Page 3-8
G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5
190-00682-00
•
TAXI LIGHTS switch to
ON
•
RECOG LIGHTS switch to
ON
•
PILOT WSHLD ANTI-ICE switch to
ON
•
COPILOT WSHLD ANTI-ICE switch to
ON
•
STALL WARN ICE PROTECTION switch to
ON
•
LEFT/RIGHT FUEL VENT ICE PROTECTION switch to
ON
•
LEFT/RIGHT PITOT ICE PROTECTION switch to
ON
•
ELEC HEAT switch to
NORM
•
LEFT/RIGHT BLEED AIR VALVES switch to
OPEN
•
LEFT/RIGHT ENGINE ANTI-ICE switch to
ON
•
CABIN TEMP MODE switch to
AUTO
•
PROP SYNC switch to
ON
(depressed)
•
BOOST PUMP-LEFT switch to
ON
•
BOOST PUMP-RIGHT switch to
ON
•
SURFACE DEICE switch to
SINGLE
9. Observe the DC electrical load (EXT PWR ON, BATT charge, External lights, anti-ice systems) from
the amp meter and record in Table 1 as DP2.
10. Turn off all switches referenced in paragraph 8.
11. Configure the aircraft to measure G1000/GFC700 system loads by making or verifying the following
switch selections:
12. Ensure that the circuit breakers in paragraph 5 are closed with the exception of
RADAR
circuit
breaker.
•
EXT PWR –
ON
•
AVIONICS MASTER PWR –
ON
•
BUS SENSE –
NORM
•
GEN TIES –
NORM
•
MASTER PANEL LIGHTS –
ON
•
OVERHEAD FLOOD LIGHT CONTROL –
ON
and adjusted to max brightness
•
INSTRUMENT INDIRECT LIGHT CONTROL –
ON
and adjusted to max brightness
•
PILOT PFD LIGHT CONTROL –
ON
and adjusted to max brightness
•
STBY INST LIGHT CONTROL -
ON
and adjusted to max brightness
•
MFD LIGHT CONTROL -
ON
and adjusted to max brightness
•
OVHD PED & SUBPANEL LIGHT CONTROL -
ON
and adjusted to max brightness
