Toliss Airbus A330-900 NEO for X-plane 12

Описание к видео 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.

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