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Figure 5-125 Loaded Approach
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 267
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13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-126. These altitudes are loaded from the database and are displayed as light blue text, indicating these values are “designated” for use in computing vertical deviation guidance.
Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the following:
a) Press the FMS Knob to activate the cursor.
b) Turn the small FMS Knob to highlight the desired altitude.
c) Press the CLR Key.
d) Press the FMS Knob to deactivate the cursor.
After making the altitude “non-designated”, it is displayed as white text.
Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-126. Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS altitude source, therefore, the displayed altitude values are for reference only.
Figure 5-126 Vertical Guidance is Active to the FAF
268 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FPA. To change the vertical flight path, perform the following steps.
a) Select the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 5-127.
b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to enter the desired value.
Note the information now displayed in the ‘CURRENT VNV PROFILE’ box. Also, note the offset waypoint (orange box) and gray circle are now displayed on the map. The gray circle marks the Top of Descent (TOD). In this example, vertical guidance is provided at the TOD that results in a -3.0 degree FPA descent to an altitude of 10,000 feet upon reaching the offset waypoint.
Figure 5-127 Adjusting the Descent
c) Press the ENT Key.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 269
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
15) As seen in Figure 5-128, the aircraft is approaching TOD. Note the target vertical speed required to reached the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are now displayed on the PFD as shown in Figure 5-129.
Figure 5-128 Approaching Top of Descent (TOD)
Figure 5-129 VDI & RVSI Upon Reaching Top of Descent (TOD)Required Vertical Speed Indicator(RVSI)Vertical Deviation Indicator(VDI)TargetAltitude
270 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 5-130.
Figure 5-130 VDI & RVSI Showing Correctly Established DescentAlign Actual Vertical Speed with Required Vertical SpeedKeep Vertical Deviation Indicator Centered
17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 5-131. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet.
Figure 5-131 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 271
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
　
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