before each subsequent flight until modified.\n\n \n\nNote: Pilot in command may perform and certify for visual inspection.\n\n \n\n2. Unless already accomplished as per SB No. 114-14 modify as per Part 2 of SB No. 114-14A within 100 hours time in service after 15 August 1978.\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":1643},"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"The directive maintains a tightly focused scope on the specific airworthiness issue (aileron hinge support integrity) for the specified aircraft models. Despite being a revision (indicated by the '2A' suffix), it does not expand beyond the original safety-critical inspection and modification requirements."},"complexity_factors":["Reliance on external technical documents (Rockwell Service Bulletin SB-114-14A) for procedural details","Specific serial number applicability limiting scope (S/Nos. 14000-14376)","Dual compliance tracks (ongoing inspections vs one-time modification)","Technical time-in-service metric ('100 hours time in service') requiring flight log calculations","Historical date-based compliance threshold ('after 15 August 1978')"],"plain_english_summary":"This airworthiness directive orders owners of Rockwell/Gulfstream 114 aircraft (S/N 14000–14376) to inspect aileron hinge supports immediately using Rockwell SB-114-14A and to have the pilot perform a visual hinge check before every flight until the permanent modification is done.\n\nThe permanent fix required by Part 2 of the Service Bulletin must be carried out within 100 flight hours after 15 August 1978 to prevent possible loss of control."}},"importantCases":[],"_links":{"self":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection","history":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection/history","analysis":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection/analysis","conflicts":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection/conflicts","importantCases":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection/important-cases","documents":"/api/acts/ad-rock-114-2a-aileron-hinge-supports-inspection/documents"}}