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Garmin G1000 Cockpit Reference Guide for the DA42
190-00406-05 Rev. B
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-1
SECTION 6: AUTOMATIC FLIGHT
CONTROL
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 pilot’s control stick, pressing this
button disengages the autopilot. Pressing it also
acknowledges an autopilot disconnect.
• CWS (Control Wheel Steering) Button — Located
on the pilot’s control stick, 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
handle, the GA Button disengages the autopilot and
selects Go-around Mode.
• AP TRIM (Autopilot Trim) Switch — 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 field
on the PFD. Pressing the AP TRIM ARM Switch
also acknowledges an autopilot disconnect.
Figure 6-1 AFCS Keys
Pressing the FD Key activates only the flight director
in the default Pitch/Roll Hold modes without engaging the
autopilot. Pressing the AP Key activates the flight director
and yaw damper, and engages the autopilot. When
only the flight director is engaged, pressing the FD Key
disengages the flight director.
Upon activation of the autopilot and/or flight director,
command bars are displayed on the PFD. If the attitude
information being sent to the flight director becomes
invalid or unavailable, the command bars are removed
from the display.
Figure 6-2 Command Bars
6.1 MODE ANNUNCIATIONS
Mode annunciations are displayed on the PFD. Figure
6-3 shows the AFCS Status Box fields. Modes associated
with aircraft movement about the roll axis are displayed
on the left side. Modes associated with aircraft movement
about the pitch axis are displayed on the right. Armed
modes are displayed in white and active modes are
displayed in green.
- Integrated Flight Deck 1
- WARNINGS 4
- CAUTIONS, & NOTES 4
- RECORD OF REVISIONS 7
- TABLE OF CONTENTS 10
- SECTION 1: SYSTEM OVERVIEW 13
- 1.1 PFD/MFD CONTROLS 14
- SECTION 1 15
- SYSTEM OVERVIEW 15
- 1.4 MFD PAGE GROUPS 21
- 1.5 BACKLIGHTING 21
- 1.6 DATABASE UPDATES 22
- Power down the G1000 23
- SECTION 2: FLIGHT INSTRUMENTS 25
- SECTION 2 26
- FLIGHT INSTRUMENTS 26
- 2.1 AIRSPEED INDICATOR 27
- 2.2 ATTITUDE INDICATOR 27
- 2.3 ALTIMETER 28
- INDICATOR 29
- 2.6 VERTICAL SPEED INDICATOR 29
- Course Pointer 31
- DME (optional) 32
- Navigation Source 32
- SECTION 3: ENGINE INDICATION 33
- SYSTEM (EIS) 33
- 3.3 FUEL DISPLAY 34
- SECTION 4: NAV/COM AND 35
- TRANSPONDER 35
- SECTION 4 – NAV/COM & 36
- 4.1 RADIO STATUS INDICATIONS 37
- 4.2 VOLUME 37
- 4.3 AUTOMATIC SQUELCH 37
- 4.5 OPTIONAL NAV RADIOS 37
- 4.6 FREQUENCY AUTO-TUNING 38
- 4.7 TRANSPONDER 39
- Flight ID Reporting 40
- SECTION 5: AUDIO PANEL 41
- 5.1 COM RADIO SELECTION 42
- 5.2 SPLIT COM FUNCTION 42
- 5.3 MARKER BEACON RECEIVER 42
- SECTION 5 – AUDIO PANEL 43
- 5.6 INTERCOM SQUELCH CONTROL 44
- AND PLAYER 44
- SECTION 6: AUTOMATIC FLIGHT 45
- Automatic Disengagement 46
- 6.3 LOSS OF DATA 47
- 6.4 PITCH AXIS MODES 47
- Pitch Hold Mode (PIT) 48
- Altitude Hold Mode (ALT) 49
- Vertical Speed Mode (VS) 50
- SECTION 6 – AUTOMATIC 51
- FLIGHT CONTROL 51
- Go-around Mode (GA) 52
- Glideslope (GS) 52
- 6.5 ROLL AXIS MODES 53
- Heading Select Mode (HDG) 54
- Go Around (GA) 56
- Departure 58
- Intercepting a VOR Radial 59
- Flying a GPS Flight Plan 60
- Flight Level Change (Descent) 61
- ILS Approach 62
- Go-Around / Missed Approach 63
- AFCS Status Alerts 64
- Overspeed Protection 65
- SECTION 7: NAVIGATION 67
- SECTION 7 – NAVIGATION 68
- 7.3 AIRPORT INFORMATION 69
- 7.4 INTERSECTION INFORMATION 70
- 7.5 NDB INFORMATION 70
- 7.6 VOR INFORMATION 71
- 7.8 NEAREST AIRPORTS 71
- 7.9 NEAREST INTERSECTIONS 73
- 7.10 NEAREST NDB 73
- 7.11 NEAREST VOR 74
- 7.12 NEAREST USER WAYPOINT 74
- 7.13 NEAREST FREQUENCIES 75
- 7.14 NEAREST AIRSPACES 75
- SECTION 8: FLIGHT PLANNING 77
- Map Page 78
- SECTION 8 – FLIGHT PLANNING 79
- 8.7 CREATE A NEW FLIGHT PLAN 80
- VNAV Page Menu Options 85
- SECTION 9: PROCEDURES 87
- 9.2 APPROACHES 88
- SECTION 9 – PROCEDURES 89
- SECTION 10: HAZARD AVOIDANCE 91
- Stormscope Page 92
- 10.3 XM WEATHER (OPTIONAL) 93
- Weather Products and Symbols 96
- Weather Product Age 96
- TAS600 Series 99
- Proximity Page 100
- Navigation Map 101
- (OPTIONAL) 102
- SECTION 10 – HAZARD 103
- AVOIDANCE 103
- 190-00406-05 Rev. B 105
- Figure 10-23 MPEL Boundary 105
- Operation in Weather Mode 107
- SECTION 11: ABNORMAL 117
- OPERATION 117
- 11.2 ABNORMAL COM OPERATION 118
- 11.3 UNUSUAL ATTITUDES 118
- LOSS OF HEADING INPUT 118
- SECTION 12 – ANNUNCIATIONS 119
- & ALERTS 119
- 12.1 ALERT LEVEL DEFINITIONS 120
- 12.2 AIRCRAFT ALERTS 121
- Annunciation Advisory Alerts 122
- Message Advisory Alerts 122
- TIS Voice Alerts 122
- 12.3 AFCS ALERTS 123
- Database Message Advisories 128
- GMA 1347 Message Advisories 129
- GIA 63 Message Advisories 129
- GEA 71 Message Advisories 131
- GTX 33 Message Advisories 132
- GRS 77 Message Advisories 132
- GMU 44 Message Advisories 133
- GDL 69/69A Message Advisories 133
- GDC 74A Message Advisories 133
- GWX 68 Message Advisories 133
- Blank Page 140
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