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Garmin G1000H Bell 407GX Pilot's Guide - Page 98

Dual Tachometer, Alternate Engine Data Source Annunciations, TAKEOFF TIMER

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ENGINE INDICATION & CREW ALERTING SYSTEM TAKEOFF TIMER After the engine has been started, if Q or MGT are within the takeoff limitation ranges, the G1000H displays a 5-minute countdown timer inside the PSI gauge. The timer flashes beginning when 30 seconds remain until an exceedance will occur; the timer is automatically removed when either Q or MGT fall below takeoff limits. DUAL TACHOMETER The dual tachometer displays rotor speed (NR) and power turbine speed (NP) as percentages. A readout for NR is provided. The long pointer represents NR along the gauge scale; NP is shown with the short pointer. Limitations are shown as colored arcs. A white tick mark represents the FADEC normal governing point. When Quiet Mode is active, a magenta reference bug is shown the tachometer to indicate the Quiet Mode governing point. The NR and NP pointers will be the same color as the arc(s) they are presently within. During autorotation with an engine failure, the NP pointer will be displayed in gray and the dual tachometer gauge scale will display power-off limitations. ALTERNATE ENGINE DATA SOURCE ANNUNCIATIONS If the G1000H is using alternate analog data sources to determine Q, MGT, NG, NP, or NR, a yellow 'ALTN' annunciation box will appear to the right of the PSI gauge. In addition, a yellow subscript 'A' will be shown with the affected parameter readout(s) (Figure 3-6). In the event an alternate analog data source is unavailable or invalid, a white 'ALTN' annunciation box is shown to the right of the PSI gauge A white subscript 'A' will be shown with affected the parameter readout(s) (Figure 3-6). Alternate Source Data In-Use for Torque Alternate Data Source InUse Annunciation No Alternate Data Source Available for Torque Alternate Data Source Missing or Invalid Figure 3-6 Alternate Engine Data Source Annunciations If no valid data sources are available, a red 'X' is displayed instead of a readout, and any affected pointers will be removed from the gauges. 86 Garmin G1000H™ Pilot's Guide for the Bell 407GX 190-01255-00 Rev. A

Section	Page
Section 1 System Overview	13
1.1 System Description	13
1.2 Line Replaceable Units (LRU)	14
1.3 G1000H Controls	18
PFD Controls	18
Audio Panel Controls	20
1.4 Secure Digital Cards	22
1.5 System Power-up	23
1.6 System Operation	24
Normal Display Operation	24
Reversionary Display Operation	25
AHRS Operation	26
G1000H System Annunciations	27
Softkey Function	28
GPS Receiver Operation	33
1.7 Accessing G1000H Functionality	38
Menus	38
MFD Page Groups	39
MFD System Pages	43
1.8 Display Backlighting	56
Automatic Adjustment	56
Manual Adjustment	56
Section 2 Flight Instruments	59
2.1 Flight Instruments	62
Airspeed Indicator	62
Attitude Indicator	63
Altimeter	64
Vertical Speed Indicator (VSI)	66
Vertical Deviation	67
Horizontal Situation Indicator (HSI)	68
Course Deviation Indicator (CDI)	74
2.2 Supplemental Flight Data	81
Temperature Displays	81
Wind Data	82
Vertical Navigation (VNV) Indications	83
2.3 PFD Annunciations and Alerting Functions	84
System Alerting	84
Marker Beacon Annunciations	84
Traffic Annunciation	85
HTAWS Annunciations	85
Altitude Alerting	86
Low Altitude Annunciation	86
Minimum Descent Altitude/Decision Height Alerting	87
Radar Altimeter	88
2.4 Abnormal Operations	90
Abnormal GPS Conditions	90
Unusual Attitudes	91
Section 3 Engine and Crew Alerting systems	93
3.1 Engine Indication System (EIS) Strip	95
Power Situation Indicator	97
Dual Tachometer	98
Alternate Engine Data Source Annunciations	98
3.3 Engine Page	99
Power Assurance Check	100
3.4 Crew Alerting System (CAS)	101
CAS Message Prioritization	102
Section 4 Audio Panel and CNS	105
4.1 Overview	105
MFD/PFD Controls and Frequency Display	106
Audio Panel Controls	108
4.2 COM Operation	110
COM Transceiver Selection and Activation	110
COM Transceiver Manual Tuning	111
Quick-Tuning and Activating 121.500 MHz	112
Auto-Tuning the COM Frequency	113
Frequency Spacing	117
Automatic Squelch	118
COM Volume	118
4.3 NAV Operation	119
NAV Radio Selection and Activation	119
NAV Receiver Manual Tuning	120
Auto-Tuning a NAV Frequency from the MFD	122
Marker Beacon Receiver (Optional)	127
DME Tuning (Optional)	128
4.4 GTX 33 Mode S Transponder	129
Transponder Controls	129
Transponder Mode Selection	130
Entering a Transponder Code	133
IDENT Function	134
4.5 Additional Audio Panel Functions	135
Power-Up	135
Mono/Stereo Headsets	135
Intercom	135
Clearance Recorder and Player (Optional)	141
Split COM	142
Entertainment Inputs	143
4.6 Audio Panel Preflight Procedure	144
4.7 Abnormal Operation	145
Stuck Microphone	145
COM Tuning Failure	145
Audio Panel Fail-Safe Operation	145
Section 5 Flight Management	147
5.1 Introduction	147
Navigation Status Box	148
5.2 Using Map Displays	150
Map Orientation	150
Map Range	152
Map Panning	154
Measuring Bearing and Distance	159
Topography	160
Map Symbols	163
Airways	169
Track Vector	171
Wind Vector	172
Nav Range Ring	173
Fuel Range Ring	174
Field of View (SVS)	175
5.3 Waypoints	176
Airports	177
Intersections	184
NDBs	186
VORs	188
User Waypoints	190
5.4 Airspaces	196
5.5 Direct-to-Navigation	200
5.6 Flight Planning	206
Flight Plan Creation	207
Adding Waypoints to an Existing Flight Plan	212
Adding Airways to a Flight Plan	214
Adding Procedures to a Stored Flight Plan	216
Flight Plan Storage	223
Flight Plan Editing	225
Along Track Offsets	228
Parallel Track	230
Activating a Flight Plan Leg	233
Inverting a Flight Plan	234
Flight Plan Views	235
Closest Point of FPL	237
5.7 Vertical Navigation	238
Altitude Constraints	240
5.8 Procedures	244
Departures	244
Arrivals	247
Approaches	249
5.9 Trip Planning	255
Trip Planning	255
5.10 RAIM Prediction	259
5.11 Navigating a Flight Plan	263
5.12 Abnormal Operation	291
Section 7 Automatic Flight Control System	381
Section 8 Additional Features	383
8.1 Synthetic Vision System (SVS)	384
SVS Operation	385
SVS Features	387
Field of View	396
8.2 SafeTaxi	398
8.3 ChartView	404
ChartView Softkeys	404
Terminal Procedures Charts	405
Chart Options	413
Day/Night View	419
ChartView Cycle Number and Expiration Date	421
8.4 FliteCharts	424
FliteCharts Softkeys	424
Terminal Procedures Charts	425
Chart Options	432
Day/Night View	436
FliteCharts Cycle Number and Expiration Date	438
8.5 AOPA Airport Directory	441
AOPA Database Cycle Number and Revision	442
8.6 Satellite Telephone and Data Link Services	444
Registering With Garmin Flight Data Services	444
Disable/Enable Iridium Transceiver	447
Telephone Communication	448
Text Messaging (SMS)	455
WI-FI Connections	466
System Data Logging	472
8.7 XM Radio Entertainment	475
Activating XM Satellite Radio Services	475
Using XM Radio	476
8.8 Scheduler	480
8.9 Auxiliary Video	482
Video Setup	483
Display Selection	484
Input Selection	485
Zoom/Range	485
8.9 Abnormal Operation	486
SVS Troubleshooting	486
Reversionary Mode	486
Unusual Attitudes	487
Appendices	491
Annunciations and Alerts	491
CAS Messages	491
G1000H System Annunciations	493
G1000H System Message Advisories	498
Flight Plan Import/Export Messages	507
Database Management	509
Jeppesen Databases	509
Garmin Databases	513
Glossary	519
Frequently Asked Questions	525
General TIS Information	529
Introduction	529
TIS vs. TAS/TCAS	529
TIS Limitations	529
Display Symbols	531
Index	535
Index	535

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Garmin G1000H

™

Pilot’s Guide for the Bell 407GX

190-01255-00

Rev. A

ENGINE INDICATION & CREW ALERTING SYSTEM

TAKEOFF TIMER

After the engine has been started, if Q or MGT are within the takeoff limitation ranges, the G1000H displays

a 5-minute countdown timer inside the PSI gauge.

The timer ﬂashes beginning when 30 seconds remain until

an exceedance will occur; the timer is automatically removed when either Q or MGT fall below takeoff limits.

DUAL TACHOMETER

The dual tachometer displays rotor speed (NR) and power turbine speed (NP) as percentages.

A readout

for NR is provided.

The long pointer represents NR along the gauge scale; NP is shown with the short pointer.

Limitations are shown as colored arcs.

A white tick mark represents the FADEC normal governing point.

When

Quiet Mode is active, a magenta reference bug is shown the tachometer to indicate the Quiet Mode governing

point.

The NR and NP pointers will be the same color as the arc(s) they are presently within.

During autorotation with an engine failure, the NP pointer will be displayed in gray and the dual tachometer

gauge scale will display power-off limitations.

ALTERNATE ENGINE DATA SOURCE ANNUNCIATIONS

If the G1000H is using alternate analog data sources to determine Q, MGT, NG, NP, or NR, a yellow ‘ALTN’

annunciation box will appear to the right of the PSI gauge.

In addition, a yellow subscript ‘A’ will be shown with

the affected parameter readout(s) (Figure 3-6).

In the event an alternate analog data source is unavailable or invalid, a white ‘ALTN’ annunciation box is

shown to the right of the PSI gauge

A white subscript ‘A’ will be shown with affected the parameter readout(s)

(Figure 3-6).

Figure 3-6

Alternate Engine Data Source Annunciations

Alternate Data Source In-

Use Annunciation

Alternate Source

Data In-Use for

Torque

Alternate Data Source

Missing or Invalid

No Alternate

Data Source

Available for

Torque

If no valid data sources are available, a red ‘X’ is displayed instead of a readout, and any affected pointers will

be removed from the gauges.