The project directory is structured as follows:
- docs <Specific docs for the project>
- src <src files required for the project>
- out <contains MSFS package folder after the build>
The out folder can be deleted as it is completely recreated during the build.
This is essentially a clean build.
These systems are currently not operational / these features are missing and shall thus not lead to bug reports.
This list is divided into standardized ATA chapters, if there are no noteworthy systems missing from a chapter, the chapter heading is hidden (this was different in a previous version of this list). This list is not exhaustive, there might be details missing in other systems which are not stated here.
- FLS
- THR NOISE, DCLB
- AFS CP ALT button (immediate level-off, and alt hold indication)
- Incomplete pages see fbw-a380x/src/systems/instruments/src/MFD/pages
- Full separation into three synchronized FMCs and two FMSs (currently one FMC serving one FMS)
- EO modes / EO SID
- Accurate CI, OPT and REC MAX FL computation
- NADP (see THR NOISE above)
- Fuel planning on FMS/FUEL&LOAD page
- ATC / datalink / CPDLC
- FCU BKUP
- STEP ALTs: Optimum step calculation
- RMP: HF, TEL, MENU, SATCOM, DATALINK pages
- CIDS: CALLS buttons
- Completely migrated SLAT/FLAP CTL implementation (adapted A32NX computers at the moment)
- Automatic THS setting on ground
- Refuel Driver/Refuel Application placeholder pseudo-FQMS implementation (pre-cursor for realistic FQMS implementation while supporting instant load)
- CPIOM etc. not implemented yet.
- Portions of the automatic fuel transfer system -- main transfers from the inner, mid, trim, and outer tanks are implemented with the correct scheduling as are CG control transfers from the trim tank to the appropriate inner, mid, or feed tanks. Not implemented yet are load alleviation transfers, transfers based on remaining time to destination, cold fuel transfers, and automatic transfers that occur on the ground. The transfer pump pushbuttons work and can be used to interrupt an automatic transfer.
- The crossfeed valves work, but fuel will not be taken from the correct tank until the FADEC WASM is modified
- Manual fuel transfer
- Manually controlling how much fuel each tank receives when fueling
- Integrated Refuel Panel - Simulated in the systems but not modeled in the plane model, or fully connected to ELEC
- MFD entry - Not supported yet (ZFW/ZFWCG entry - Possible via EFB currently for testing)
- No accumulators / LEHGS systems
- Brakes: Systems were carried over from A32NX, with adapted parameters for A380X
- Gear system: Some systems were carried over from A32NX, with adapted parameters for A380X
- Hydraulic actuation of flaps/slats not finalized
- Hydraulics Cooling
- CDS / displays (automatic) reconfiguration
- PFD backup scales
- Interactive ND
- Vertical Display: Only fixed vertical range (until FL240) w/o FMS trajectory
- Independent QNH
- KCCU soft keyboard
- ECAM: Completely accurate STS page implementation
- ECAM: AUTO RCL
- ECAM: Correct behavior of RCL / RCL LAST
- ECAM: Time limited failures
- Video: ETACS due to sim limitation
- Latest FMA indications for landing modes (e.g. LAND3 instead of CAT3)
- SD VIDEO page
- Gear system not yet final
- Wrong door sequence
- BTV simplified logic only
- Basic braking distance calculations
- No glide slope adaptation
- No handling of brakes/OANS errors
- Push button in overhead for logo lights
- MMR implementation including GPIRS position
- GLS
- Weather radar / WXR
- TAWS obstacles
- Automatic detection of landing runway (needs FMS to have landing runway selected)
- Shift of touchdown point according to position on glide slope
- Oxygen masks test P/B
- Communication between systems using AFDX (ARINC protocol used mostly)
- CKPT DOOR functions
- All cargo and passenger doors animated. Most of main deck done right now
- Custom engine model (current model is modified LEAP-1A)
- ACUTE
- METOTS
- Reversers: Electrical system for triple lock safety system