G1000 Reference Guide - SkyHoppers

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SECTION 6 – AUTOMATICFLIGHT CONTROLSelected Altitude Capture Mode (ALTS)Selected Altitude Capture Mode arms automaticallywhen the flight director is in Pitch Hold, Vertical Speed,Flight Level Change, or Go Around Mode. This modeis also armed automatically under Vertical Path TrackingMode when the Selected Altitude is to be capturedinstead of the VNAV Target Altitude. The white ‘ALTS’annunciation indicates Selected Altitude Capture Mode isarmed (see Figure 6-5 for example).The ALT Knob is used to set the Selected Altitude,shown above the Altimeter until Selected Altitude CaptureMode becomes active.As the aircraft nears the Selected Altitude, the flightdirector automatically transitions to Selected AltitudeCapture Mode with Altitude Hold Mode armed (Figure6-7). This automatic transition is indicated by the green‘ALTS’ annunciation flashing for up to ten seconds and theappearance of the white ‘ALT’ annunciation. The SelectedAltitude is shown as the Altitude Reference beside the‘ALTS’ annunciation.At 50 ft from the Selected Altitude, the flight directorautomatically transitions from Selected Altitude Captureto Altitude Hold Mode and holds the Selected Altitude(shown as the Altitude Reference). As Altitude Hold Modebecomes active, the white ‘ALT’ annunciation moves to theactive pitch mode field and flashes green for ten secondsto indicate the automatic transition.Altitude Reference (InThis Case, Equal toSelected Altitude)Flash Up to 10 sec, Indicating Automatic TransitionFigure 6-6 Automatic Mode Transitions During Altitude CaptureChanging the Selected AltitudeNOTE: Pressing the CWS Button while in SelectedAltitude Capture Mode does not cancel themode.Use of the ALT Knob to change the Selected Altitudewhile Selected Altitude Capture Mode is active causes theflight director to revert to Pitch Hold Mode with SelectedAltitude Capture Mode armed for the new SelectedAltitude.Altitude Hold Mode (ALT)Altitude Hold Mode can be activated by pressing theALT Key; the flight director maintains the current aircraftaltitude (to the nearest ten feet) as the Altitude Reference.The flight director’s Altitude Reference is shown in theAFCS Status Box and is independent of the SelectedAltitude, displayed above the Altimeter. Altitude HoldMode active is indicated by a green ‘ALT’ annunciation inthe AFCS Status Box.Altitude Hold Mode is automatically armed whenthe flight director is in Selected Altitude Capture Mode.Selected Altitude Capture Mode automatically transitionsto Altitude Hold Mode when the altitude error is less than50 ft. In this case, the Selected Altitude becomes the flightdirector’s Altitude Reference.Changing the Altitude ReferenceNOTE: Turning the ALT Knob while in AltitudeHold Mode changes the Selected Altitude, butnot the flight director’s Altitude Reference anddoes not cancel the mode.With the CWS Button depressed, the aircraft can behand-flown to a new Altitude Reference. When the CWSButton is released at the desired altitude, the new altitudeis established as the Altitude Reference.6-6Garmin G1000 Cockpit Reference Guide for the Cessna Nav III190-00384-07 Rev. A
SECTION 6 – AUTOMATICFLIGHT CONTROLIf the Selected Altitude is reached during CWSmaneuvering, the Altitude Reference is not changed.To adjust the Altitude Reference in this case, the CWSButton must be pressed again after the Selected Altitudeis reached.Altitude HoldMode ActiveFlight Director AltitudeReferenceSelected AltitudeSelected Altitude BugCommand Bars HoldPitch Attitude to MaintainAltitude ReferenceFigure 6-7 Altitude Hold ModeVertical Speed Mode (VS)Vertical Speed Mode is activated by pressing the VSIn Vertical Speed Mode, the flight director acquires Key; the ‘VS’ annunciation appears in the AFCS Status Boxand maintains a Vertical Speed Reference. Current aircraft to indicate the active pitch mode, along with the Verticalvertical speed (to the nearest 100 fpm) becomes the Speed Reference to the right. The Vertical Speed ReferenceVertical Speed Reference at the moment of Vertical Speed is also displayed above the Vertical Speed Indicator. AMode activation. Vertical Speed Mode does not consider Vertical Speed Reference Bug corresponding to the Verticalthe relative position of the Selected Altitude in relation to Speed Reference is shown on the indicator.the current aircraft altitude at the time of mode activation,so it is possible to use Vertical Speed Mode while notclimbing/descending to the Selected Altitude.190-00384-07 Rev. AGarmin G1000 Cockpit Reference Guide for the Cessna Nav III6-7
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TABLE OF CONTENTSSECTION 1: SYSTEM
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TABLE OF CONTENTSBlank PageivGarmin
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SECTION 1SYSTEM OVERVIEW1.1 PFD/MFD
Page 17 and 18: SECTION 1SYSTEM OVERVIEW1.2 PFD SOF
Page 19 and 20: SECTION 1SYSTEM OVERVIEWGPS - Displ
Page 21 and 22: SECTION 1SYSTEM OVERVIEWAIRWAYS - P
Page 23 and 24: SECTION 1SYSTEM OVERVIEWLarge TextS
Page 25 and 26: SECTION 1SYSTEM OVERVIEW2) Apply po
Page 27 and 28: SECTION 2FLIGHT INSTRUMENTSSECTION
Page 29 and 30: SECTION 2FLIGHT INSTRUMENTS2.1 AIRS
Page 31 and 32: SECTION 2FLIGHT INSTRUMENTSMetric D
Page 33 and 34: SECTION 2FLIGHT INSTRUMENTS2.5 MARK
Page 35 and 36: SECTION 2FLIGHT INSTRUMENTSTurn Rat
Page 37 and 38: SECTION 2FLIGHT INSTRUMENTSBearing
Page 39 and 40: SECTION 2FLIGHT INSTRUMENTS2.10 GEN
Page 41 and 42: SECTION 3 - ENGINEINDICATION SYSTEM
Page 51 and 52: SECTION 4 - NAV/COM &TRANSPONDERSEC
Page 53 and 54: SECTION 4 - NAV/COM &TRANSPONDER4.1
Page 55 and 56: SECTION 4 - NAV/COM &TRANSPONDERAlt
Page 57 and 58: SECTION 5 - AUDIO PANELSECTION 5: A
Page 59 and 60: SECTION 5 - AUDIO PANEL5.3 NAV RADI
Page 61 and 62: SECTION 6 - AUTOMATICFLIGHT CONTROL
Page 65: SECTION 6 - AUTOMATICFLIGHT CONTROL
Page 97 and 98: SECTION 7 - NAVIGATIONSECTION 7: NA
Page 99 and 100: SECTION 7 - NAVIGATIONFigure 7-5 Re
Page 101 and 102: SECTION 7 - NAVIGATION4) Turn the l
Page 103 and 104: SECTION 7 - NAVIGATION4) V4 will no
Page 105 and 106: SECTION 7 - NAVIGATIONl) V4 is now
Page 107 and 108: SECTION 7 - NAVIGATION10) At Lamar
Page 109 and 110: SECTION 7 - NAVIGATIONb) ‘SELECT
Page 111 and 112: SECTION 7 - NAVIGATIONa) Press the
Page 113 and 114: SECTION 7 - NAVIGATION19) After pas
Page 115 and 116: SECTION 7 - NAVIGATION23) After cro
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SECTION 7 - NAVIGATION26) The aircr
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SECTION 7 - NAVIGATIONAccess Runway
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SECTION 7 - NAVIGATION7.8 USER WAYP
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SECTION 7 - NAVIGATION7.11 NEAREST
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SECTION 8 - FLIGHT PLANNINGCreate U
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SECTION 8 - FLIGHT PLANNING8.7 CREA
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SECTION 8 - FLIGHT PLANNING8) Turn
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SECTION 8 - FLIGHT PLANNING8.18 DEL
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SECTION 8 - FLIGHT PLANNINGBlank Pa
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SECTION 9 - PROCEDURES9.2 APPROACHE
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SECTION 9 - PROCEDURESBlank Page9-4
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SECTION 10 - HAZARDAVOIDANCEAt a ma
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SECTION 10 - HAZARDAVOIDANCEDisplay
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SECTION 10 - HAZARDAVOIDANCE• Fre
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SECTION 10 - HAZARDAVOIDANCETraffic
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SECTION 10 - HAZARDAVOIDANCE10.7 TE
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SECTION 10 - HAZARDAVOIDANCE3) Pres
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SECTION 10 - HAZARDAVOIDANCEExcessi
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SECTION 10 - HAZARDAVOIDANCETAWS Al
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SECTION 10 - HAZARDAVOIDANCEBlank P
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SECTION 11 - ABNORMALOPERATION11.2
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SECTION 11 - ABNORMALOPERATIONwill
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SECTION 12 - ANNUNCIATIONS& ALERTS1
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SECTION 12 - ANNUNCIATIONS& ALERTS1
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SECTION 12 - ANNUNCIATIONS& ALERTST
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SECTION 12 - ANNUNCIATIONS& ALERTSS
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SECTION 12 - ANNUNCIATIONS& ALERTSM
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SECTION 12 - ANNUNCIATIONS& ALERTSD
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SECTION 12 - ANNUNCIATIONS& ALERTSG
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SECTION 12 - ANNUNCIATIONS& ALERTSM
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INDEXFLTA 10-13Forward Looking Terr
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INDEXWeather product symbol 10-5Wea
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