Garmin G600 Pilots Guide - Page 132

Terrain Alerts

Page 132 highlights

Foreword System Sec 1 PFD Sec 2 MFD Sec 3 Features Avoidance Hazard Sec 4 Additional Sec 5 4.1.2 Terrain Alerts TERRAIN uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS altitude is derived from satellite measurements. GPS altitude is converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used to determine TERRAIN alerts. GPS-MSL altitude accuracy is affected by factors such as satellite geometry, but it is not subject to variations in pressure and temperature that normally affect pressure altitude devices. GPS-MSL altitude does not require local altimeter settings to determine MSL altitude. Therefore, GPS altitude provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts. TERRAIN utilizes terrain and obstacle databases that are referenced to mean sea level (MSL). Using the GPS position and GPS-MSL altitude, TERRAIN displays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. Furthermore, the GPS position and GPS-MSL altitude are used to calculate and "predict" the aircraft's flight path in relation to the surrounding terrain and obstacles. In this manner, TERRAIN can provide advanced alerts of predicted dangerous terrain conditions. Detailed alert modes are described in Section 6. A TAWS warning received from the GNS 500W Series TAWS units will be displayed above the Altitude Tape. A new warning will flash for approximately five seconds. TAWS Annunciation Description TERRAIN has been inhibited by flight crew TAWS not available Excessive Descent Rate Caution Excessive Descent Rate Warning Forward Looking Terrain Avoidance Caution for Terrain Forward Looking Terrain Avoidance Warning for Terrain Forward Looking Terrain Avoidance Caution for Obstacle Forward Looking Terrain Avoidance Warning for Obstacle & Alerts Annun. Sec 6 Symbols Sec 7 Appendix A Glossary Sec 8 Index Appendix B 4-6 Garmin G600 Pilot's Guide 190-00601-02 Rev. B

  • 1
  • 2
  • 3
  • 4
  • 5
  • 6
  • 7
  • 8
  • 9
  • 10
  • 11
  • 12
  • 13
  • 14
  • 15
  • 16
  • 17
  • 18
  • 19
  • 20
  • 21
  • 22
  • 23
  • 24
  • 25
  • 26
  • 27
  • 28
  • 29
  • 30
  • 31
  • 32
  • 33
  • 34
  • 35
  • 36
  • 37
  • 38
  • 39
  • 40
  • 41
  • 42
  • 43
  • 44
  • 45
  • 46
  • 47
  • 48
  • 49
  • 50
  • 51
  • 52
  • 53
  • 54
  • 55
  • 56
  • 57
  • 58
  • 59
  • 60
  • 61
  • 62
  • 63
  • 64
  • 65
  • 66
  • 67
  • 68
  • 69
  • 70
  • 71
  • 72
  • 73
  • 74
  • 75
  • 76
  • 77
  • 78
  • 79
  • 80
  • 81
  • 82
  • 83
  • 84
  • 85
  • 86
  • 87
  • 88
  • 89
  • 90
  • 91
  • 92
  • 93
  • 94
  • 95
  • 96
  • 97
  • 98
  • 99
  • 100
  • 101
  • 102
  • 103
  • 104
  • 105
  • 106
  • 107
  • 108
  • 109
  • 110
  • 111
  • 112
  • 113
  • 114
  • 115
  • 116
  • 117
  • 118
  • 119
  • 120
  • 121
  • 122
  • 123
  • 124
  • 125
  • 126
  • 127
  • 128
  • 129
  • 130
  • 131
  • 132
  • 133
  • 134
  • 135
  • 136
  • 137
  • 138
  • 139
  • 140
  • 141
  • 142
  • 143
  • 144
  • 145
  • 146
  • 147
  • 148
  • 149
  • 150
  • 151
  • 152
  • 153
  • 154
  • 155
  • 156
  • 157
  • 158
  • 159
  • 160
  • 161
  • 162
  • 163
  • 164
  • 165
  • 166
  • 167
  • 168
  • 169
  • 170
  • 171
  • 172
  • 173
  • 174
  • 175
  • 176
  • 177
  • 178
  • 179
  • 180
  • 181
  • 182
  • 183
  • 184
  • 185
  • 186
  • 187
  • 188
  • 189
  • 190
  • 191
  • 192
  • 193
  • 194
  • 195
  • 196
  • 197
  • 198
  • 199
  • 200
  • 201
  • 202
  • 203
  • 204
  • 205
  • 206
  • 207
  • 208
  • 209
  • 210
  • 211
  • 212
  • 213
  • 214
  • 215
  • 216
  • 217
  • 218
  • 219
  • 220
  • 221
  • 222
  • 223
  • 224
  • 225
  • 226
  • 227
  • 228
  • 229
  • 230
  • 231
  • 232
  • 233
  • 234
  • 235
  • 236
  • 237
  • 238
  • 239
  • 240

4-6
Garmin G600 Pilot’s Guide
190-00601-02
Rev. B
Foreword
Sec 1
System
Sec 2
PFD
Sec 3
MFD
Sec 4
Hazard
Avoidance
Sec 5
Additional
Features
Sec 6
Annun.
& Alerts
Sec 7
Symbols
Sec 8
Glossary
Appendix A
Appendix B
Index
4.1.2
Terrain Alerts
TERRAIN uses information provided from the GPS receiver to provide
a horizontal position and altitude. GPS altitude is derived from satellite
measurements. GPS altitude is converted to a mean sea level (MSL)-based
altitude (GPS-MSL altitude) and is used to determine TERRAIN alerts. GPS-MSL
altitude accuracy is affected by factors such as satellite geometry, but it is not
subject to variations in pressure and temperature that normally affect pressure
altitude devices. GPS-MSL altitude does not require local altimeter settings to
determine MSL altitude. Therefore, GPS altitude provides a highly accurate and
reliable MSL altitude source to calculate terrain and obstacle alerts.
TERRAIN utilizes terrain and obstacle databases that are referenced to mean
sea level (MSL). Using the GPS position and GPS-MSL altitude, TERRAIN
displays a 2-D picture of the surrounding terrain and obstacles relative to the
position and altitude of the aircraft. Furthermore, the GPS position and GPS-MSL
altitude are used to calculate and “predict” the aircraft’s flight path in relation
to the surrounding terrain and obstacles. In this manner, TERRAIN can provide
advanced alerts of predicted dangerous terrain conditions. Detailed alert modes
are described in Section 6.
A TAWS warning received from the GNS 500W Series TAWS units will be
displayed above the Altitude Tape. A new warning will flash for approximately
five seconds.
TAWS Annunciation
Description
TERRAIN has been inhibited by flight crew
TAWS not available
Excessive Descent Rate Caution
Excessive Descent Rate Warning
Forward Looking Terrain Avoidance
Caution for Terrain
Forward Looking Terrain Avoidance
Warning for Terrain
Forward Looking Terrain Avoidance
Caution for Obstacle
Forward Looking Terrain Avoidance
Warning for Obstacle