Electrical system

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Across
  1. 1. One of the big 6 for load shedding.
  2. 5. Will automatically turn off if bus is running off batteries and airspeed is less than 50 KIAS.
  3. 6. Lower gear before _______ volts.
  4. 8. DDBA power output is dependent upon _______. The DDBA provides 500 to 1500 W at 65% engine speed, and 1800 to 2900 W at 100% engine speed.
  5. 10. The primary function of _____ 1 is to convert AC power from the DDBA into DC power for the Ku SATCOM, and BJB on Bus 2.
  6. 11. If EGI ____ fails, the Ku SATCOM will not be able to aim properly, which may cause the aircraft to lose Ku-band link and go lost link.
Down
  1. 2. Number of batteries.
  2. 3. Number of minutes batteries provide power for critical systems with airborne modem on.
  3. 4. The fuel heater will automatically shed when aircraft voltage drops below ____ V.
  4. 7. At minimum amperage of about 60 amperes, the batteries will provide a flight time of approximately _______ minutes.
  5. 9. Provides power to the Bus 2 Battery Junction Box and KU SATCOM components.