Garmin Software Version 0369.13 Guide de l'utilisateur Page 70
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Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-07 Rev. A
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-12
When a descent leg is captured (Figure 6-12), Vertical
Path Tracking becomes active and tracks the descent pro-
file. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed
as appropriate.
Figure 6-12 Vertical Path Tracking Mode
VNAV Target Altitude Capture ArmedVertical Path Tracking Active
VNAV
Target
Altitude
Vertical
Deviation
Indicator
Required
Vertical
Speed Bug
HSI Set to GPS
Terminal
Phase of
Flight
Automatic Pitch Hold Reversion
Several situations can occur while Vertical Path
Tracking Mode is active which cause the flight director to
revert to Pitch Hold Mode. Vertical Path Tracking and the
appropriate altitude capture modes are armed for possible
descent profile recapture if the vertical deviation:
• Exceeds 200 ft during an overspeed condition
• Experiences a discontinuity exceeding 200 ft due to
a flight plan change
• Becomes invalid due to excessive cross-track error,
track angle error
• Cannot be computed for a leg type (such as a hold
or procedure turn)
The following circumstances cause mode reversion
without arming Vertical Path Tracking Mode:
• Navigation source manually changed from GPS
• CNCL VNV Softkey selected on the Active Flight
Plan Page (MFD)
• All remaining vertical waypoints deleted from the
flight plan
• Displays entering Reversionary Mode
Non-Path Descents
Pitch Hold, Vertical Speed, and Flight Level Change
modes can also be used to fly non-path descents while
- DA40/40F 1
- WARNINGS 6
- CAUTIONS, & NOTES 6
- RECORD OF REVISIONS 10
- TABLE OF CONTENTS 12
- SECTION 1: SYSTEM OVERVIEW 15
- 1.1 PFD/MFD CONTROLS 16
- SECTION 1 17
- SYSTEM OVERVIEW 17
- ADF/DME 21
- 1.3 MFD SOFTKEYS 22
- 1.4 MFD PAGE GROUPS 23
- 1.5 VERTICAL NAVIGATION 24
- 1.6 BACKLIGHTING 26
- 1.8 DATABASE UPDATES 26
- Garmin Databases 27
- SECTION 2: FLIGHT INSTRUMENTS 29
- SECTION 2 30
- FLIGHT INSTRUMENTS 30
- 2.1 AIRSPEED INDICATOR 31
- 2.2 ATTITUDE INDICATOR 31
- 2.3 ALTIMETER 32
- Metric Display 33
- GLIDESLOPE INDICATOR 34
- 2.6 VERTICAL SPEED INDICATOR 35
- Course Pointer 37
- DME (optional) 39
- Navigation Source 39
- 2.9 WIND DATA 40
- 2.10 GENERIC TIMER 41
- SECTION 3: ENGINE INDICATION 43
- SYSTEM (EIS) 43
- 3.1 DA40 ENGINE DISPLAY 44
- 3.2 DA40F ENGINE DISPLAY 45
- 3.3 ENGINE LEANING 46
- SECTION 3 – ENGINE 47
- INDICATION SYSTEM (EIS) 47
- SECTION 4: NAV/COM AND 49
- TRANSPONDER 49
- SECTION 4 – NAV/COM & 50
- 4.1 RADIO STATUS INDICATIONS 51
- 4.2 VOLUME 51
- 4.3 AUTOMATIC SQUELCH 51
- 4.5 OPTIONAL NAV RADIOS 51
- 4.6 FREQUENCY AUTO-TUNING 52
- 4.7 TRANSPONDER 52
- Reply Status 53
- Code Selection 53
- Flight ID Reporting 54
- SECTION 5: AUDIO PANEL 55
- 5.1 COM RADIO SELECTION 56
- 5.2 MARKER BEACON RECEIVER 56
- 5.5 INTERCOM SQUELCH CONTROL 57
- AND PLAYER 58
- SECTION 6: AUTOMATIC FLIGHT 59
- Command Bars 60
- 6.3 FLIGHT DIRECTOR MODES 61
- SECTION 6 – AUTOMATIC 62
- FLIGHT CONTROL 62
- Roll Modes 74
- Course and deviation 77
- 6.4 AUTOPILOT OPERATION 79
- Disengaging the Autopilot 80
- Departure 82
- Intercepting a VOR Radial 83
- Approach 88
- Go Around/Missed Approach 90
- AFCS Status Alerts 91
- Overspeed Protection 92
- SECTION 7: NAVIGATION 93
- SECTION 7 – NAVIGATION 100
- 7.4 AIRPORT INFORMATION 113
- 7.5 INTERSECTION INFORMATION 115
- 7.6 NDB INFORMATION 116
- 7.7 VOR INFORMATION 116
- 7.9 NEAREST AIRPORTS 117
- 7.10 NEAREST INTERSECTIONS 118
- 7.11 NEAREST NDB 119
- 7.12 NEAREST VOR 119
- 7.13 NEAREST USER WAYPOINT 120
- 7.14 NEAREST FREQUENCIES 120
- 7.15 NEAREST AIRSPACES 121
- SECTION 8: FLIGHT PLANNING 123
- Map Page 124
- SECTION 8 – FLIGHT PLANNING 125
- 8.7 CREATE A NEW FLIGHT PLAN 126
- 8.17 COPY A FLIGHT PLAN 130
- 8.18 DELETE A FLIGHT PLAN 130
- 8.20 TRIP PLANNING 130
- SECTION 9: PROCEDURES 133
- 9.2 APPROACHES 134
- SECTION 9 – PROCEDURES 135
- SECTION 10: HAZARD AVOIDANCE 137
- Stormscope Page 138
- 10.3 XM WEATHER (OPTIONAL) 139
- SECTION 10 – HAZARD 140
- AVOIDANCE 140
- Weather Products and Symbols 141
- Weather Product Age 142
- TIS Audio Alert 143
- 10.5 AVIDYNE 144
- TAS600 SERIES 144
- Proximity Page 145
- Navigation Map 145
- SYSTEM (TAWS) DISPLAY 146
- (OPTIONAL) 146
- Enable/Disable Aviation Data 147
- TAWS Inhibit 148
- Manual System Test 148
- Premature Descent Alert (PDA) 149
- Alert (NCR) 149
- “Five-Hundred” Aural Alert 150
- Pop-up Alerts 150
- TAWS Alerts Summary 151
- Alert Annunciations 152
- SECTION 11: ABNORMAL 153
- OPERATION 153
- SECTION 11 – ABNORMAL 154
- 11.6 DEAD RECKONING 155
- SECTION 12 – ANNUNCIATIONS 157
- & ALERTS 157
- 12.1 ALERT LEVEL DEFINITIONS 158
- 12.2 AIRCRAFT ALERTS 159
- 12.4 AFCS ALERTS 160
- 12.5 TAWS ALERTS 161
- Database Message Advisories 166
- GMA 1347 Message Advisories 168
- GIA 63 Message Advisories 168
- GIA 63W Message Advisories 171
- GEA 71 Message Advisories 173
- GTX 33 Message Advisories 174
- GRS 77 Message Advisories 174
- GMU 44 Message Advisories 175
- GDL 69A Message Advisories 175
- GDC 74A Message Advisories 175
- 190-00324-07 Rev. A 184
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