Gps receiver operation, System overview, Use the small fms knob to select gps status page – Garmin G1000 King Air C90GT User Manual

Page 40

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190-00663-01 Rev. A

Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT

26

SYSTEM OVERVIEW

SY

STEM

O

VER

VIEW

FLIGHT

INSTRUMENTS

EIS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID

ANCE

AFCS

ADDITIONAL FEA

TURES

APPENDICES

INDEX

Figure 1-21 MFD Softkeys

MAP

DCLTR

TOPO

BACK

TERRAIN

DCLTR-2

DCLTR-3

DCLTR-1

Select the BACK Softkey

on this level to return to the

top softkey level.

NEXRAD

XM LTNG

SHW CHRT

CHKLIST

(optional)

AIRWAYS

AIRWY LO

AIRWAY HI

AIRWY ON

STRMSCP

TRAFFIC

(optional)

GPS RECEIVER OPERATION

Each GIA 63W Integrated Avionics Unit (IAU) contains a GPS receiver. Information collected by the specified

receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status Page.

GPS1 provides information to the pilot-side PFD and GPS2 provides data to the copilot-side PFD. Internal

system checking is performed to ensure both GPS receivers are providing accurate data to the PFDs. In some
circumstances, both GPS receivers may be providing accurate data, but one receiver may be providing a better
GPS solution than the other receiver. In this case the GPS receiver producing the better solution is automatically
coupled to both PFDs. “BOTH ON GPS 1” or “BOTH ON GPS 2” is displayed in the Reversionary Sensor
Window (see Appendix A) indicating which GPS receiver is being used. Both GPS receivers are still functioning
properly, but one receiver is performing better than the other at that particular time.

These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has

acquired satellites before the other, or one of the GPS receivers has not yet acquired a WAAS signal. While
the aircraft is on the ground, the WAAS signal may be blocked by obstructions causing one GPS receiver to
have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS
receivers temporarily losing the WAAS signal.

If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD.

If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2.
Discrepancies may indicate a problem.

Viewing GPS receiver status information

1)

Use the large FMS Knob to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD
page groups).

2)

Use the small FMS Knob to select GPS Status Page.

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