{"product_id":"can-bus-bridge","title":"CAN Bus Bridge","description":"\u003cdiv class=\"flybox-canbridge-wrapper\" style=\"font-family: inherit; line-height: 1.85; color: #1e293b; font-size: 1.25rem;\"\u003e\n\n  \u003c!-- Hero Header Panel --\u003e\n  \u003cdiv style=\"background: linear-gradient(135deg, #0C1B2A 0%, #1e293b 100%); color: #ffffff; padding: 2.75rem 2.25rem; border-radius: 12px; margin-bottom: 2.75rem; box-shadow: 0 4px 12px rgba(12, 27, 42, 0.15);\"\u003e\n    \u003cdiv style=\"font-size: 1.05rem; font-weight: 800; letter-spacing: 2px; text-transform: uppercase; color: #38bdf8; margin-bottom: 0.75rem;\"\u003e\n      Genuine Flybox Avionics Hardware\n    \u003c\/div\u003e\n    \u003ch2 style=\"font-size: 2rem; font-weight: 700; margin: 0 0 1.35rem 0; color: #ffffff; line-height: 1.3;\"\u003e\n      Flybox CAN Bus Bridge \/ Isolator Module\n    \u003c\/h2\u003e\n    \u003cp style=\"font-size: 1.3rem; color: #e2e8f0; margin: 0; line-height: 1.75;\"\u003e\n      The \u003cstrong\u003eFlybox CAN Bus Bridge\u003c\/strong\u003e is an intelligent dual-channel avionics network gateway and galvanic isolator designed for \u003cstrong\u003eUltralight, Light Sport (LSA), and Experimental aircraft\u003c\/strong\u003e. Engineered to link distinct digital networks—such as bridging Rotax iS engine ECUs to Flybox glass cockpits—it filters telemetry, translates baud rates, and isolates sensitive flight displays from inductive electrical noise and bus faults.\n    \u003c\/p\u003e\n  \u003c\/div\u003e\n\n  \u003c!-- Key Specs Dashboard Strip --\u003e\n  \u003cdiv style=\"background-color: #f8fafc; border: 1px solid #cbd5e1; border-radius: 8px; padding: 1.75rem; margin-bottom: 3rem; display: flex; flex-wrap: wrap; justify-content: space-between; gap: 1.5rem;\"\u003e\n    \u003cdiv style=\"flex: 1 1 220px;\"\u003e\n      \u003cspan style=\"display: block; font-size: 1rem; font-weight: 800; color: #64748b; text-transform: uppercase;\"\u003eDevice Role\u003c\/span\u003e\n      \u003cspan style=\"font-size: 1.35rem; font-weight: 700; color: #0C1B2A;\"\u003eCAN Gateway \/ Bridge\u003c\/span\u003e\n    \u003c\/div\u003e\n    \u003cdiv style=\"flex: 1 1 220px;\"\u003e\n      \u003cspan style=\"display: block; font-size: 1rem; font-weight: 800; color: #64748b; text-transform: uppercase;\"\u003eChannels\u003c\/span\u003e\n      \u003cspan style=\"font-size: 1.35rem; font-weight: 700; color: #0C1B2A;\"\u003e2x Isolated Ports\u003c\/span\u003e\n    \u003c\/div\u003e\n    \u003cdiv style=\"flex: 1 1 220px;\"\u003e\n      \u003cspan style=\"display: block; font-size: 1rem; font-weight: 800; color: #64748b; text-transform: uppercase;\"\u003eElectrical Bus\u003c\/span\u003e\n      \u003cspan style=\"font-size: 1.35rem; font-weight: 700; color: #0C1B2A;\"\u003e10 V – 30 V DC\u003c\/span\u003e\n    \u003c\/div\u003e\n    \u003cdiv style=\"flex: 1 1 220px;\"\u003e\n      \u003cspan style=\"display: block; font-size: 1rem; font-weight: 800; color: #64748b; text-transform: uppercase;\"\u003eStandard\u003c\/span\u003e\n      \u003cspan style=\"font-size: 1.35rem; font-weight: 700; color: #0C1B2A;\"\u003eISO 11898 (CAN 2.0)\u003c\/span\u003e\n    \u003c\/div\u003e\n  \u003c\/div\u003e\n\n  \u003c!-- Section: Core Capabilities (2x2 Grid) --\u003e\n  \u003ch3 style=\"font-size: 1.55rem; color: #0C1B2A; text-transform: uppercase; letter-spacing: 1px; margin-bottom: 0.75rem; font-weight: 700;\"\u003e\n    Network Reliability \u0026amp; Avionics Protection\n  \u003c\/h3\u003e\n  \u003cp style=\"font-size: 1.25rem; color: #475569; margin: 0 0 2rem 0;\"\u003e\n    Why an isolated CAN bridge is essential for modern electronically controlled cockpits:\n  \u003c\/p\u003e\n\n  \u003cdiv style=\"display: grid; grid-template-columns: repeat(auto-fit, minmax(320px, 1fr)); gap: 1.75rem; margin-bottom: 3rem;\"\u003e\n    \n    \u003cdiv style=\"border: 1px solid #cbd5e1; border-radius: 8px; padding: 1.75rem; background: #ffffff; border-top: 4px solid #0C1B2A;\"\u003e\n      \u003cdiv style=\"display: flex; align-items: center; margin-bottom: 0.85rem;\"\u003e\n        \u003cspan style=\"background: #0C1B2A; color: #ffffff; width: 32px; height: 32px; border-radius: 50%; display: inline-flex; align-items: center; justify-content: center; font-size: 0.95rem; font-weight: 700; margin-right: 12px;\"\u003e01\u003c\/span\u003e\n        \u003ch4 style=\"margin: 0; font-size: 1.35rem; color: #0C1B2A; font-weight: 700;\"\u003eGalvanic Fault Isolation\u003c\/h4\u003e\n      \u003c\/div\u003e\n      \u003cp style=\"margin: 0; font-size: 1.18rem; color: #334155; line-height: 1.75;\"\u003e\n        Electrically decouples the engine ECU and high-power servo channels from the main instrument bus. Prevents ground loops, alternator voltage spikes, and starter surges from damaging flight deck processors.\n      \u003c\/p\u003e\n    \u003c\/div\u003e\n\n    \u003cdiv style=\"border: 1px solid #cbd5e1; border-radius: 8px; padding: 1.75rem; background: #ffffff; border-top: 4px solid #0C1B2A;\"\u003e\n      \u003cdiv style=\"display: flex; align-items: center; margin-bottom: 0.85rem;\"\u003e\n        \u003cspan style=\"background: #0C1B2A; color: #ffffff; width: 32px; height: 32px; border-radius: 50%; display: inline-flex; align-items: center; justify-content: center; font-size: 0.95rem; font-weight: 700; margin-right: 12px;\"\u003e02\u003c\/span\u003e\n        \u003ch4 style=\"margin: 0; font-size: 1.35rem; color: #0C1B2A; font-weight: 700;\"\u003eBaud Rate \u0026amp; Protocol Gateway\u003c\/h4\u003e\n      \u003c\/div\u003e\n      \u003cp style=\"margin: 0; font-size: 1.18rem; color: #334155; line-height: 1.75;\"\u003e\n        Translates and buffers telemetry packets across busses running at mismatched speeds (e.g. 250 kbps engine ECU data linked to a 500 kbps or 1 Mbps glass cockpit flight bus) without packet loss.\n      \u003c\/p\u003e\n    \u003c\/div\u003e\n\n    \u003cdiv style=\"border: 1px solid #cbd5e1; border-radius: 8px; padding: 1.75rem; background: #ffffff; border-top: 4px solid #0C1B2A;\"\u003e\n      \u003cdiv style=\"display: flex; align-items: center; margin-bottom: 0.85rem;\"\u003e\n        \u003cspan style=\"background: #0C1B2A; color: #ffffff; width: 32px; height: 32px; border-radius: 50%; display: inline-flex; align-items: center; justify-content: center; font-size: 0.95rem; font-weight: 700; margin-right: 12px;\"\u003e03\u003c\/span\u003e\n        \u003ch4 style=\"margin: 0; font-size: 1.35rem; color: #0C1B2A; font-weight: 700;\"\u003eBus Traffic Filtering\u003c\/h4\u003e\n      \u003c\/div\u003e\n      \u003cp style=\"margin: 0; font-size: 1.18rem; color: #334155; line-height: 1.75;\"\u003e\n        Selectively filters high-frequency raw broadcast traffic, forwarding only relevant engine and air data parameters to keep primary flight computers responsive and prevent bus saturation.\n      \u003c\/p\u003e\n    \u003c\/div\u003e\n\n    \u003cdiv style=\"border: 1px solid #cbd5e1; border-radius: 8px; padding: 1.75rem; background: #ffffff; border-top: 4px solid #0C1B2A;\"\u003e\n      \u003cdiv style=\"display: flex; align-items: center; margin-bottom: 0.85rem;\"\u003e\n        \u003cspan style=\"background: #0C1B2A; color: #ffffff; width: 32px; height: 32px; border-radius: 50%; display: inline-flex; align-items: center; justify-content: center; font-size: 0.95rem; font-weight: 700; margin-right: 12px;\"\u003e04\u003c\/span\u003e\n        \u003ch4 style=\"margin: 0; font-size: 1.35rem; color: #0C1B2A; font-weight: 700;\"\u003eFault Containment\u003c\/h4\u003e\n      \u003c\/div\u003e\n      \u003cp style=\"margin: 0; font-size: 1.18rem; color: #334155; line-height: 1.75;\"\u003e\n        Contains wiring faults to their respective branch. If a severed wire or short occurs on an actuator or engine harness, the bridge prevents the fault from crashing the primary PFD network.\n      \u003c\/p\u003e\n    \u003c\/div\u003e\n\n  \u003c\/div\u003e\n\n  \u003chr style=\"border: 0; border-top: 1px solid #cbd5e1; margin: 3.5rem 0;\"\u003e\n\n  \u003c!-- Technical Specifications Table --\u003e\n  \u003ch3 style=\"font-size: 1.55rem; color: #0C1B2A; text-transform: uppercase; letter-spacing: 1px; margin-bottom: 2rem; display: flex; align-items: center; font-weight: 700;\"\u003e\n    \u003cspan style=\"display: inline-block; width: 14px; height: 14px; background-color: #0C1B2A; border-radius: 50%; margin-right: 14px;\"\u003e\u003c\/span\u003e\n    Technical Specifications\n  \u003c\/h3\u003e\n  \n  \u003cdiv style=\"overflow-x: auto; border: 1px solid #cbd5e1; border-radius: 8px; margin-bottom: 2.25rem;\"\u003e\n    \u003ctable style=\"width: 100%; border-collapse: collapse; font-size: 1.2rem; line-height: 1.7;\"\u003e\n      \u003ctbody\u003e\n        \u003ctr style=\"border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A; width: 44%;\"\u003eProduct Role\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eDual-Channel CAN Bus Bridge \/ Gateway \u0026amp; Electrical Isolator\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"background-color: #f8fafc; border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eAvionics System Compatibility\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eFlybox Eclipse NG, Flybox Vigilus EIS, Flybox EngiMaster EIS, and Oblò PFD\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eOperating Voltage Range\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003e10 V – 30 V DC (12 V and 24 V aircraft electrical systems)\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"background-color: #f8fafc; border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eCAN Channels\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003e2x Independent High-Speed CAN ports (CAN 1 \u0026amp; CAN 2)\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eProtocol Standards\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eISO 11898 • CAN 2.0A (Standard 11-bit) \u0026amp; CAN 2.0B (Extended 29-bit)\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"background-color: #f8fafc; border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eGalvanic Isolation\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eUp to 1 kV galvanic isolation between ports\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eSupported Baud Rates\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003e125 kbps, 250 kbps, 500 kbps, and 1 Mbps (independent per port)\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"background-color: #f8fafc; border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eTermination Provision\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eIntegrated\/configurable 120 Ω bus termination resistors\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr style=\"border-bottom: 1px solid #e2e8f0;\"\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eOperating Temperature Range\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003e-20°C to +85°C (cockpit and avionics sub-panel rated)\u003c\/td\u003e\n        \u003c\/tr\u003e\n        \u003ctr\u003e\n          \u003ctd style=\"padding: 18px 24px; font-weight: 700; color: #0C1B2A;\"\u003eTarget Aircraft\u003c\/td\u003e\n          \u003ctd style=\"padding: 18px 24px; color: #1e293b;\"\u003eUltralights, Light Sport (LSA), Microlights, and Homebuilt Experimental aircraft\u003c\/td\u003e\n        \u003c\/tr\u003e\n      \u003c\/tbody\u003e\n    \u003c\/table\u003e\n  \u003c\/div\u003e\n\n  \u003c!-- Operational Note Callout --\u003e\n  \u003cdiv style=\"background-color: #f1f5f9; border-left: 6px solid #0C1B2A; padding: 1.75rem 2rem; border-radius: 4px; font-size: 1.18rem; color: #334155; line-height: 1.8;\"\u003e\n    \u003cstrong\u003eInstallation Advisory:\u003c\/strong\u003e Mount the bridge module securely to an avionics tray or behind the instrument panel away from high-heat ducting. Each isolated CAN segment must be properly terminated with two 120 Ω resistors (one at each physical end of that bus segment). Always use Mil-Spec twisted shielded pair cabling (e.g. M27500 \/ Tefzel) for all CAN-H and CAN-L data lines.\n  \u003c\/div\u003e\n\n\u003c\/div\u003e","brand":"Flybox Avionics","offers":[{"title":"25cm","offer_id":59019859657035,"sku":"105820","price":32.0,"currency_code":"GBP","in_stock":true},{"title":"50cm","offer_id":59019859689803,"sku":"105830","price":34.0,"currency_code":"GBP","in_stock":true},{"title":"100cm","offer_id":59019859722571,"sku":"105840","price":36.0,"currency_code":"GBP","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/1000\/9719\/6363\/files\/Flybox_Avionics_Cabl_CanBus_Omnia_105820.jpg?v=1793104890","url":"https:\/\/www.albionaero.co.uk\/products\/can-bus-bridge","provider":"Albion Aero Services Ltd","version":"1.0","type":"link"}