Pitot/Static Heading Synchro XYZ
information from an HSI bootstrap, OAT
from a Shadin Avionics OAT probe (supplied), Fuel
Flow information (may require transducers),
RS-232 / RS-422 from GPS
Output:
RS-232 / 422 fed to the GPS receiver
to
display the following information: Individual
engine fuel flow (GPS calculates fuel
remaining/used, fuel to destination,
left/right engine used, etc.), TAS, Winds
Aloft, Wind Component, Mach, IAS, IVS,
TAT, ROT, OAT, PA, DA, MH