System overview – Garmin G1000 Socata TBM 850 User Manual

Page 41

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190-00709-01 Rev. A

Garmin G1000 Pilot’s Guide for the Socata TBM 850

29

SYSTEM OVERVIEW

SY

STEM

O

VER
VIEW

FLIGHT

INSTRUMENTS

EAS

AUDIO P

ANEL

& CNS

FLIGHT

MANA

GEMENT

HAZARD

AV

OID
ANCE

AFCS

ADDITIONAL

FEA
TURES

APPENDICES

INDEX

8)

Use the FMS Knob to enter an arrival date and press the ENT Key.

9)

With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one
of the following is displayed:

• ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination

• ‘COMPUTING AVAILABILITY’—RAIM calculation in progress

• ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date

• ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date

• SBAS Selection (SBAS Softkey is selected)(WAAS capable systems only)

In certain situations, such as when the aircraft is outside or on the fringe of the WAAS coverage area, it may

be desireable to disable WAAS (although it is not recommended). When disabled, the SBAS field in the GPS
Status box indicates DISABLED.

Disabling WAAS

1)

Select the GPS Status Page.

2)

If necessary, select the SBAS Softkey.

3)

Press the FMS Knob. ‘WAAS’ is highlighted.

4)

Press the ENT Key to uncheck the box.

5)

Press the FMS Knob to remove the cursor.

• GPS Satellite Signal Strengths

The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite

coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed
for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for WAAS) below each
bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance:

- No bar—Receiver is looking for the indicated satellite
- Hollow bar—Receiver has found the satellite and is collecting data
- Light blue bar—Receiver has collected the necessary data and the satellite signal can be used
- Green bar—Satellite is being used for the GPS solution
- Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion)
- “D” indication—Denotes the satellite is being used as part of the differential computations

Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before

the satellite may be used for navigation (signal strength bar becomes solid).

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