{"id":"F2006L02213","name":"AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit","slug":"ad-amd-10-22-amdt-1-overwing-emergency-exit","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":117541,"registerId":"commonwealth-F2006L02213-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"AMD Falcon 10 Series Aeroplanes","sectionType":"division","heading":"AMD Falcon 10 Series Aeroplanes","content":"### AMD Falcon 10 Series Aeroplanes\n\n| AD/AMD 10/22 Amdt 1 | Overwing Emergency Exit | 8/2006 |\n| ------------------- | ----------------------- | ------ |\n\n| Applicability: | All Falcon 10 aircraft for which the Aircraft Maintenance Manual (AMM) Airworthiness Limitation Section, Chapter 5-40, is not at Revision 08 or above.                                                                                                                                                                                                |\n| -------------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n| Requirement:   | Insert a copy of EASA AD 2006-0147 into Chapter 5-40 of the Aircraft Maintenance Manual.Note: Updating Chapter 5-40 with Revision 08 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 Amendment 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.Amendment 1 is issued in response to a new EASA AD, which supersedes DGAC AD 1999-211-023(B) (the original issue of this Directive), and 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/AMD 10/22 Amdt 1","sectionType":"part","heading":"AD/AMD 10/22 Amdt 1","content":"## AD/AMD 10/22 Amdt 1","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":{"kimi_summary":{"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This is a targeted amendment to a specific airworthiness directive. It remains narrowly focused on the original safety issue (overwing emergency exit interference) and does not expand beyond the Falcon 10 aircraft type or the specific maintenance procedure."},"complexity_factors":["Single, specific aircraft type (Falcon 10 series)","One clear compliance action (insert document into manual)","Simple conditional logic (applies only if manual revision below 08)","Single defined term (AMM - Aircraft Maintenance Manual)","No nested exceptions or cross-references to other legislation","Clear deadline (30 days after 3 August 2006)","Total length: approximately 200 words"],"plain_english_summary":"This AD requires operators of certain Falcon 10 jets to insert EASA AD 2006‑0147 into their maintenance manual within 30 days of 3 August 2006, unless the manual is already at Revision 08 or later. It mandates periodic (24‑month) checks because interior trim could block overwing emergency exits, posing an escape risk. Once the manual is updated to Revision 08, this notice can be removed."},"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"},"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":true,"description":"Amendment 1 replaces the earlier directive by adopting EASA AD 2006-0147 (superseding DGAC AD 1999-211-023(B)) and extends the repetitive overwing emergency-exit opening test interval to 24 months; it requires insertion of that EASA AD into AMM Chapter 5-40 for affected Falcon 10 aircraft until the AMM is updated to Revision 08."},"complexity_factors":["Cross-reference to an external document (EASA AD 2006-0147) means operators must obtain and incorporate another regulator's text into their AMM.","Applicability is conditional on the AMM revision state (applies only where Chapter 5-40 is not at Revision 08 or above), creating an administrative eligibility check.","Termination condition: updating AMM Chapter 5-40 to Revision 08 removes the obligation — requires record-keeping and follow-up.","Short compliance deadline (30 days after 3 August 2006) imposes prompt administrative action.","Substantive change to maintenance practice: extends the repetitive overwing-exit opening test interval to 24 months (amends prior AD).","Narrow technical scope (Falcon 10 series) reduces operational breadth but concentrates impact on affected operators and maintenance organisations."],"plain_english_summary":"This directive requires operators of Falcon 10 series aircraft whose Aircraft Maintenance Manual (AMM) Chapter 5-40 is below Revision 08 to insert EASA AD 2006-0147 into that AMM. It updates the overwing emergency-exit maintenance regime (extending the opening-test interval to 24 months) and must be complied with within 30 days after 3 August 2006; once AMM Chapter 5-40 is updated to Revision 08 the insertion requirement ends."}},"importantCases":[],"_links":{"self":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit","history":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit/history","analysis":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit/analysis","conflicts":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit/conflicts","importantCases":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit/important-cases","documents":"/api/acts/ad-amd-10-22-amdt-1-overwing-emergency-exit/documents"}}