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
6-30
Non-path descent using Flight Level
Change Mode:
1)
Command a non-path descent using Flight Level
Change Mode:
a) Using the ALT Knob, set the Selected Altitude
below the current aircraft altitude to an alti
-
tude (in this case, 9,400 feet) at which to level
off between VNV flight plan altitudes.
b) Press the
FLC Key before the planned TOD
during an altitude hold while VPTH is armed.
The Airspeed Reference defaults to the current
aircraft airspeed. Vertical Path Tracking and
Selected Altitude Capture Mode are armed
automatically.
2)
Reduce power to allow descent in Flight Level
Change Mode. The autopilot maintains the
Airspeed Reference.
3)
As the aircraft nears the Selected Altitude, the flight
director transitions to Selected Altitude Capture
Mode, indicated by the green ‘ALTS’ annunciation
flashing for up to 10 seconds.
Figure 6-36 Non-path Descent
HABUK
VNAV Target Altitude of 10,000 MSL
VNAV Target Altitude of 9,000 MSL
ALT Mode
Planned Descent
P
ath
Selected Altitude of 9,400 MSL
ALT Mode
VPTH Mode
1
2
3
FLC Mode
4
VPTH Mode
ALT Mode
Selected Altitude
5
TOD
Planned
TO
D
BOD
BOD
OPSHN
3 nm
The green ‘ALT’ annunciation flashes for up to 10
seconds upon reaching 50 feet from the Selected
Altitude; the autopilot transitions to Altitude Hold
Mode and levels the aircraft.
4)
When the next TOD is reached, Vertical Path Tracking
becomes active (may require acknowledgment to
allow descent path capture).
5)
As the aircraft nears the VNV Target Altitude, the
flight director transitions to VNV Target Altitude
Capture Mode, indicated by the green ‘ALTV’
annunciation flashing for up to 10 seconds.
The green ‘ALT’ annunciation flashes for up to
10 seconds upon reaching 50 feet from the VNV
Target Altitude; the autopilot transitions to Altitude
Hold Mode and levels the aircraft at the vertical
waypoint.










