Garmin G1000 Checkout Procedure page 44

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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
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LEFT/RIGHT BLEED AIR VALVES switch to OPEN
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LEFT/RIGHT ENGINE ANTI-ICE switch to ON
•
CABIN TEMP MODE switch to AUTO
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PROP SYNC switch to ON (depressed)
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BOOST PUMP-LEFT switch to ON
•
BOOST PUMP-RIGHT switch to ON
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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.
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EXT PWR – ON
•
AVIONICS MASTER PWR – ON
•
BUS SENSE – NORM
•
GEN TIES – NORM
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MASTER PANEL LIGHTS – ON
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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
Page 3-8 G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Revision 5 190-00682-00