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Nominal battery voltage for this aircraft

Nominal generator voltage for this aircraft

Battery capacity for each battery in this aircraft

The bus that the APU is connected to, starting at bus 0

The bus that is considered essential, and that is fed by the RAT emergency generator if so equipped. Index starting at bus 0

Bitfield indicating which busses are tied together when the bus cross tie is closed. If busses 0 and 2 are conected by the tie, this would be set to 2^0 + 2^2 = 1+4 = 5

Busses that can feed the essential bus. If busses 0 and 2 can feed the essential bus, this would be set to 2^0 + 2^2 = 1+4 = 5

The number of batteries on this plane

The number of busses on this plane

The number of generators on this plane

The number of inverters on this plane

How fast the APU EGT cools down after use - influences how long the APU runs in cool down mode before it is shut down

How long the APU door takes to open or close

Fuel flow of the APU running at 100% RPM.

Which tank the APU draws fuel from, tanks being numbered 0 to 8

How long the APU takes to spool down to 10 percent

How long the APU takes to spool up to 100 percent

The maximum thrust boost at full afterburners, for all engines (legacy)

The maximum thrust boost at full afterburners, set per engine

Cylinder head temperature dataref reads in Celsius

Critical altitude for props

Exhaust gas temperature dataref reads in Celsius

The number of seconds it takes for full idle fuel flow to be reached on engine start, for propeller engines

Use acf_prop_gear_rat

Inter-turbine temperature dataref reads in Celsius

Max cylinder head temperature the plane can have before engine failure.

Max exhaust gas temperature the plane can have before engine failure.

Max Fuel Pressure the plane can have before engine failure.

Max internal turbine temperature the plane can have before engine failure.

Max Oil Pressure the plane can have before engine failure.

Max Oil Temperature the plane can have before engine failure.

Oil temperature dataref reads in Celsius

The maximum power provided by an engine (legacy)

The maximum power provided by an engine - per engine

Where the prop pitch angle goes when the governor loses oil pressure: 0=low pitch, 1=high pitch, 2=feather, 3=start lock

Engine idle speed.

Minimum engine speed with governor on.

Max engine speed.

Max engine speed. Array for 16 engines

The delay in increasing the throttle for jet engines - it is the number of seconds to actuate a full advance.

The delay in increasing the throttle for prop/turboprop engines - it is the number of seconds to actuate a full advance.

The number of seconds it takes for a free turbine to spin up from idle to full RPM.

The ratio of the engine's max RPM that the starter can spin the engine up to before it loses torque.

The ratio of the engine's maximum torque that the starter applies at its design RPM.

The maximum thrust provided by the engine, for all engines (legacy)

The maximum thrust provided by the engine, per engine

%N2 or Ng needed to generate enough bleed pressure to satisfy the biggest consumer. In case of a supercharged piston engine, upper deck pressure in inHg.

Boost Capacity

Boost Amount

The number of seconds it takes for full idle fuel flow to be reached on engine start, for jet engines

%Ng for turboprops. FCU will not allow idle to drop below this.

%N2 for jets. FADEC will not allow idle to drop below this.

Door current angle, not in flite since it is geo and this is a nice place to keep all the door geo.

Gear door area

Door axis of rotation (heading of axis)

Door extended angle

Door geo, 4 corners [20x4x4x3] Dimension is 960.

Door location (for reference-point of door) [20x3] Dimension is 60.

Door nrm, 4 corners [20x4x4x3] Dimension is 960.

Door retracted angle

Gear door type

Are any of the gear on this plane retractable. We strongly recommend you DO NOT write to this dataref.