Toliss Airbus A330-900 NEO for X-plane 12 скачать в хорошем качестве

Toliss Airbus A330-900 NEO for X-plane 12

Available at the X-plane.org Store: https://store.x-plane.org/Airbus-A330... Description: Officially Licensed by Airbus Most accurate system functionality for any A330 aircraft in the flight simulation world. A330-900 specific features: HUD – Head up display on both the pilot and co-pilot sides providing all relevant flight information in the pilot’s field of view during all flight phases DRAIMS - Digital Radio and Audio Integrating Management System providing easier management of radio frequencies, transponder settings as well as backup radio navigation ATSAW - Airborne Traffic Situation Awareness showing detailed information about surrounding traffic on the Navigation Display (ND) ROW/ROPS - Runway overrun warning & Runway Overrun Prevention System alerting the crew if the available runway length becomes insufficient for a safe landing TOS - take off surveillance alerting the crew if it attempts taking off from a taxiway or a runway different than selected in the FMS ISCS is now available in the EFB also, but can also be used in a separate window Detailed FMGS: -3 independent MCDUs providing real life -FMGS programming capability -2 independent autopilots -SID/STAR and airways support in a fully custom FMGS backbone supporting all A424 leg types (Arc, course or heading to intercept, Radius to Fix, Holdings, etc.) -Support for all approach types present in real life A330-900s, including GLS, ILS, SLS, FLS, LOC backcourse, etc. -Full VNAV guidance with TOC, TOD, Deceleration point, speed limits, fuel prediction, etc. -Altitude and speed constraints as the real aircraft deals with them -Support for Go-Arounds and diversions -Nav Aid autotuning -Pilot item database, such as pilot fixes, pilot navaids etc. -Flight plan saving via the Pilot routes page -Equitime point computation and nearest airports page Accurate systems:- -Fly-by-wire system with reversion between normal law and alternate law 1, alternate law 2 and direct law as per real life logics. -Hydraulic model for flight control actuators computing hydraulic flow through the actuators, the control surface hinge moment, maximum feasible deflection etc. This gives realistic surface floating angles if a control surface is lost due to combinations of hydraulic and computer faults. -Quantitative hydraulic model considering the maximum hydraulic flows of the different pumps as a function of engine speed. This is most noticeable when flying on RAT or with wind milling engines -Quantitative bleed model considering the bleed mass flow for engine start, wing anti-ice air conditioning packs etc. -High fidelity fuel system including inflight CG control by pumping fuel to and from the tail tank, fuel jettison, manual and automatic transfers between the different tanks -Detailled model of each ADIRU including alignment, small pressure sensor differences between the units, switching of sources for PFDs and autopilot inputs -Fault injection system allowing to trigger over 250 system faults either at a specific point in flight or randomly during a flight phase -Cockpit display system simulating the dependency of the displays on the Display management computers resulting in real life display limitations -ECAM system with over 30 warning and over 200 caution messages including associated ECAM actions. -Backup Speed Scale (BUSS) to provide an estimated speed based on Angle of Attack data and an estimated altitude based on GPS data. Read full description on the product page. Wanna help me create more high-quality content and support me? Become a patron: https://www.patreon.com/ThomasRasmuss... Follow me on instagram:   / rasmussen_aviation   Like me on Facebook:   / rasmussenaviation   If you like my videos, please subscribe to my channel. Thank You For Watching! 2024 (C) Thomas Rasmussen Please, notice that reupload or any use of my videos without granded permission and proper credit will be removed without further notice!