{"id":"F2006B09944","name":"AD/FA-200/9 Amdt 1 - Engine Driven Fuel Pump Outlet Tee - Replacement","slug":"ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":55201,"registerId":"commonwealth-F2006B09944-current","compilationNumber":null,"startDate":"2026-04-02","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"1","sectionType":"section","heading":"AD/FA-200/9 Amdt 1 - Engine Driven Fuel Pump Outlet Tee - Replacement","content":"---\nmeta-content-style-type: text/css\nmeta-content-type: application/xhtml+xml; charset=utf-8\nmeta-generator: Aspose.Words for .NET 22.10.0\n---\n\n?xml version=\"1.0\" encoding=\"utf-8\" standalone=\"no\"?>\n\nCOMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY\n\nSCHEDULE OF AIRWORTHINESS DIRECTIVES\n\n \n\n![](image.001.png)  Fuji FA-200 Series Aeroplanes\n\n \n\nAD/FA-200/9\n\nAmdt 1\n\n\nEngine Driven Fuel Pump Outlet Tee - Replacement\n\n\n3/83\n\n \n\nApplicability: All model FA-200-180 with S/No. 12 and subsequent. Requirement:  Install new engine driven fuel pump outlet tee P/No. AN783-6.\n\nNote: Fuji SB No. 200-004 and Japanese CAB AD TCD-2213-82 refer.\n\n \n\nCompliance: Within 100 hours time in service after 31 March 1983 and thereafter at intervals of 3000 hours time in service.\n\n \n\nBackground: Instances of fatigue cracking have been reported by the manufacturer. This AD has been amended to restrict the service life of the component.\n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n\n \n","sortOrder":0}],"analysis":{"kimi_summary":{"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This is a narrow, technical amendment to an existing Airworthiness Directive. It remains tightly focused on the original safety purpose: addressing fatigue cracking in a specific aircraft component. The amendment simply adds a recurring replacement interval (3000 hours) to the original one-time replacement requirement, which is a natural evolution of the safety measure rather than scope creep."},"complexity_factors":["Very short document (approximately 150 words)","Only 1 defined term implicitly used ('time in service')","No cross-references to other legislation sections","Single, clear compliance requirement with straightforward time-based trigger","No conditional logic or exceptions","Simple applicability test (model + serial number range)"],"plain_english_summary":"This is an **Airworthiness Directive** (a mandatory safety order) for owners and operators of specific Fuji FA-200 aeroplanes.\n\n**What it does:**\n- Requires replacement of a specific fuel pump part (the \"outlet tee\") on certain Fuji FA-200-180 aircraft\n- Mandates use of a new part number: AN783-6\n\n**Who it affects:**\n- Owners and operators of Fuji FA-200-180 model aircraft with **serial number 12 and onwards**\n\n**What you must do:**\n- Replace the part within **100 hours of flying time** after 31 March 1983\n- Then replace it again **every 3,000 hours of flying time** thereafter\n\n**Why it matters:**\nThe manufacturer found **fatigue cracking** (tiny cracks caused by repeated stress) in this fuel pump component. This amendment tightens the rules by limiting how long the part can stay in service before replacement, preventing potential fuel leaks or engine failure.\n\n**Related documents:**\n- Fuji Service Bulletin No. 200-004\n- Japanese Civil Aviation Bureau AD TCD-2213-82"},"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":true,"description":"The AD was amended to restrict the service life of the engine-driven fuel pump outlet tee. Mechanically, that change is implemented by prescribing installation of part P/No. AN783-6 and by setting a compulsory initial replacement within 100 hours after 31 March 1983 and recurring replacements every 3,000 hours time in service. The amendment thus narrows the component’s permitted in-service life through fixed-time replacement intervals. (Background; Requirement; Compliance)"},"complexity_factors":["Narrow applicability (single model and serial number range) reduces scope complexity. (Applicability)","Mandatory single-action requirement (install specified part number) simplifies compliance steps. (Requirement)","Time-based compliance schedule with an initial short window (100 hours after 31 March 1983) plus a long recurring interval (3,000 hours) introduces scheduling considerations. (Compliance)","Reference to external documents (Fuji SB No. 200-004 and Japanese AD) requires cross-checking for procedural details. (Note)","Technical risk element (fatigue cracking) requires maintenance organisations to perform correct installation and possibly inspection practice. (Background)"],"plain_english_summary":"This AD requires owners/operators of Fuji FA-200-180 aeroplanes (serial no. 12 and later) to install engine‑driven fuel pump outlet tee P/No. AN783‑6 within 100 hours’ flying time after 31 March 1983 and replace it every 3,000 hours thereafter. It was issued to address reported fatigue cracking; operators must arrange and pay for parts, labour and scheduling to meet the mandated intervals."}},"importantCases":[],"_links":{"self":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement","history":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement/history","analysis":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement/analysis","conflicts":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement/conflicts","importantCases":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement/important-cases","documents":"/api/acts/ad-fa-200-9-amdt-1-engine-driven-fuel-pump-outlet-tee-replacement/documents"}}