User manual GARMIN G1000 CESSNAMUSTANG PILOTS GUIDE

[. . . ] Cessna Citation Mustang Copyright © 2006 Garmin Ltd. This manual reflects the operation of System Software version 0435. 07 or later for the Cessna Citation Mustang. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc. , 1200 East 151st Street, Olathe, Kansas 66062, U. S. A. [. . . ] Along track offset waypoints lie along the great circle path of the existing lateral flight plan. Assigning an along track offset to a leg with indeterminate length is not permitted. Entering a negative offset distance results in an along track offset waypoint inserted before the selected lateral waypoint, whereas entering a positive offset distance results in an along track offset waypoint inserted after the selected lateral waypoint. The creation of multiple along track offset waypoints is allowed. NOTE: If the CLR Key is pressed prior to completing the definition of the along track offset waypoint, the along track offset waypoint will be removed. NOTE: An along track offset distance cannot be modified once entered. If the along track offset distance must be changed, the pilot must delete the existing along track offset waypoint and create a new one with the corrected offset distance. Entering an along track offset distance: 1) Select the Active Flight Plan Page. 4) Enter a positive or negative offset distance in the range of +/- 1 to 99 nautical miles (Figure 5-87 ). NOTE: The offset also cannot exceed the distance to the next or previous lateral non-ATK offset waypoint. Along Track Offset Distance Figure 5-87 Along Track Offset Distance 190-00494-00 Rev. B Garmin G1000 Pilot's Guide for the Cessna Citation Mustang 5-105 GPS NAVIGATION Active VNV Waypoint Altitude Target Vertical Speed Required Vertical Speed Vertical Deviation Flight Path Angle Time To Bottom of Descent Figure 5-88 VNV Profile VNV PROFILE The VNV profile can be changed by one of the following means: · Changing the Flight Path Angle (FPA) for the descent segment · Changing the target vertical speed for the descent segment Changes to the VNV profile apply to the current active waypoint only. The VNV profile is not modifiable if there is no active waypoint. An invalid entry results in the previous value being restored. The VNV profile modification is invalid if it results in any of the following conditions: · The maximum allowed FPA is exceeded · The calculated target vertical speed exceeds the maximum allowed · The TOD point is now located behind the aircraft's present position or an s-turn would be required to capture the modified vertical profile · Modifying the vertical speed target for the current waypoint The VS TGT will be computed using the FPA and current ground speed and updated on the display periodically. If there is an active waypoint with a vertical component, a valid ground speed, and the system determines the aircraft is airborne, the pilot can select and modify the VS TGT. Updates to the field will cease when the field is selected for modification. 5-106 Garmin G1000 Pilot's Guide for the Cessna Citation Mustang 190-00494-00 Rev. B GPS NAVIGATION The VS TGT may be changed using the following sequence of actions: Modifying the VS TGT: 1) Press the VNV PROF Softkey. 2) Use the small FMS Knob, or enter the desired value or to modify the value. 3) Press the VNV PROF Softkey again when finished or press the FMS Knob to remove the cursor from the VNV Profile (NOTE: VS TGT must be negative and cannot be less than the configured minimum value). Upon completion of entering a new VS TGT the G1000: · Periodically computes a new FPA using the selected VS TGT and current ground speed until the TOD is reached · Uses the newly computed FPA for the active waypoint with a vertical component · Resumes periodic updates of the VS TGT using the new FPA and current ground speed. VNV profile changes apply to the active waypoint only. The active waypoint with a vertical component and its FPA is shown in the current VNV profile information box. Modifying the flight path angle: 1) Select the FPA by pressing the VNV PROF Softkey followed by a clockwise turn of the large FMS Knob. It can also be selected by scrolling past the end of the active flight plan waypoint list. 2) Modify the value using the small FMS Knob. The FPA must be negative and cannot be less than the configured minimum value. 190-00494-00 Rev. [. . . ] Because of this, the surveillance information is approximately five seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay. These algorithms use track history data to calculate expected intruder positions consistent with the time of display. Occasionally, aircraft maneuvering may cause variations in this calculation and create slight errors on the Traffic Map Page. [. . . ]