Garmin Software Version 0369.13 Guide de l'utilisateur Page 65
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- Table des matières
- MARQUE LIVRES
Noté. / 5. Basé sur avis des utilisateurs
Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-07 Rev. A
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-7
If the Selected Altitude is reached during CWS
maneuvering, the Altitude Reference is not changed.
To adjust the Altitude Reference in this case, the CWS
Button must be pressed again after the Selected Altitude
is reached.
Figure 6-7 Altitude Hold Mode
Altitude Hold
Mode Active
Flight Director
Altitude Reference
Selected Altitude
Selected Altitude Bug
Command Bars Hold
Pitch Attitude to
Maintain Altitude
Reference
Vertical Speed Mode (VS)
In Vertical Speed Mode, the flight director acquires
and maintains a Vertical Speed Reference. Current aircraft
vertical speed (to the nearest 100 fpm) becomes the
Vertical Speed Reference at the moment of Vertical Speed
Mode activation. Vertical Speed Mode does not consider
the relative position of the Selected Altitude in relation to
the current aircraft altitude at the time of mode activation,
so it is possible to use Vertical Speed Mode while not
climbing/descending to the Selected Altitude.
Vertical Speed Mode is activated by pressing the
VS
Key; the ‘VS’ annunciation appears in the AFCS Status Box
to indicate the active pitch mode, along with the Vertical
Speed Reference to the right. The Vertical Speed Reference
is also displayed above the Vertical Speed Indicator. A
Vertical Speed Reference Bug corresponding to the Vertical
Speed Reference is shown on the indicator.
- 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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