{"id":"F2006B10857","name":"AD/INST/7 - H14 Automatic Pilot Servo Housing - Inspection","slug":"ad-inst-7-h14-automatic-pilot-servo-housing-inspection","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"repealed","isInForce":false,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":56353,"registerId":"commonwealth-F2006B10857-current","compilationNumber":null,"startDate":"2026-04-02","status":"Repealed","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/INST/7 - H14 Automatic Pilot Servo Housing - 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 - 107 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\n \n\n![](image.001.png)  Instruments and Automatic Pilots\n\n \n\nAD/INST/7 H14 Automatic Pilot Servo Housing - Inspection 1/71\n\nApplicability: All H14 Automatic Pilots (either King or Honeywell).\n\n \n\nRequirement: Inspect the linkage end of pneumatic housing (cylinder), King P/No. 047-2105-00 or Honeywell P/No. 314259, to ensure that no cracking has occurred in the wall of the housing in the areas adjacent to the formed retaining lugs. On servo assemblies which are installed on aircraft it will be sufficient to inspect the lugs on the side nearest to the cable drum only if it is not possible to inspect the remaining lugs without removing the servo from the aircraft.\n\n \n\nCompliance: Within 100 hours time in service after 26 February 1971.\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":1776},"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"The directive maintains its original narrow scope: a specific one-time inspection requirement for a particular autopilot servo housing model. No expansion of applicability or additional requirements have been added."},"complexity_factors":["Technical aviation terminology (servo housing, pneumatic cylinder, cable drum, retaining lugs)","Specific manufacturer part numbers (King P/No. 047-2105-00, Honeywell P/No. 314259)","Single conditional inspection exemption for installed assemblies"],"plain_english_summary":"This rule requires owners and operators of aircraft fitted with King or Honeywell H14 automatic pilot systems to inspect the autopilot servo’s pneumatic housing at the linkage/retaining-lug area for cracks. Inspections had to be completed within 100 flight hours after 26 February 1971. Detecting cracks is critical because a failed housing can cause unexpected autopilot loss and potential loss of control."}},"importantCases":[],"_links":{"self":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection","history":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection/history","analysis":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection/analysis","conflicts":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection/conflicts","importantCases":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection/important-cases","documents":"/api/acts/ad-inst-7-h14-automatic-pilot-servo-housing-inspection/documents"}}