G1000 NXi System Maintenance Manual
Page 110
King Air 300 Series
Revision 1
190-00716-N1
Item
Description/Procedure
Initials
Standby Battery
a)
Inspect the standby battery, rack and connectors for corrosion, or other defaults.
b)
Inspect the standby battery fuses and associated bracket for corrosion or other defects.
GIA Avionics Fan
(Qty 2)
Inspect remote avionics fans and hoses for dirt accumulation and other damage. Remove
excess dirt as required.
GTS 820/850
Traffic or GTS
Traffic Processor
(option)
Inspect the GTS 820/850 or GTS Traffic Processor unit (if installed), rack and connectors for
corrosion or other defects. Check the integrity of the shield block ground attachments to the
harness connector assembly as well as the integrity of the individual shields and their
attachment.
LMD Rack and
Modules
Inspect the LMD rack, modules, and terminations for corrosion or other defects.
Nose Wiring
harness
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
attention to possible areas of wire chafing such as the middle shelf feed-through hole,
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
Description/Procedure
Initials
Placards
Inspect that all required placards are installed on the left and right control wheels.
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.
GCU 477
Inspect the GCU 477 unit and connector for corrosion or other defects. Check the
integrity of the SHIELD BLOCK ground attachments to the harness connector assembly
as well as the integrity of the individual shields and their attachment.
ADF control unit
(relocated by STC)
Inspect the ADF control unit and connector 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.
Pedestal Wiring
Inspect all visible 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.
GTP 59 (Qty 2)
a)
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.
b)
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.
Summary of Contents for G1000 NXi
Page 112: ......
