G1000 NXi System Maintenance Manual
Page 103
King Air 300 Series
Revision 1
190-00716-N1
Maintenance Intervals
Table 4-1 shows systems and items, installed by this STC, which must undergo tests or checks
at specific intervals. If the interval is shown to be in flight time as well as calendar months, the
first interval reached should be used as the limit.
The inspection time tables used for this STC are aligned with the existing maintenance 200 hr
phase inspection program used in the current King Air 300 Series Maintenance Manual. A
complete inspection cycle for the King Air 300 Series is 800 hours or 24 calendar months,
divided into the following four phases:
Inspection Phase 1
: To be performed at 200 hours and every 800 hours thereafter.
Inspection Phase 2
: To be performed at 400 hours and every 800 hours thereafter.
Inspection Phase 3
: To be performed at 600 hours and every 800 hours thereafter.
Inspection Phase 4
: To be performed at 800 hours and every 800 hours thereafter.
Those inspections that are based on flight time, calendar elapsed time or cycles shall have
specific intervals stated in Table 4-1.
IMPORTANT
!
As allowed in the King Air 300 Series Maintenance Manual, a tolerance of
+/- 20 hours for all phase inspections.
Special Inspection Items - Calendar limited inspections have a tolerance of
± 12 days per 12 calendar months.
The intention of Garmin is to align this maintenance program as best possible with the existing
King Air 300 Series inspection program. For a complete description of the King Air inspection
program, refer to the Beechcraft King Air 300 Series Maintenance Manual listed in Table 1-1.
Table 4-1, Maintenance Intervals
Item
Description/Procedure
Manual
Section No.
Interval
G1000/GFC700 Equipment
G1000/GFC700
System Visual
Inspections
Complete Visual Inspection of GWX 68 or
GWX 70 Equipment and Wiring located in
Nose Section
(Table 4-3)
Phase 4
Complete Visual Inspection of
G1000/GFC700 Equipment and Wiring
located in Nose Avionics Compartment
(Table 4-4)
Phase 4
Complete Visual Inspection of
G1000/GFC700 Equipment and Wiring
located in Pilot’s Compartment
(Table 4-5)
Phase 3
Complete Visual Inspection of
G1000/GFC700 Equipment and Wiring
located on and behind Instrument Panel
(Table 4-6)
Phase 3
Complete Visual Inspection of
G1000/GFC700 Equipment and Wiring
located in Cabin
(Table 4-7)
Phase 3
Complete Visual Inspection of
G1000/GFC700 Equipment and Wiring
located in Rear Fuselage and Empennage
(Table 4-8)
Phase 4
Summary of Contents for G1000 NXi
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