AutoGyro Calidus - Page 132

Pilot Operating Handbook
Calidus
SECTION 7
SYSTEM DESCRIPTION
AutoGyro_POH_Calidus Revision 4.0 – Issue Date 17.JAN.2019 7-28
‘GEN 1’ in later
models
Secondary fuel
pump
5A Fuel pump Automotive Inst. Panel
914UL TCU 5A Engine control unit Automotive Inst. Panel
GEN 1 5A Primary Fuel
pump relay, where
fitted
Automotive Inst. Panel
GEN 2 5A Generator
operation, where
fitted
Automotive Inst. Panel
Cockpit 5A All electrical
gauges (rotor and
engine rpm, oil
pressure, water
and oil temps, fuel
gauge) and
warning lamps
Automotive Inst. panel
Avionics 10A Radio,
Transponder and
GPS units
Automotive Inst. panel
Landing lights 15A Strobes, landing
lights, nav lights
and aux socket.
NOTE! Aux socket
may be fitted with
additional 5amp in
line fuse.
Automotive Inst. panel
Start 5A Starter relay and
SMD module
Automotive Inst. panel
Variable pitch
propeller
(where fitted)
25A Main supply IVO-
prop variable pitch
propeller
Automotive Inst. panel
Fan 5A Thermostat control
of fan via relay
Automotive Inst. panel
Fan 10A
(15A
permissible)
Power supply to
fan via relay
Automotive Inst. panel
Vent 5A Cabin heater fan Automotive Inst. panel
Trim 5A Supplies power to
the stick controls
for operating the
pneumatic
solenoid valves
and the
compressor relay
Automotive Inst. panel
Rotax
regulator
25A ETFE
30A PVC
Charging circuit
from regulator to
battery/aircraft
supply
Automotive
25A fuse,
located
between the
30A fuse and
the cockpit
supply
Engine bay fuse
box, above left
fuel tank, on rear
face of enclosure
or engine bearer.