A standard 2000 Bell 430 made by Bell Helicopter Textron Canada was equipped with Honeywell Gold Crown III communications avionics, Honeywell KFC 500 AFCS (automatic flight control system), (GPS optional), flight avionics, Rogerson-Kratos LCD IIDS (integrated instrumentation display system) comprised of two active matrix LCDs displaying engine and system parameters with optional Rogerson-Kratos EFIS (electronic flight instrumentation system).
This is not to say N430MK is necessarily so-equipped, nor your series serials noted. That would depend on what was perhaps special-ordered originally and any subsequent approved avionics installations/modifications. A query direct to Bell at telephone: (+1 514) 437 3400 (Quebec) might answer specifics as to serial number avionics configurations as ordered/produced.
The standard Bell 430 flying controls were: Fully powered hydraulic, elastomeric pitch change and flapping bearings, fixed tailplane with leading-edge slats and endplate fins, strakes under sponsons, single-pilot IFR system without auto-stabilization.
Dual hydraulic systems (dual for main rotor collective and cyclic, single for tail rotor). Dual 28 Volt DC electrical systems, powered by two 30 Volt DC 200 Amp engine-mounted starter/generators derated to 180 Amps and a 24 Volt 28 Amp Hour Ni/Cd battery.