Garmin G1000 Manual
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Page 501
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850487 AUTOMATIC FLIGHT CONTROL SYSTEM VNV TARGET ALTITUDE CAPTURE MODE (ALTV) NOTE: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive. However, Selected Altitude Capture Mode is armed implicitly (not annunciated) whenever VNV Target Altitude Capture Mode is armed. VNV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically after the VNV Key is pressed and...
Page 502
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A488 AUTOMATIC FLIGHT CONTROL SYSTEM GLIDEPATH MODE (GP) NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glidepath upon release of the CWS Button. Glidepath Mode is used to track the WAAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box. Selecting Glidepath Mode: 1) Ensure a GPS approach with...
Page 503
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850489 AUTOMATIC FLIGHT CONTROL SYSTEM Figure 7-18 Glidepath Mode Command Bars IndicateDescent on Glidepath Glidepath Mode ActiveGPS Approach Mode Active Glidepath Indicator LNAV/VNAV Approach ActiveGPS is Selected NavigationSource
Page 504
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A490 AUTOMATIC FLIGHT CONTROL SYSTEM GLIDESLOPE MODE (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glideslope upon release of the CWS Button. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the...
Page 505
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850491 AUTOMATIC FLIGHT CONTROL SYSTEM TAKEOFF (TO) AND GO AROUND (GA) MODES In Takeoff and Go Around modes, the flight director commands a constant set pitch attitude. The GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground. Selected Altitude Capture Mode is automatically armed when the aircraft is at least 400 feet below the Selected altitude...
Page 506
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A492 AUTOMATIC FLIGHT CONTROL SYSTEM 7.4 LATERAL MODES The following table relates each GFC 700 lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding Takeoff and Go Around modes. NOTE: The GFC 700 may generate a lower bank angle than the maximum roll command\ limit in degrees indicated in table 7-3 by the amount needed to produce a turn rate equal\ to or less than...
Page 507
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850493 AUTOMATIC FLIGHT CONTROL SYSTEM ROLL HOLD MODE (ROL) NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls wings level. When the flight director is activated or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle condition. Bank Angle Flight...
Page 508
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A494 AUTOMATIC FLIGHT CONTROL SYSTEM HEADING SELECT MODE (HDG) Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI. CHANGING THE SELECTED HEADING NOTE: Pressing the HDG Knob synchronizes the Selected Heading to the current heading. The Selected...
Page 509
190-00709-04 Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850495 AUTOMATIC FLIGHT CONTROL SYSTEM NAVIGATION MODES (GPS, VOR, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode. Pressing the N AV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected...
Page 510
Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04 Rev. A496 AUTOMATIC FLIGHT CONTROL SYSTEM CHANGING THE SELECTED COURSE If the navigation source is VOR or localizer or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob corresponding to the selected flight director (CRS1 for the pilot side, CRS2 for the copilot side). Pressing the CWS Button and hand-flying the aircraft does not change the Selected Course while in Navigation Mode. The...
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