FAA Approved Airplane Flight Manual Supplement
Hawker Beechcraft B300 and B300C King Air 190-00716-03 Rev.4
Page 22 of 173 FAA APPROVED
G1000 INTEGRATED AVIONICS SYSTEM
The GARMIN G1000 Cockpit Reference Guide P/N 190-01344-01, Rev A, or later FAA accepted revision,
must be immediately available to the flight crew during all phases of flight.
Tuning of the COM and NAV radios using the GCU477 controller must be done from the left seat pilot’s
station and only referencing the pilot’s PFD.
Required flight crewmembers must wear and use headsets when the overhead cockpit speaker audio is
selected OFF.
Do not take off unless all display units are installed and operational.
Do not take off with any display in reversionary mode.
Do not take off with any of the following messages displayed in the ALERTS window:
GPS1 FAIL and GPS2 FAIL simultaneously PFD1 SERVICE
GPS NAV LOST PFD2 SERVICE
GIA1 SERVICE GMA1 SERVICE
GIA2 SERVICE GMA2 SERVICE
MFD SERVICE GEO LIMITS
The G1000 system must be turned on and operated for at least 30 minutes before takeoff if ground
outside air temperature is -40°C (-40°F) or below.
The following temperature limitations apply only to aircraft with G1000 systems installed per Garmin
drawing 005-00629-00 Revision 6 or previous and not modified by Garmin service bulletin No. 1375:
Do not takeoff if the PFD1 FAN FAIL, PFD2 FAN FAIL or MFD FAN FAIL is displayed in the
ALERTS window AND the Outside Air Temperature is greater than 41°C (106°F) AND cabin air
conditioning is inoperative.
Do not takeoff if GIA1 FAN FAIL or GIA2 FAN FAIL is displayed in the ALERTS window AND the
Outside Air Temperature is greater than 42°C (107°F).
Ground operation of the G1000 system is limited to 18 minutes when the Outside Air Temperature is
greater than 47°C (116°F) AND cabin air conditioning is inoperative.
For airplanes with system software 0985.06 or earlier, use of VNAV is prohibited during the intermediate
segment of an approach that includes a teardrop course reversal. VNAV will become ‘Unavailable’ at the
beginning of the teardrop segment of the course reversal. Use of VNAV is prohibited with course
changes greater than 90°.
The barometric altimeter must be used as the primary altitude reference for all baro VNAV operations,
including instrument approach procedure step-down fixes. Use of baro VNAV to a DA is not authorized
with a remote altimeter setting. A current altimeter setting for the landing airport is required. When
using remote altimeter minima, the baro VNAV function may be used to the published LNAV MDA.
When a flight is predicated on flying a RNP approach with an RF leg at the destination and/or alternate,
the pilot must determine that the AFCS is operational. At a minimum, the flight director must be
displayed and utilized when conducting procedures containing Radius-to-Fix (RF) segments.