190-00716-02 Rev. 7 Beechcraft King Air 300/300LW
FAA APPROVED Page 15 of 173
Within Europe,
Using the G1000 WFDE Prediction program,
Europe’s AUGER GPS RAIM Prediction Tool at http://augur.ecacnav.com/augur/app/home.
This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of
flight. The route planning and WFDE prediction program may be downloaded from the GARMIN G1000
website on the internet. For information on using the WFDE Prediction Program, refer to GARMIN WAAS
FDE Prediction Program, part number 190-00643-01, ‘WFDE Prediction Program Instructions’.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153A for
database integrity, quality, and database management practices for the Navigation database. Flight crews
and operators can view the LOA status at FlyGarmin.com then select” Type 2 LOA Status”.
Navigation information is referenced to the WGS-84 reference system.
ELECTRONIC FLIGHT BAG
The G1000 Integrated Avionics System as installed in this aircraft supports approval of AC 120-76A
Hardware Class 3, Software Type B Electronic Flight Bag (EFB) electronic aeronautical chart applications
when using current FliteChart or ChartView data. Additional operational approvals may be required.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153 for
database integrity, quality, and database management practices for the FliteChart database. Flight crews
and operators can view the LOA status by selecting the Type 2 LOA status quick link at
www.FlyGarmin.com.
For operations under 14 CFR Part 91, it is suggested that a secondary or back up source of aeronautical
information necessary for the flight be available to the pilot in the aircraft. The secondary or backup
information may be either traditional paper-based material or displayed electronically. If the source of
aeronautical information is in electronic format, operators must determine non-interference with the G1000
system and existing aircraft systems for all flight phases.
REDUCED VERTICAL SEPARATION MINIMUMS (RVSM)
This aircraft has been evaluated in accordance with 14 CFR Part 91, Appendix G, “Operations in Reduced
Vertical Separation Minimum (RVSM) Airspace,” and FAA Advisory Circular 91-85, “Authorization of Aircraft
and Operators for Flight in Reduced Vertical Separation Minimums Airspace,” and is qualified for RVSM
operations as a group aircraft. This finding does not constitute approval to conduct RVSM operations.