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Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-11 Rev. C
86
Additional Features
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
4) Press the
FMS
Knob to activate the cursor.
5) Turn the large
FMS
Knob to place the cursor in the STABILITY & PROTECTION
field.
6) Turn the small
FMS
Knob to select ‘ENABLE’ or ‘DISABLE’.
7) Press the
FMS
Knob to remove the cursor.
ESP
™
is automatically enabled on system power up.
Roll Engagement
Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating
where ESP
™
will engage. As roll attitude exceeds 45°, ESP
™
will engage and the on-side
Roll Limit Indicator will move to 30°. The Roll Limit Indicator is now showing where
ESP
™
will disengage as roll attitude decreases to within the desirable roll attitude range.
Once engaged, ESP
™
force will be applied between 30° and 75°. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force is
intended to encourage pilot input that returns the airplane to a more normal roll at-
titude. As roll attitude decreases, ESP
™
will disengage at 30°
Pitch Engagement
ESP
™
engages at 15° nose-up and 18° nose-down. Once ESP
™
is engaged, it will
apply increasing opposing force between 15° and 20° nose-up and between 18° and
23° nose-down. Maximum opposing force is applied between 20° and 50° nose-up and
between 23° and 50° nose-down. ESP
™
disengages when 50° is exceeded in a nose-up
or nose-down attitude.
With ESP
™
engaged, and the aircraft in a nose-up condition, opposing force steadily
decreases from 20° nose-up to 10° nose-up as aircraft pitch moves toward zero degrees.
ESP
™
disengages at 10° nose-up. With ESP
™
engaged, and the aircraft in a nose-down
condition, opposing force steadily decreases from 23° nose-down to 13° nose-down as
aircraft pitch moves toward zero degrees. ESP
™
disengages at 13° nose-down.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch axis
in the direction of the normal pitch attitude range for the aircraft.
There are no indications marking the pitch ESP
™
engage and disengage limits in these
nose-up/nose-down conditions.
High Airspeed Protection
Exceeding Vne will result in ESP
™
applying force to raise the nose of the aircraft.
When the high airspeed condition is remedied, ESP
™
force is no longer applied.
- Integrated Flight Deck 1
- 190-00324-11 Rev. C 10
- Record of Revisions 11
- 190-00324-11 Rev. C i 13
- Table of Contents 14
- FLIGHT INSTRUMENTS 17
- 190-00324-11 Rev. C 3 19
- Flight Instruments 20
- ENGINE INDICATION SYSTEM 21
- Engine Indication System 22
- DA40 ENGINE DISPLAY 22
- DA40F ENGINE DISPLAY 23
- ENGINE LEANING 24
- Nav/Com/XPDR/Audio Panel 27
- ENTER OR CHANGE FLIGHT ID 27
- ADF TUNING (OPTIONAL) 27
- DME TUNING (OPTIONAL) 27
- FLIGHT DIRECTOR ACTIVATION 31
- VERTICAL MODES 32
- LATERAL MODES 33
- GPS NAVIGATION 35
- GPS Navigation 36
- ACTIVATE A STORED FLIGHT PLAN 36
- ACTIVATE A FLIGHT PLAN LEG 36
- STOP NAVIGATING A FLIGHT PLAN 37
- VERTICAL NAVIGATION (VNAV) 37
- FLIGHT PLANNING 41
- Flight Planning 42
- ANOTHER WAYPOINT 45
- DELETE A USER WAYPOINT 46
- CREATE A FLIGHT PLAN 47
- INVERT AN ACTIVE FLIGHT PLAN 50
- STORE A FLIGHT PLAN 51
- EDIT A STORED FLIGHT PLAN 51
- COPY A FLIGHT PLAN 52
- DELETE A FLIGHT PLAN 52
- PROCEDURES 55
- Procedures 56
- ACTIVATE AN ARRIVAL LEG 56
- HAZARD AVOIDANCE 59
- 190-00324-11 Rev. C 45 61
- Hazard Avoidance 62
- Displaying TFR Data: 62
- WORLDWIDE WEATHER (OPTIONAL) 64
- GFDS Weather Data Requests 69
- WORLDWIDE WEATHER PRODUCTS 72
- Precipitation 72
- Precipitation Limitations 73
- Infrared Satellite 73
- Data Link Lightning 73
- SIGMETs and AIRMETs 74
- METARs and TAFs 74
- Displaying PIREP text 75
- Winds Aloft 76
- Displaying Winds Aloft data 76
- TRAFFIC SYSTEMS 76
- TERRAIN-SVS 79
- Enable/Disable Aviation Data 80
- Terrain-SVS Inhibit 80
- Manual System Test 81
- TAWS Inhibit 82
- ADDITIONAL FEATURES 83
- , ChartView, or FliteCharts 84
- , it may 84
- ChartView 85
- FliteCharts 85
- Change Day/Night View 86
- AOPA AIRPORT DIRECTORY 86
- 190-00324-11 Rev. C 71 87
- 190-00324-11 Rev. C 73 89
- Incoming Calls 90
- Answering an incoming call: 91
- Outgoing Calls 91
- To make a call: 91
- Text Messaging (SMS) 92
- Reply to a Text Message 94
- Sending a Text Message 94
- Predefined Text Messages 95
- Send a Predefined Text Message 96
- Text Message Boxes 96
- Show Inbox Messages 96
- Show Outbox Messages 97
- Show Draft Messages 97
- Arranging Text Messages 97
- Mark Selected Message As Read 99
- Mark All Messages As Read 99
- Delete a Message 99
- Additional Features 100
- ) (OPTIONAL) 101
- Roll Engagement 102
- Pitch Engagement 102
- High Airspeed Protection 102
- AUXILIARY VIDEO (OPTIONAL) 103
- Video Setup 103
- Display Selection 104
- Zoom/Range 104
- ABNORMAL OPERATION 105
- Abnormal Operation 106
- UNUSUAL ATTITUDES 106
- DEAD RECKONING 106
- ANNUNCIATIONS & ALERTS 109
- Annunciations & Alerts 110
- ALERT MESSAGE 110
- AFCS ALERTS 111
- TERRAIN-SVS ALERTS 112
- TAWS ALERTS 113
- VOICE ALERTS 115
- DATABASE MESSAGE ADVISORIES 116
- GMA 1347 MESSAGE ADVISORIES 120
- GIA 63 MESSAGE ADVISORIES 120
- GEA 71 MESSAGE ADVISORIES 126
- GTX 33 MESSAGE ADVISORIES 127
- GRS 77 MESSAGE ADVISORIES 127
- GSR 56 MESSAGE ADVISORIES 128
- GMU 44 MESSAGE ADVISORIES 128
- GDC 74A MESSAGE ADVISORIES 128
- GDL 69A MESSAGE ADVISORIES 129
- APPENDIX 135
- Appendix 136
- , and ADF/ 138
- , and ADF/frequency 138
- MFD SOFTKEY MAP 140
- LOADING UPDATED DATABASES 142
- Database 144
- 190-00324-11 Rev. C 147
- Blank Page 150
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