{"id":"F2006L02196","name":"AD/F2000/19 - Overwing Emergency Exit","slug":"ad-f2000-19-overwing-emergency-exit","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":117525,"registerId":"commonwealth-F2006L02196-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/F2000/19 | Overwing Emergency Exit | 8/2006 |\n| ----------- | ----------------------- | ------ |\n\n| Applicability: | All Falcon 2000 aircraft for which the Aircraft Maintenance Manual (AMM) Airworthiness Limitation Section, Chapter 5-40, is not at Revision 11 or above.All Falcon 2000EX aircraft for which AMM Chapter 5-40 is not at Revision 02 or above.All Falcon 2000EX EASy aircraft for which AMM Chapter 5-40 is not at Revision 02 or above.                                             |\n| -------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n| Requirement:   | Insert a copy of EASA AD 2006-0148 in Chapter 5-40 of the Aircraft Maintenance Manual.Note: Updating Chapter 5-40 with its appropriate revision; Revision 11 for Falcon 2000, Revision 02 for Falcon 2000EX, and Revision 02 for Falcon 2000EX EASy aircraft, terminates the requirement of this Directive, upon which the copy of this Directive may then be removed from the AMM. |\n| Compliance:    | Within 30 days after 3 August 2006.                                                                                                                                                                                                                                                                                                                                                 |\n|                | This Airworthiness Directive becomes effective on 3 August 2006.                                                                                                                                                                                                                                                                                                                    |\n| Background:    | During an attempted operation of a Falcon 50 emergency exit, interference was reported between interior trim and the exit. This Directive is issued in response to a new EASA AD (superseding DGAC AD 1999-210-009(B)), which extends the repetitive overwing emergency exit opening test interval to 24 months.                                                                    |\n\n![](image.001.png)  \nDavid Villiers  \nDelegate of the Civil Aviation Safety Authority\n\n23 June 2006","sortOrder":0},{"sectionNumber":"AD/F2000/19","sectionType":"part","heading":"AD/F2000/19","content":"## AD/F2000/19","sortOrder":1},{"sectionNumber":"Overwing Emergency Exit","sectionType":"part","heading":"Overwing Emergency Exit","content":"## Overwing Emergency Exit","sortOrder":2},{"sectionNumber":"8/2006","sectionType":"part","heading":"8/2006","content":"## 8/2006","sortOrder":3}],"analysis":{"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":false,"description":"This Directive implements (adopts) EASA AD 2006-0148 for the named Falcon 2000 variants by requiring insertion of that AD into the AMM until the AMM is updated to specified revisions. It does not expand the set of affected aircraft beyond those listed, nor does it add technical requirements beyond adoption of the referenced EASA AD."},"complexity_factors":["Administrative action only: requirement is to insert a copy of an external AD into the AMM rather than mandating physical modification or inspection.","Multiple model-specific thresholds: different AMM revision cut-offs apply (Falcon 2000 Rev 11; Falcon 2000EX Rev 02; Falcon 2000EX EASy Rev 02), which can cause implementation ambiguity for mixed fleets.","Cross-reference to external instrument: depends on EASA AD 2006-0148 (which supersedes DGAC AD 1999-210-009(B)), requiring operators to obtain and rely on that document.","Termination condition tied to AMM update: obligation ends only when AMM is revised to specified levels, so ongoing compliance tracking is required.","Short compliance window: 30 days from 3 August 2006 increases administrative urgency for operators."],"plain_english_summary":"This Airworthiness Directive requires operators/maintenance organisations of certain Dassault Falcon 2000 family aeroplanes to insert a copy of EASA AD 2006-0148 into Chapter 5-40 (Airworthiness Limitation Section) of the Aircraft Maintenance Manual if their AMM is below specified revision levels. It is effective 3 August 2006 and must be complied with within 30 days. The measure adopts EASA’s change extending the overwing emergency-exit opening test interval to 24 months, and the insertion may be removed once the AMM is updated to the stated revisions."},"kimi_summary":{"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This Airworthiness Directive maintains its original narrow scope — addressing a specific maintenance interval for overwing emergency exits on a limited range of Dassault Falcon aircraft. The directive does not expand beyond its initial safety purpose of ensuring proper emergency exit function through periodic testing."},"complexity_factors":["Single, specific requirement with clear applicability criteria based on aircraft model and manual revision number","Only 3 defined applicability categories (Falcon 2000, 2000EX, 2000EX EASy)","One cross-reference to external European regulation (EASA AD 2006-0148)","Simple conditional termination clause (requirement ends when manual is updated)","Single compliance timeframe (30 days after effective date)","No nested exceptions or complex conditional logic","Short document (approximately 200 words of substantive content)"],"plain_english_summary":"This AD requires owners/operators of certain Dassault Falcon 2000 series jets with older maintenance manuals to insert EASA AD 2006-0148 into their manuals, extending mandatory overwing emergency-exit inspections to 24 months. It’s a one-time administrative action tied to a safety concern—interior trim could interfere with exit operation on a similar model—and was required within 30 days of 3 August 2006.\n\nUpdating the manual to the specified revision clears the directive from records."},"flash_summary_failed":{"failed":true,"reason":"A positive credit balance is required for all requests, including BYOK, so fallback providers remain available. Add credits at https://vercel.com/d?to=%2F%5Bteam%5D%2F%7E%2Fai%3Fmodal%3Dtop-up to continue.","source":"analysis-cron"}},"importantCases":[],"_links":{"self":"/api/acts/ad-f2000-19-overwing-emergency-exit","history":"/api/acts/ad-f2000-19-overwing-emergency-exit/history","analysis":"/api/acts/ad-f2000-19-overwing-emergency-exit/analysis","conflicts":"/api/acts/ad-f2000-19-overwing-emergency-exit/conflicts","importantCases":"/api/acts/ad-f2000-19-overwing-emergency-exit/important-cases","documents":"/api/acts/ad-f2000-19-overwing-emergency-exit/documents"}}