G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90
Page 3-7
190-00682-00
Revision 5
•
AURAL WARN (if installed)
•
MODE CTL
•
STBY ALTM
•
PFD 1 (sec)
•
AHRS 1 (sec)
•
ADC 1 (sec)
•
GIA 1 (sec)
•
PFD/GIA FANS (right)
•
PFD/GIA FANS (left)
•
PFD 1 (prim)
•
AHRS 1 (prim)
•
ADC 1 (prim)
•
GIA 1 (prim)
•
MFD FAN
•
PFD 2
•
AHRS 2
•
ADC 2
•
GIA 2
•
FMS CTL
•
STBY ATT
•
STBY AUX BAT
•
AVIONICS MASTER
•
R TORQ
•
R PROP/N1 TACH
•
R ENG INST
•
R FUEL FLOW
•
R OIL PRESS
•
L TORQ
•
L PROP/N1 TACH
•
L ENG INST
•
L FUEL FLOW
•
L OIL PRESS
6. Make the following switch selections:
•
EXT PWR –
ON
7. Observe the non-switchable DC electrical load (EXT PWR ON) from the amp meter and record in
Table 1 as DP1. (Note: This load may be extremely low and can be considered negligible if under 1
amp)
8. Verify the aircraft is secure. This test should be limited in duration to minimize risks to the aircraft
systems and/or airframe. Activate the following systems:
•
BATT switch
ON
•
ICE LIGHTS switch to
ON
•
NAV LIGHTS switch to
ON
•
BEACON LIGHTS switch to
ON
•
STROBE LIGHTS switch to
ON
•
TAIL FLOOD LIGHT switch to
ON
•
LEFT/RIGHT LANDING LIGHTS switch to
ON
