Garmin Software Version 0500.00 Guía de usuario Pagina 97
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Garmin G1000 Cockpit Reference Guide for the Beechcraft 58/G58
10-13
SECTION 10 – HAZARD
AVOIDANCE
AGL while within 1 nm of the threshold. During
the final descent, algorithms will set a threshold
for alerting based on speed, distance, and other
parameters.
• Non-Precision Approach Loaded - PDA alerting
begins when the FAF is the active waypoint AND the
aircraft is within 15 nm of the destination airport.
Again, algorithms are used to set a threshold for
alerting based upon various parameters. PDA
alerting ends at 0.5 nm from the runway threshold
OR at an altitude of 125 feet AGL while within 1
nm of the threshold.
• ILS Approach Loaded—PDA alerting begins when
the FAF is the active waypoint AND the aircraft is
within 15 nm of the destination airport. Prior to
reaching the FAF, a PDA alert will be issued if the
aircraft descends 200 feet below the FAF altitude.
Once the aircraft intercepts the glideslope, PDA will
alert the pilot if the aircraft descends 0.7 degrees
below the glideslope. PDA alerting ends 0.5 nm
from the runway threshold OR at an altitude of 125
feet AGL while within 1 nm of the threshold.
0
.
5
n
m
Runway Threshold
Final Approach Fix
2
0
0
'
b
e
l
o
w
F
A
F
A
l
t
i
t
u
d
e
1
5
n
m
C
A
U
T
I
O
N
Figure 10-20 Non-Precision Approach PDA Alert Threshold
Runway Threshold
Final Approach Fix
2
0
0
'
b
e
l
o
w
F
A
F
A
l
t
i
t
u
d
e
1
5
n
m
C
A
U
T
I
O
N
PDA Alert is
0.7 Below Glideslope
Glideslope Intercept
0
.
5
n
m
Figure 10-21 ILS Approach PDA Alert Threshold
Excessive Descent Rate Alert (EDR)
The purpose of the Excessive Descent Rate alert is to
provide suitable alerts when the aircraft is determined
to be closing (descending) upon terrain at an excessive
speed. Figure 10-22 displays the correlation between
height above terrain and descent rate, resulting in the two
EDR alerts. EDR alerts have two levels of severity, caution
(sink rate) and warning (pull-up).
5000
4500
4000
3500
3000
2500
2000
1500
1000
500
0
2000 4000 6000 8000 10000 12000
"PULL UP""
P
U
L
L
U
P
"
"
S
I
N
K
R
A
T
E
"
Descent Rate (FPM)
Height Above Terrain (Feet)
Figure 10-22 Excessive Descent Rate
- Cockpit Reference Guide 1
- WARNINGS 4
- CAUTIONS, & NOTES 4
- RECORD OF REVISIONS 7
- Ground Mode (Automatic) 9
- Reply Status 9
- Code Selection 9
- Navigation Mode Armed 9
- TABLE OF CONTENTS 10
- SECTION 1: SYSTEM OVERVIEW 13
- 1.1 PFD/MFD CONTROLS 14
- SECTION 1 15
- SYSTEM OVERVIEW 15
- 1.2 PFD SOFTKEYS 16
- 1.3 MFD SOFTKEYS 19
- 1.4 MFD PAGE GROUPS 20
- 1.5 BACKLIGHTING 20
- SECTION 2: FLIGHT INSTRUMENTS 21
- SECTION 2 22
- FLIGHT INSTRUMENTS 22
- 2.1 AIRSPEED INDICATOR 23
- 2.2 ATTITUDE INDICATOR 23
- 2.3 ALTIMETER 24
- INDICATOR 24
- 2.6 VERTICAL SPEED INDICATOR 25
- Course Pointer 26
- DME Radio (optional) 27
- Navigation Source 27
- SECTION 3: ENGINE INDICATION 29
- SYSTEM (EIS) 29
- 3.3 ENGINE SYSTEM DISPLAY 30
- SECTION 4: NAV/COM AND 31
- TRANSPONDER 31
- SECTION 4 – NAV/COM & 32
- 4.1 RADIO STATUS INDICATIONS 33
- 4.2 VOLUME 33
- 4.3 AUTOMATIC SQUELCH 33
- 4.5 OPTIONAL NAV RADIOS 33
- 4.6 FREQUENCY AUTO-TUNING 34
- 4.7 TRANSPONDER 34
- Flight ID Reporting 35
- SECTION 5: AUDIO PANEL 37
- 5.1 COM RADIO SELECTION 38
- 5.2 MARKER BEACON RECEIVER 38
- 5.5 INTERCOM SQUELCH CONTROL 39
- WITH PLAYBACK CAPABILITY 40
- SECTION 6: AUTOMATIC FLIGHT 41
- 6.2 OVERSPEED PROTECTION 42
- 6.4 LOSS OF DATA 43
- 6.5 PITCH AXIS MODES 43
- Pitch Hold Mode (PIT) 44
- Altitude Hold Mode (ALT) 45
- Vertical Speed Mode (VS) 46
- SECTION 6 – AUTOMATIC 47
- FLIGHT CONTROL 47
- Go-Around Mode (GA) 48
- Glideslope (GS) 48
- 6.6 ROLL AXIS MODES 49
- Heading Select Mode (HDG) 50
- Go Around (GA) 52
- Departure 54
- Intercepting a VOR Radial 55
- Flight Level Change (Descent) 57
- ILS Approach 58
- Go-Around / Missed Approach 59
- SECTION 7: NAVIGATION 61
- SECTION 7 – NAVIGATION 62
- 7.3 AIRPORT INFORMATION 63
- 7.4 INTERSECTION INFORMATION 64
- 7.5 NDB INFORMATION 64
- 7.6 VOR INFORMATION 65
- 7.8 NEAREST AIRPORTS 65
- 7.9 NEAREST INTERSECTIONS 66
- 7.10 NEAREST NDB 67
- 7.11 NEAREST VOR 67
- 7.12 NEAREST USER WAYPOINT 68
- 7.13 NEAREST FREQUENCIES 68
- 7.14 NEAREST AIRSPACES 69
- SECTION 8: FLIGHT PLANNING 71
- Modify a User Waypoint 72
- Delete a User Waypoint 72
- 8.7 CREATE A NEW FLIGHT PLAN 73
- 8.8 LOAD A DEPARTURE 74
- 8.9 LOAD AN ARRIVAL 74
- 8.10 LOAD AN APPROACH 74
- SECTION 8 – FLIGHT PLANNING 75
- 8.16 COPY A FLIGHT PLAN 76
- 8.17 DELETE A FLIGHT PLAN 76
- 8.19 TRIP PLANNING 76
- VNAV Page Menu Options 79
- SECTION 9: PROCEDURES 81
- 9.2 APPROACHES 82
- SECTION 9 – PROCEDURES 83
- SECTION 10: HAZARD AVOIDANCE 85
- Stormscope Page 86
- 10.3 XM WEATHER (OPTIONAL) 87
- Weather Products and Symbols 89
- Weather Product Age 90
- TIS Audio Alert 91
- SYSTEM (TAS)(OPTIONAL) 92
- Proximity Page 93
- Navigation Map 93
- SYSTEM (TAWS) DISPLAY 94
- (OPTIONAL) 94
- Enable/Disable Aviation Data 95
- TAWS Inhibit 96
- Manual System Test 96
- Premature Descent Alert (PDA) 96
- "PULL UP"" 97
- Alert (NCR) 98
- “Five-Hundred” Aural Alert 98
- Pop-up Alerts 99
- TAWS Alerts Summary 100
- Alert Annunciations 101
- 10.8 AIRBORNE WEATHER RADAR 102
- Vertically Scan a Storm Cell 103
- Adjusting Gain 104
- Ground Mapping 104
- Sector Scan 104
- Antenna Stabilization 105
- SECTION 10 – HAZARD 106
- AVOIDANCE 106
- SECTION 11: ABNORMAL 107
- OPERATION 107
- 11.2 ABNORMAL COM OPERATION 108
- 11.3 UNUSUAL ATTITUDES 108
- LOSS OF HEADING INPUT 108
- SECTION 12 – ANNUNCIATIONS 109
- & ALERTS 109
- 12.1 ALERT LEVEL DEFINITIONS 110
- WARNING Annunciation 111
- CAUTION Annunciation 111
- ADVISORY Annunciation 111
- Alert Message 111
- 12.3 AFCS ALERTS 112
- 12.4 TAWS ALERTS 113
- Traffic Voice Alerts 114
- MFD & PFD Alert Messages 117
- Database Alert Messages 118
- GMA 1347 Alert Messages 119
- GIA 63 Alert Messages 119
- GIA 63 Alert Messages (Cont.) 120
- GEA 71 Alert Messages 121
- GTX 33 Alert Messages 122
- GRS 77 Alert Messages 122
- GMU 44 Alert Messages 123
- GDL 69 Alert Messages 123
- GDC 74A Alert Messages 123
- GWX 68 Alert Messages 123
- Miscellaneous Alert Messages 124
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