Airplane Flight Manual Supplement

Hawker Beechcraft C90A and C90GT King Air 190-00682-02 Rev. C
Page 8 of 95
North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace
per AC 91-49 and AC 120-33. Both GPS/SBAS receivers are required to be operating
and receiving usable signals except for routes requiring only one Long Range Navigation
sensor.
NOTE
Each display computes an independent navigation solution based on the on-side
GPS sensor. However, either display will automatically revert to the cross-side
sensor if the on-side sensor fails or if the cross-side sensor is determined to be
more accurate. A “BOTH ON GPS1” or “BOTH ON GPS2” message does not
necessarily mean that one GPS has failed. Refer to the MFD AUX-GPS STATUS
page to determine the state of the unused GPS.
Enroute and Terminal including RNP5/BRNAV and PRNAV (RNP-1) - In accordance with
JAA TGL-10 Rev 1, ACJ 20X4, AC 90-96A, and AC 90-100A provided the FMS is
receiving usable navigation information from one or more GPS/SBAS receivers.
The G1000 Integrated Avionics system as installed in this is aircraft is eligible for
B-RNAV in accordance with AMJ20X2.
The G1000 Integrated Avionics system as installed in this aircraft is eligible for PRNAV in
accordance with PRNAV requirements: JAA Administrative & Guidance Material Section
One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and
Operational Approval for Precession RNAV Operations in Designated European Airspace
7.1 Required Functions.
Navigation information is referenced to WGS-84 reference system, and should only be
used where the Aeronautical Information Publication (including electronic data and
aeronautical charts) conform to WGS-84 or equivalent.
ELECTRONIC FLIGHT BAG
The G1000 Integrated Avionics System as installed in this aircraft supports approval of AC 120-76A
Hardware Class 3, Software Type C Electronic Flight Bag (EFB) electronic aeronautical chart applications
when using current FliteChart or ChartView data. Additional operational approvals may be required.
For operations under 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.