{"id":"F2006B07961","name":"Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-36 (Pawnee Brave) Series Aeroplanes","slug":"airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":115004,"registerId":"commonwealth-F2006B07961-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-36 (Pawnee Brave) Series Aeroplanes","content":"Airworthiness Directives 2004\n\nI, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety\n\nAuthority, acting under subregulation 39.001 (1) of the Civil\n\nAviation Safety Regulations 1998:\n\n(a) revoke the Airworthiness Directives mentioned in\n\nSchedule 1; and\n\n(b) make, as separate instruments, each Airworthiness\n\nDirective mentioned in Schedule 1 and attached.\n\n![](image.001.png)\n\nDavid Villiers\n\nDelegate of the Civil Aviation Safety Authority\n\n20 December 2004\n\nNote: Each attached Airworthiness Directive is being re-made in exactly the\n\nsame form as appears in the latest published edition of the Directive.\n\n  \nSchedule 1 Revocation and Remaking of\n\nAirworthiness Directives\n\nPiper PA-36 (Pawnee Brave) Series Aeroplanes\n\nAD Name AD Number\n\nWing Spar Centre Section Bolts - Replacement AD/PA-36/1\n\nStall Warning Detector - Relocation AD/PA-36/2\n\nPilot Seat Restraint Installation - Modification AD/PA-36/3\n\nFlap Control - Modification AD/PA-36/4\n\nPre-Certification Requirements - Modifications AD/PA-36/5 Amdt 1\n\nWing Structural Fatigue Limitations AD/PA-36/6 Amdt 3\n\nWing Main Spar Centre Section - Modification AD/PA-36/7\n\nForward and Aft Wing Attachment Fittings - Inspection and Modification AD/PA-36/8\n\nControl System Torque Tube Front Bearing Plate Attachment Bolt - Inspection AD/PA-36/9\n\nSpray Pump Windmill - Modification AD/PA-36/10\n\nMuffler Clamp - Installation AD/PA-36/11\n\nWing Main Spar Lower Attachment Bolt - Retirement Life - CANCELLED AD/PA-36/12\n\nFuel Tank Vent - Inspection AD/PA-36/13\n\nRudder Control Horn Attachment Bolts - Inspection and Modification AD/PA-36/14 Amdt 1\n\nTail Wheel Assembly - Modification AD/PA-36/15 Amdt 1\n\nControl Rod End Bearings - Replacement AD/PA-36/16\n\nRudder Spar - Inspection AD/PA-36/17\n\nWing Main Spar Carry Through Assembly - Inspection AD/PA-36/18\n\nElevator and Aileron System Control Rod End Bearings - Inspection and AD/PA-36/19 Amdt 1\n\nEngine Mount Attach Brackets - Inspection and Modification AD/PA-36/20 Amdt 1\n\nRudder Cable and Seat Belt Attachment Shackles - Inspection AD/PA-36/21\n\nForward Fuselage Tubes AD/PA-36/22\n\nAircraft Repair AD/PA-36/23","sortOrder":0}],"analysis":{"flash_summary_failed":{"failed":true,"reason":"Unauthenticated. Configure AI_GATEWAY_API_KEY or use a provider module. Learn more: https://ai-sdk.dev/unauthenticated-ai-gateway","source":"analysis-cron"},"kimi_summary":{"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"This instrument performs a pure consolidation/reformatting function. The scope remains exactly as originally intended: maintaining airworthiness standards for Piper PA-36 aircraft. There is no expansion of regulatory reach — the document explicitly states each AD is being re-made 'in exactly the same form' as previously published."},"complexity_factors":["Very short document (under 2 pages)","Only 1 defined term implicitly used (subregulation 39.001(1) reference)","Simple binary structure: revocation list + reissuance list","No conditional logic or nested exceptions — just a straightforward table of 23 items","No cross-references to other legislation beyond the enabling regulation (CASR 1998)","Content is purely administrative — the actual technical complexity sits in the attached ADs, not this instrument itself"],"plain_english_summary":"This CASA order cancels and reissues 23 airworthiness directives for the Piper PA‑36 (Pawnee Brave), replacing each former AD with a new, separate legal instrument while keeping their content unchanged. It affects Pawnee Brave owners, operators and maintenance engineers.\n\nIt’s a technical housekeeping step to preserve enforceability and administrative clarity without altering any safety requirements."},"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":false,"description":"The instrument does not change substantive scope. It expressly revokes the listed ADs and re-issues them \"in exactly the same form\" as their latest published editions, preserving existing requirements (see operative recital citing subregulation 39.001(1) and the Note)."},"complexity_factors":["Legal mechanism is a simple revoke-and-remake using delegated power under subregulation 39.001(1) (explicit in the instrument).","Large list of 23 distinct ADs across structural, control, engine and equipment issues (Schedule 1), which disperses operational compliance obligations.","Some ADs show amendments and one entry is noted as CANCELLED (AD/PA-36/12), requiring cross-referencing to current amendment status.","Instrument relies on attached AD texts being the \"latest published edition\" and re-made \"in exactly the same form\", creating a technical attachment/enclosure dependency.","Single decision point: instrument executed by the CASA delegate (David Alan Villiers), concentrating administrative discretion over form and timing.","Compliance burden is borne by aircraft owners/operators/maintainers who must follow the re-made ADs; administrative costs arise from ensuring conformity to each separate instrument."],"plain_english_summary":"This instrument revokes a list of Airworthiness Directives (ADs) for Piper PA-36 (Pawnee Brave) aeroplanes and re‑issues each AD as a separate instrument in the same form as its latest published edition. It is made by a CASA delegate under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The change preserves existing inspection, modification and compliance requirements for owners, operators and maintainers of the Piper PA-36 series, who remain responsible for meeting the re‑made ADs."}},"importantCases":[],"_links":{"self":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes","history":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes/history","analysis":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes/analysis","conflicts":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes/conflicts","importantCases":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes/important-cases","documents":"/api/acts/airworthiness-directives-2004-revocation-and-remaking-piper-pa-36-pawnee-brave-series-aeroplanes/documents"}}