Garmin Software Version 0369.13 Guide de l'utilisateur Page 78
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Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-07 Rev. A
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-20
When the CDI has automatically switched from GPS to
LOC during a LOC/ILS approach, GPS Navigation Mode
remains active, providing GPS steering guidance until
the localizer signal is captured. LOC Navigation Mode is
armed in anticipation of localizer signal capture if the APR
Key is not pressed prior to the automatic source switch.
If Navigation Mode is active and either of the following
occur, the flight director reverts to Roll Hold Mode (wings
rolled level):
• Different VOR is tuned while in VOR Navigation
Mode (VOR Navigation Mode reverts to armed)
• Navigation source is manually switched
• Localizer signal is not captured by the final approach
fix (FAF) while in LOC Navigation Mode
Changing the Selected Course
The Selected Course on the PFD is controlled using the
CRS Knob. Pressing the CWS Button and hand-flying
the aircraft does not change the Selected Course while in
Navigation Mode. The autopilot guides the aircraft back
to the Selected Course (or GPS flight plan) when the CWS
Button is released.
Approach Mode (GPS, VAPP, LOC)
NOTE: The selected navigation receiver must have
a valid VOR or LOC signal or active GPS course
for the flight director to enter Approach Mode.
Approach Mode is activated when the APR Key is
pressed. Approach Mode acquires and tracks the selected
navigation receiver on the HSI (GPS, VOR, or LOC),
depending on the loaded approach. This mode uses the
selected navigation receiver deviation and desired course
inputs to fly the approach. Approach Mode provides
greater sensitivity for signal tracking than Navigation
Mode.
Pressing the APR Key when the CDI is greater than
one dot arms the selected approach mode (annunciated
in white to the left of the active roll mode). If the selected
navigation receiver is GPS, pressing the
APR Key arms
GPS Approach Mode, provided that a GPS approach has
been loaded into the flight plan. If the loaded approach
provides WAAS-based vertical guidance, Glidepath Mode
is also armed (Figure 6-16). If GPS Approach Mode is
selected while in GPS Navigation Mode, capture can occur
with crosstrack error of up to 2 nm.
Figure 6-24 GPS Approach Mode Armed
LOC Approach Mode allows the autopilot to fly a LOC/
ILS approach with a glideslope. LOC Approach Mode is
armed (along with Glideslope Mode; see Figure 6-17)
when the APR Key is pressed and either of the following
have been done:
• Navigation source is set to LOC
• A LOC/ILS approach is loaded into the flight plan
and the corresponding localizer frequency tuned
(even if the selected navigation source is GPS)
Localizer capture is suppressed until the navigation
source is changed to LOC.
If Approach Mode is active and either of the following
occur, the flight director reverts to Roll Hold Mode (wings
rolled level):
• Vectors-to-Final is activated
• Navigation source is manually switched
• Localizer signal is not captured by the final approach
fix (FAF) while in LOC Navigation Mode
Changing the Selected Course
The Selected Course on the PFD is controlled using the
CRS Knob. Pressing the CWS Button and hand-flying
the aircraft does not change the Selected Course while in
Approach Mode. The autopilot guides the aircraft back to
the Selected Course (or GPS flight plan) when the CWS
Button is released.
- 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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