Total Fuel Quantity; Fuel Used; Fuel Tank Temperature; Fuel Boost Pump Status - Honeywell PRIMUS 1000 Pilot's Manual

NOTES: 1. The pointer and digital readout have the same color
2. When the fuel quantity enters the amber or red
3. Left wing fuel quantity is supplied by DAU No. 1.
4. The kg or lb designation is set during installation.
Total Fuel Quantity -- Total fuel quantity is computed from the sum
D
of the fuel in the left and right fuel tanks.
Fuel Used -- Fuel used is determined by periodically evaluating fuel
D
flow rate and calculating the amount of fuel used for each engine and
maintaining a running total. APU fuel consumption is also added to
the total.
Fuel Tank Temperature -- Wing tank fuel temperature is shown in
D
green digits, the range is from --64°to +64 ° C with 1°resolution.
When the fuel temperature is less than --40 ° C, the display is shown
in amber.
Fuel Boost Pump Status -- The left and right fuel boost pump
D
status is shown in the fuel quantity display. The A, B, and C identify
pumps, or OFF can be displayed in green.
A28--1146--112--00
PRIMUSr1000 Integrated Avionics System
as the scale.
range, the digital display is boxed. The box flashes
for the first five seconds.
Right wing and fuselage fuel quantity is supplied by
DAU No. 2.
Electronic Flight Instrument System (EFIS)
4-91