Table 4-5, Pilot's Compartment Visual Inspection Procedure - Garmin G1000 Nxi System Maintenance Manual

Item
a) Inspect the standby battery, rack and connectors for corrosion, or other defaults.
Standby Battery
b) Inspect the standby battery fuses and associated bracket for corrosion or other defects.
GIA Avionics Fan Inspect remote avionics fans and hoses for dirt accumulation and other damage. Remove
(Qty 2) excess dirt as required.
GTS 820/850 Inspect the GTS 820/850 or GTS Traffic Processor unit (if installed), rack and connectors for
Traffic or GTS corrosion or other defects. Check the integrity of the shield block ground attachments to the
Traffic Processor harness connector assembly as well as the integrity of the individual shields and their
(option) attachment.
LMD Rack and
Inspect the LMD rack, modules, and terminations for corrosion or other defects.
Modules
a) Inspect bulkhead connectors for security of attachment, corrosion or other defects.
b) Inspect wire and coax for chafing, damage, proper routing of wire bundles and security
of attachment in accordance with AC 43.13-1B, Chapter 11, Section 8, Paragraph 11-96
and the Nose Wire Harness Routing drawing, listed in Table 1-1 . Pay particular
Nose Wiring
attention to possible areas of wire chafing such as the middle shelf feed-through hole,
harness
wheel well protrusion etc.
c) Inspect Ground blocks for security of attachment, corrosion or other defects.
d) Ensure all connectors are securely fastened.

Table 4-5, Pilot's Compartment Visual Inspection Procedure

Item
Inspect that all required placards are installed on the left and right control wheels.
Placards Placards must be legible, secure and in good condition. Refer to the Control Wheel
Modification drawing listed in Table 1-1.
Locate equipment in the aft pedestal for the following inspection.
Inspect the GCU 477 unit and connector for corrosion or other defects. Check the
GCU 477 integrity of the SHIELD BLOCK ground attachments to the harness connector assembly
as well as the integrity of the individual shields and their attachment.
Inspect the ADF control unit and connector for corrosion or other defects. Check the
ADF control unit
integrity of the SHIELD ground attachments to the harness connector assembly as well
(relocated by STC)
as the integrity of the individual shields and their attachment.
Inspect all visible wire harness for chafing, damage, proper routing of wire bundles and
Pedestal Wiring security of attachment in accordance with AC 43.13-1B, Chapter 11, Section 8,
Paragraph 11-96 and the Cabin Wire Harness Routing drawing, listed in Table 1-1.
a)
GTP 59 (Qty 2)
b)
G1000 NXi System Maintenance Manual
King Air 300 Series
190-00716-N1
Description/Procedure
Description/Procedure
Inspect the GTP 59 units and connectors for corrosion or other defects. Check the
integrity of the SHIELD ground attachments to the harness connector assembly as
well as the integrity of the individual shields and their attachment.
Inspect wire harness for chafing, damage, proper routing of wire bundles and
security of attachment in accordance with AC 43.13-1B, Chapter 11, Section 8,
Paragraph 11-96 and the Cabin Wire Harness Routing drawing, listed in Table 1-1.
Initials
Initials
Page 110
Revision 1