Cockpit Reference Guide
Table Of Contents
- Section 1: System Overview
- Section 2: Flight Instruments
- Section 3: Engine Indication System (EIS)
- Section 4: NAV/COM and Transponder
- Section 5: Audio Panel
- Section 6: Automatic Flight Control
- Section 7: Navigation
- 7.1 Navigation Map Page
- 7.2 Direct-to Navigation
- 7.3 Navigating an Example Flight Plan
- 7.4 Airport Information
- 7.5 Intersection Information
- 7.6 NDB Information
- 7.7 VOR Information
- 7.8 User Waypoint Information Page
- 7.9 Nearest Airports
- 7.10 Nearest Intersections
- 7.11 Nearest NDB
- 7.12 Nearest VOR
- 7.13 Nearest User Waypoint
- 7.14 Nearest Frequencies
- 7.15 Nearest Airspaces
- Section 8: Flight Planning
- 8.1 User Defined Waypoints
- 8.2 Viewing the Active Flight Plan
- 8.3 Activate a Stored Flight Plan
- 8.4 Activate a Flight Plan Leg
- 8.5 Stop Navigating a Flight Plan
- 8.6 Invert Active Flight Plan
- 8.7 Create a New Flight Plan
- 8.8 Enter an Airway in a Flight Plan
- 8.9 Load a Departure
- 8.10 Load an Arrival
- 8.11 Load an Approach
- 8.12 Remove a Departure, Arrival, Approach, or Airway from a Flight Plan
- 8.13 Store a Flight Plan
- 8.14 Edit a Stored Flight Plan
- 8.15 Delete a Waypoint from the Flight Plan
- 8.16 Invert and Activate a Stored Flight Plan
- 8.17 Copy a Flight Plan
- 8.18 Delete a Flight Plan
- 8.19 Graphical Flight Plan Creation
- 8.20 Trip Planning
- Section 9: Procedures
- Section 10: Hazard Avoidance
- 10.1 Customizing the Hazard Displays on the Navigation Map
- 10.2 STORMSCOPE® (Optional)
- 10.3 XM Weather (Service Optional)
- 10.4 Traffic Systems
- 10.5 Terrain and Obstacle Proximity
- 10.6 Terrain Awareness & Warning System (TAWS) Display (Optional)
- Displaying Terrain on the TAWS Page
- Enable/Disable Aviation Data
- TAWS Inhibit
- Manual System Test
- Forward Looking Terrain Avoidance (FLTA)
- Premature Descent Alert (PDA)
- Excessive Descent Rate Alert (EDR)
- Negative Climb Rate After TakeoffAlert (NCR)
- “Five-Hundred” Aural Alert
- Displaying Terrain and Obstacles on the Navigation Map
- Pop-up Alerts
- TAWS Alerts Summary
- Alert Annunciations
- Section 11: Abnormal Operation
- Section 12: Annunciations & Alerts
- 12.1 Alert Level Definitions
- 12.2 NAV III Aircraft Alerts
- 12.3 CO Guardian Messages
- 12.4 AFCS Alerts
- 12.5 TAWS Alerts
- 12.6 Other G1000 Aural Alerts
- 12.7 G1000 System Annunciations
- 12.8 G1000 System Message Advisories
- MFD & PFD Message Advisories
- Database Message Advisories
- GMA 1347 Message Advisories
- GIA 63 Message Advisories
- GIA 63W Message Advisories
- GEA 71 Message Advisories
- GTX 33 Message Advisories
- GRS 77 Message Advisories
- GMU 44 Message Advisories
- GDL 69A Message Advisories
- GDC 74A Message Advisories
- Miscellaneous Message Advisories
- Index
Garmin G1000 Cockpit Reference Guide for the Cessna Nav III
190-00384-08 Rev. A
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-7
If the Selected Altitude is reached during CWS
maneuvering, the Altitude Reference is not changed.
To adjust the Altitude Reference in this case, the CWS
Button must be pressed again after the Selected Altitude
is reached.
Figure 6-7 Altitude Hold Mode
Altitude Hold
Mode Active
Flight Director Alti
-
tude Reference
Selected Altitude
Selected Altitude Bug
Command Bars Hold
Pitch Attitude to Main-
tain Altitude Reference
Vertical Speed Mode (VS)
In Vertical Speed Mode, the flight director acquires
and maintains a Vertical Speed Reference. Current aircraft
vertical speed (to the nearest 100 fpm) becomes the
Vertical Speed Reference at the moment of Vertical Speed
Mode activation. Vertical Speed Mode does not consider
the relative position of the Selected Altitude in relation to
the current aircraft altitude at the time of mode activation,
so it is possible to use Vertical Speed Mode while not
climbing/descending to the Selected Altitude.
Vertical Speed Mode is activated by pressing the
VS
Key; the ‘VS’ annunciation appears in the AFCS Status Box
to indicate the active pitch mode, along with the Vertical
Speed Reference to the right. The Vertical Speed Reference
is also displayed above the Vertical Speed Indicator. A
Vertical Speed Reference Bug corresponding to the Vertical
Speed Reference is shown on the indicator.