{"id":"F2010L00129","name":"AD/CESSNA 560/7 Amdt 1 - Engine and Auxiliary Power Unit Fire Bottle Wiring","slug":"ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":122865,"registerId":"commonwealth-F2010L00129-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Cessna 560 (Citation V) Series Aeroplane","sectionType":"division","heading":"Cessna 560 (Citation V) Series Aeroplanes","content":"### Cessna 560 (Citation V) Series Aeroplanes\n\n| AD/CESSNA 560/7 Amdt 1 | Engine and Auxiliary PowerUnit Fire Bottle Wiring | 2/2010 |\n| ---------------------- | ------------------------------------------------- | ------ |\n\n| Applicability: | Model 560 and 560XL aeroplanes as identified in the appropriate Cessna Service Bulletins (SB) stated in the Requirement document.                                                                                                                                                                                                                         |\n| -------------- | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n| Requirement:   | Action in accordance with the technical requirements of FAA AD 2007-11-17 Amendment 39-15074.Note: Cessna Service Bulletins SB560-26-01 and SB560XL-26-02 also refer. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.                                                               |\n| Compliance:    | Unless previously accomplished in accordance with the original issue of this AD, as specified in the Requirement document.                                                                                                                                                                                                                                |\n|                | This Amendment becomes effective on 28 January 2010.                                                                                                                                                                                                                                                                                                      |\n| Background:    | The FAA has received reports of mis-wired fire extinguisher bottles. Such a condition could result in the circuit breaker disengaging (tripping) when an attempt is made to discharge the bottles. This amendment alters the presentation of the AD and refers to the latest FAA AD 2007-11-17 which supersedes previously referred to FAA AD 2006-04-10. |\n\n![](image.001.png)\n\nMike Higgins  \nDelegate of the Civil Aviation Safety Authority\n\n14 January 2010","sortOrder":0},{"sectionNumber":"AD/CESSNA 560/7 Amdt 1","sectionType":"part","heading":"AD/CESSNA 560/7 Amdt 1","content":"## AD/CESSNA 560/7 Amdt 1","sortOrder":1},{"sectionNumber":"Engine and Auxiliary PowerUnit Fire Bott","sectionType":"part","heading":"Engine and Auxiliary PowerUnit Fire Bottle Wiring","content":"## Engine and Auxiliary Power  \nUnit Fire Bottle Wiring","sortOrder":2},{"sectionNumber":"2/2010","sectionType":"part","heading":"2/2010","content":"## 2/2010","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 amendment does not expand the scope beyond the original purpose. It is purely administrative — updating the referenced FAA directive number and improving presentation. The safety issue (fire bottle wiring) and affected aircraft remain identical to the original AD."},"complexity_factors":["Very short document (approximately 250 words of substantive content)","Only 2 defined terms implicitly used (AD, Service Bulletin) — both standard aviation terminology","Single operational requirement: comply with external FAA directive","No nested conditions or exceptions — only one straightforward exemption for prior compliance","No internal cross-references within the instrument itself","Structure is simple table format with standard AD fields (Applicability, Requirement, Compliance, Background)"],"plain_english_summary":"This Airworthiness Directive requires owners/operators of Cessna 560 and 560XL jets to inspect and correct mis-wired fire-extinguisher circuitry that can trip the circuit breaker and prevent bottle discharge during an engine or APU fire. It mandates following FAA AD 2007-11-17 and related Cessna service instructions.\n\nAmendment 1 updates references to the newer FAA AD and clarifies presentation; operators who complied with the original AD need take no further action."},"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":false,"description":"The amendment updates presentation and points to FAA AD 2007-11-17 (which supersedes FAA AD 2006-04-10) but retains the same operational requirement: inspect and correct mis-wired engine/APU fire-bottle wiring as specified in the FAA AD and Cessna Service Bulletins. No broader applicability or additional mandatory actions are introduced beyond those identified in the Requirement and Applicability text."},"complexity_factors":["Cross-reference to external FAA AD 2007-11-17 as the mandatory technical requirement (Requirement).","Dependence on manufacturer Service Bulletins (SB560-26-01 and SB560XL-26-02) and acceptance of later approved revisions creates administrative tracking burden (Requirement).","Narrow technical scope focused on wiring for engine and APU fire bottles — requires hands-on maintenance and possible parts/labour (Background; Requirement).","Applicability limited to Model 560 and 560XL units identified in the SBs — requires operators to verify applicability per SB identification (Applicability).","Compliance clause allowing prior accomplishment per original AD introduces evidence/records review for operators (Compliance).","Amendment states it \"alters the presentation\" and updates cross-reference to the later FAA AD, creating minimal substantive change but potential interpretive uncertainty for implementers (Background)."],"plain_english_summary":"This AD requires operators of Cessna 560/560XL aeroplanes to inspect and, where necessary, correct engine and APU fire-bottle wiring by following FAA AD 2007-11-17 and the referenced Cessna Service Bulletins. It responds to reports that mis-wired bottles can trip circuit breakers and prevent discharge. Owners/operators pay for inspections and any rewiring; compliance may rely on later approved SB revisions and takes effect 28 January 2010."}},"importantCases":[],"_links":{"self":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring","history":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring/history","analysis":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring/analysis","conflicts":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring/conflicts","importantCases":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring/important-cases","documents":"/api/acts/ad-cessna-560-7-amdt-1-engine-and-auxiliary-power-unit-fire-bottle-wiring/documents"}}