G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Page 1-4
190-00682-00
Revision 5
GDU 1040A (PFD1)
GDU 1500 (MFD)
No. 1 GIA 63W
System Integration
Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
WAAS
VNAV
AFCS Mode Logic
No. 1 Flight Director
Servo Communication
No. 1 GDC 74B
Air Data Computer
Airspeed, Altitude,
Vertical Speed, OAT
No. 1 GEA
Engine / Airframe
Unit
GSA 80
Roll Servo
GSA 81
Pitch Trim Servo
GSA 80
Pitch Servo
No. 1 GTX 33
Mode S Transponder
No. 2 GMA
1347D
GDL69A
XM Satalite Datalink
(WX & Radio)
No.1 GTP59
OAT Probe
GMC 710 (AFCS Controller)
No. 1 GMU44
Magnotometer
GSA 80
Yaw Servo
DME
WX-500
SKY899
No. 2 GIA 63W
System Integration
Processors
I/O Processors
VHF COM
VHF NAV/LOC
GPS
Glideslope
WAAS
VNAV
AFCS Mode Logic
No. 2 Flight Director
Servo Communication
No. 2 GDC 74B
Air Data Computer
Airspeed, Altitude,
Vertical Speed, OAT
No. 2 GEA
Engine / Airframe
Unit
No. 2 GRS 77 AHRS
Atitude
Rate of Turn
Slip/Skid
No. 1 GRS 77 AHRS
Atitude
Rate of Turn
Slip/Skid
No. 2 GMU44
Magnotometer
No. 2 GTX 33
Mode S Transponder
No. 2 GTP59
OAT Probe
GDU 1040A (PFD2)
No. 1 GMA
1347D
GCU 475 (FMS Controller)
GWX 68
WX Radar
No. 1 ST—26
Tach-Gen
Adapter
No. 2 ST—26
Tach-Gen
Adapter
PC-920
FF Signal
Conditioner
Figure 1-1. G1000 & GFC 700 in King Air C90A/C90GT
