{"id":"F2006L00747","name":"AD/F2000/9 - Engine Fuel System","slug":"ad-f2000-9-engine-fuel-system","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":136770,"registerId":"commonwealth-F2006L00747-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Dassault Aviation Falcon 2000 Series Aer","sectionType":"division","heading":"Dassault Aviation Falcon 2000 Series Aeroplanes","content":"### Dassault Aviation Falcon 2000 Series Aeroplanes\n\n| AD/F2000/9 | Engine Fuel System | 4/2006 |\n| ---------- | ------------------ | ------ |\n\n| Applicability: | Falcon 2000 aircraft which have not been modified under DASSAULT AVIATION Service Bulletin (SB) F2000-202 (modification of injectors of both engines in accordance with CFE Company Service Bulletin CFE738 F2000-2578).                                                                                                                               |\n| -------------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |\n| Requirement:   | 1. Add self-adhesive labels limiting use of fuel in compliance with SB F2000-080.2. Incorporate TC No. 34 supplement to the Falcon 2000 Flight Manual into the Aeroplane Flight Manual, and comply with its instructions.Embodiment of SB F2000-202 cancels the requirements of requirement 1 and 2 of this AD.Note: DGAC AD 1996-290-001(B)R1 refers. |\n| Compliance:    | Within 30 days after the effective date of this AD unless previously accomplished.                                                                                                                                                                                                                                                                     |\n|                | This Airworthiness Directive becomes effective on 13 April 2006.                                                                                                                                                                                                                                                                                       |\n| Background:    | This AD is issued in order to minimize the risks of flame-out of CFE 738-1-IS engines installed on Falcon 2000 in case of use of JP4, JET B and EMS 53113 fuel types.                                                                                                                                                                                  |\n\n![](image.001.png)  \nJames Coyne  \nDelegate of the Civil Aviation Safety Authority\n\n3 March 2006","sortOrder":0},{"sectionNumber":"AD/F2000/9","sectionType":"part","heading":"AD/F2000/9","content":"## AD/F2000/9","sortOrder":1},{"sectionNumber":"Engine Fuel System","sectionType":"part","heading":"Engine Fuel System","content":"## Engine Fuel System","sortOrder":2},{"sectionNumber":"4/2006","sectionType":"part","heading":"4/2006","content":"## 4/2006","sortOrder":3}],"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":2,"scope_assessment":{"changed":false,"description":"This is a standard single-issue airworthiness directive focused on a specific engine fuel system safety risk. It has not expanded beyond its original purpose of addressing flame-out risks with specific fuel types."},"complexity_factors":["Very short document (approximately 200 words)","Only 2 substantive requirements with a clear alternative compliance path (the SB F2000-202 modification)","Minimal defined terms (only standard aviation abbreviations like AD, SB, TC)","No nested conditional logic or cross-references to other legislation","Single applicability criterion based on modification status","Straightforward compliance deadline with single exception"],"plain_english_summary":"This AD requires owners/operators of Dassault Falcon 2000s (unless already modified per SB F2000‑202) to add fuel‑use warning labels and update the Flight Manual with a technical supplement to prevent CFE 738‑1‑IS engine flame‑outs when using JP4, JET B or EMS 53113. It mandates compliance within 30 days of 13 April 2006 (by 13 May 2006)."},"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":false,"description":"The AD targets unmodified Falcon 2000s as an interim mitigation against engine flame‑out risks from specified fuel types. Requirements are limited, time‑bound and are cancelled if SB F2000‑202 is embodied; the instrument does not expand scope beyond that safety purpose."},"complexity_factors":["Narrow applicability: only Falcon 2000 aircraft not modified under SB F2000‑202 are covered (Applicability).","Simple, discrete actions required: fitting labels and inserting an AFM supplement (Requirement).","Short compliance window creates operational scheduling pressure: 30 days (Compliance).","Conditional cancellation: embodying SB F2000‑202 cancels the AD requirements, creating a two‑path compliance model (Requirement).","Cross‑references to other service bulletins and an earlier DGAC AD increase document dependency (Requirement; Background).","Direct operational constraint on fuel types used (Background) with enforcement left to operator compliance and regulator oversight."],"plain_english_summary":"This airworthiness directive requires Falcon 2000 aeroplanes that have not been modified under SB F2000‑202 to add self‑adhesive fuel‑use limitation labels, incorporate a flight‑manual supplement and follow its instructions to reduce the risk of CFE 738‑1‑IS engine flame‑outs when JP4, JET B or EMS 53113 fuels are used (Requirement; Background). Operators must accomplish these actions within 30 days of the AD becoming effective (Compliance)."}},"importantCases":[],"_links":{"self":"/api/acts/ad-f2000-9-engine-fuel-system","history":"/api/acts/ad-f2000-9-engine-fuel-system/history","analysis":"/api/acts/ad-f2000-9-engine-fuel-system/analysis","conflicts":"/api/acts/ad-f2000-9-engine-fuel-system/conflicts","importantCases":"/api/acts/ad-f2000-9-engine-fuel-system/important-cases","documents":"/api/acts/ad-f2000-9-engine-fuel-system/documents"}}