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Garmin G1000 Cockpit Reference Guide for the DA40/40F
190-00324-07 Rev. A
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-1
SECTION 6: AUTOMATIC FLIGHT
CONTROL
The GFC 700 AFCS is optional on the DA40 and
DA40F. In aircraft without the GFC 700 option, refer
to the operating instructions for the installed autopilot
system for details.
6.1 AFCS CONTROLS
The following dedicated AFCS keys are located on the
bezels of the MFD:
Figure 6-1 AFCS Keys
In addition to the AFCS (Automatic Flight Control
System) keys on the MFD, as discussed in the System
Overview section, the following buttons and switches
used by the AFCS are located in the cockpit separately
from the PFD and MFD.
• AP DISC (Autopilot Disconnect) Button —
Located on the left and right control sticks, pressing
this button disengages the autopilot. Pressing it also
acknowledges an autopilot disconnect.
• CWS (Control Wheel Steering) Button —
Located on the left and right control sticks, pressing
and holding the CWS button disengages the control
surface servos without disengaging the autopilot. If
the flight director has not been activated, pressing
the CWS button will activate the flight director in
the default pitch and roll hold modes.
• GA (Go Around) Button — Located on the throttle
lever, the GA button disengages the autopilot and
selects the Go Around (wings level) mode.
• AP TRIM (Autopilot Trim) Switch — Located on
the left control stick, this switch is used to operate
manual electric pitch trim. Moving both switches
forward simultaneously trims the aircraft nose down.
Moving both switches aft simultaneously trims the
aircraft nose up. The left switch is the ARM contact
and the right switch controls the up/down trim.
Pressing the ARM switch disengages the autopilot, if
currently engaged. If one side of the switch is active
for more than three seconds without the other side
also being active, ‘PTRM’ is displayed in the AFCS
System Status Box on the PFD. Pressing the ARM
switch also acknowledges an autopilot disconnect.
6.2 FLIGHT DIRECTOR OPERATION
With the flight director activated, the aircraft can be
hand-flown to follow the path shown by the Command
Bars. Maximum commanded pitch (+20°/-15°) and bank
(22°) angles, vertical acceleration, and roll rate are limited
to values established during AFCS certification. The flight
director also provides commands to the autopilot.
- 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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