Page 6-20 G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 4 190-00716-01
VIEW OF LEFT SIDE NOSE AVIONICS BAY
(NOT ALL ITEMS SHOWN FOR CLARITY)
COOLING FAN HOSE (TYP)
COOLING FAN
NOSE WHEEL WELL HOUSING
FAN INLET DUCT (IF INSTALLED)
P/N 115-00580-02
Figure 6-7, GIA Cooling Fan Inlet Duct Identification
Configuration applicable to MDL 005-00629-00 Rev. 7 or later FAA-approved
revision, or modified per Garmin Service Bulletin 1375
Reinstallation:
1. Reinstallation of the avionics cooling fan is the reverse of the removal. Reference the Electrical
Equipment Install, Nose Bay drawing, listed in Table 1-2, for more details.
2. If further maintenance is not required, proceed to Section 8.
6.30 GDU Cooling Fans
Removal:
1. Remove the display associated with the cooling fan, per Section
6.1.
2. Disconnect the electrical connector of the cooling fan.
3. Use a Phillips screwdriver to remove the attachment screws from the cooling fan.
4. Remove the cooling fan.
Reinstallation:
1. Reinstallation of the Sandia GDU cooling fan is the reverse of the removal. Reference the Main
Instrument Panel Installation drawing, listed in Table 1-2, for more details.
2. If further maintenance is not required, proceed to Section 8.
6.31 GTS 820/850 Traffic Unit
CAUTION:
After any maintenance or modification is made to the GTS 820/850
TAS/TCAS cables such as replacing a connector or entire cable, be
sure to adhere to all of the specifications and limitations such as
minimum and maximum cable attenuation, attenuation balance
between cables, phase matching etc.
To Next Page
Loading...
Need help?
General
