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Garmin G1000H Bell 407GX Pilot's Guide - Page 103

Table 3-1, Warning Cas Messages, Battery Hot, Engine Fire, Engine Out, Engine Ovspd, Fadec Fail

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ENGINE INDICATION & CREW ALERTING SYSTEM NOTE: See the Rotorcraft Flight Manual (RFM) for recommended pilot actions. Annunciation Text BATTERY HOT ENGINE FIRE ENGINE OUT ENGINE OVSPD FADEC FAIL XMSN OIL PRESS XMSN OIL TEMP Description Battery overheat detected. Fire/Overheat detector senses a temperature greater than or equal to 338°F. Ng less than 55% or FADEC senses engine out. Ng greater than 110% or NP vs torque is above maximum continuous limit. Both the primary and reversionary channels have failed. Transmission oil pressure is low. Transmission oil overheat is detected. Table 3-1 Warning CAS Messages Audio Alert Single Chime Continuous Chime Continuous Fast-Pulsing Chime Single Chime Repeating Ding-Dong Chime Single Chime Single Chime Annunciation Text BAGGAGE DOOR BATTERY RLY ENGINE CHIP FADEC DEGRADED FADEC FAULT FADEC MANUAL FLOAT ARM FUEL FILTER FUEL LOW FUEL VALVE GEN FAIL HEATER OVERTMP HYDRAULIC SYS L/FUEL BOOST L/FUEL XFR LITTER DOOR MGT EXCEED MGT MISCOMP NG EXCEED NG MISCOMP NP EXCEED NP MISCOMP NR MISCOMP PEDAL STOP Q EXCEED Description Baggage door is not securely latched. Battery relay energized when battery switch is off. Battery still connected to DC bus. Chip detector has detected debris in engine oil. FADEC fault detected that may result in degraded engine performance. A fault is recorded in the FADEC. FADEC is in manual mode. Floats Arm switch is in the armed position. External fuel filter is partially blocked before impending bypass. Fuel feed tank sensor indicates low fuel. 100 ± 10 pounds of fuel remain in aft tank. Fuel valve is in transition or is not in the commanded position. Generator not connected to DC bus. An over temperature condition has been detected either under the pilot's seat, copilot's seat, or in the vertical tunnel. Low pressure in hydraulic system. Left fuel boost pump has failed. Left fuel transfer pump has failed. Litter door is not securely latched. MGT is in exceedance. MGT miscompare event. Engine Ng is in exceedance. Ng miscompare event. Engine NP is in exceedance. NP miscompare event. NR miscompare event. Pedal stop check or failed to engage or disengage upon command. Or, loss of ADC inputs. Engine torque is in exceedance. Audio Alert Single Ping 190-01255-00 Rev. A Garmin G1000H™ Pilot's Guide for the Bell 407GX 91

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

Match case Limit results 1 per page

190-01255-00

Rev. A

Garmin G1000H

™

Pilot’s Guide for the Bell 407GX

ENGINE INDICATION & CREW ALERTING SYSTEM

NOTE:

See the Rotorcraft Flight Manual (RFM) for recommended pilot actions.

Annunciation Text

Description

Audio Alert

BATTERY HOT

Battery overheat detected.

Single Chime

ENGINE FIRE

Fire/Overheat detector senses a temperature greater than or equal to 338°F.

Continuous Chime

ENGINE OUT

Ng less than 55% or FADEC senses engine out.

Continuous Fast-Pulsing Chime

ENGINE OVSPD

Ng greater than 110% or NP vs torque is above maximum continuous limit.

Single Chime

FADEC FAIL

Both the primary and reversionary channels have failed.

Repeating Ding-Dong Chime

XMSN OIL PRESS

Transmission oil pressure is low.

Single Chime

XMSN OIL TEMP

Transmission oil overheat is detected.

Single Chime

Table 3-1

Warning CAS Messages

Annunciation Text

Description

Audio Alert

BAGGAGE DOOR

Baggage door is not securely latched.

Single Ping

BATTERY RLY

Battery relay energized when battery switch is off.

Battery still connected to DC bus.

ENGINE CHIP

Chip detector has detected debris in engine oil.

FADEC DEGRADED

FADEC fault detected that may result in degraded engine performance.

FADEC FAULT

A fault is recorded in the FADEC.

FADEC MANUAL

FADEC is in manual mode.

FLOAT ARM

Floats Arm switch is in the armed position.

FUEL FILTER

External fuel ﬁlter is partially blocked before impending bypass.

FUEL LOW

Fuel feed tank sensor indicates low fuel.

100 ± 10 pounds of fuel remain in aft tank.

FUEL VALVE

Fuel valve is in transition or is not in the commanded position.

GEN FAIL

Generator not connected to DC bus.

HEATER OVERTMP

An over temperature condition has been detected either under the pilot’s seat, copilot’s seat, or

in the vertical tunnel.

HYDRAULIC SYS

Low pressure in hydraulic system.

L/FUEL BOOST

Left fuel boost pump has failed.

L/FUEL XFR

Left fuel transfer pump has failed.

LITTER DOOR

Litter door is not securely latched.

MGT EXCEED

MGT is in exceedance.

MGT MISCOMP

MGT miscompare event.

NG EXCEED

Engine Ng is in exceedance.

NG MISCOMP

Ng miscompare event.

NP EXCEED

Engine NP is in exceedance.

NP MISCOMP

NP miscompare event.

NR MISCOMP

NR miscompare event.

PEDAL STOP

Pedal stop check or failed to engage or disengage upon command.

Or, loss of ADC inputs.

Q EXCEED

Engine torque is in exceedance.