User manual GARMIN G1000 CESSNAMUSTANG PILOTS GUIDE

[. . . ] 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. Tel: 913/397. 8200 Fax: 913/397. 8282 Garmin AT, Inc. , 2345 Turner Road SE, Salem, OR 97302, U. S. A. [. . . ] B Garmin G1000 Pilot's Guide for the Cessna Citation Mustang 5-101 GPS NAVIGATION White Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not being used by the system to determine vertical speed and deviation guidance. Altitude is not being used to determine vertical speed and deviation guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Altitude is being used by the system for vertical speed and deviation guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. Altitude is being used by the system for vertical speed and deviation guidance. Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database. Light Blue Halftone Text Large Text The system cannot use this altitude in determining vertical speed and deviation guidance. Small Text The system cannot use this altitude in determining vertical speed and deviation guidance. Table 5-3 VNV Altitude Text Size and Color Some altitudes retrieved from the database have associated restrictions indicating to stay `At', `At or Above', or `At or Below' a specific altitude. These restrictions are indicated using a `bar' above and/or below the appropriate altitude as shown in Figure 5-85. Stay AT or ABOVE 5, 000 ft Stay AT 2, 300 ft Stay AT or BELOW 3, 000 ft Figure 5-85 Altitude Restrictions Note: Vertical constraints and along track offset waypoints are not retained in stored flight plans. Enabling/Cancelling VNV guidance: 1) 2) Select the Active Flight Plan Page. Canceling VNV results in VNV outputs V DEV (vertical deviation), VS REQ (vertical speed required), and TIME TO TOD/BOD (time to top of descent/bottom of descent) going invalid. As a result the non-numeric vertical deviation and VS REQ indicators on the PFD are removed. Additionally the V DEV, VS REQ, and TIME TO TOD displayed in the Current VNV Profile box on the Active Flight Plan Page is dashed. Once cancelled, VNV will remain disabled until manually enabled or a direct-to waypoint is entered while in reversionary mode. VNV can be enabled by pressing the ENBL VNV Softkey causing a VNV waypoint to be selected (if possible) and vertical navigation to resume. 5-102 Garmin G1000 Pilot's Guide for the Cessna Citation Mustang 190-00494-00 Rev. B GPS NAVIGATION ALTITUDE CONSTRAINTS The G1000 provides a means to enter altitude constraints associated with waypoints in the active flight plan so long as the waypoint is not the final approach fix, a waypoint after the FAF, or part of an unsupported lateral leg type. Altitude constraints are displayed and entered in mean sea level (MSL) values to the nearest hundreth. An altitude constraint in above ground level (AGL) format is supported for airports. To convert the value to AGL, turn the FMS Knob when MSL is highlighted and press the ENT Key. When a database altitude restriction is displayed, the G1000 allows user entry of a different altitude when creating a waypoint, effectively overriding the database restriction (only before the FAF). The G1000 allows activation of a displayed database altitude restriction by highlighting the database constraint and selecting the ENT Key. When a database altitude restriction of type "AT or ABOVE" or "AT or BELOW" is activated, the G1000 uses the "AT" portion of the restriction to define the vertical profile. The G1000 annunciates all constraints that cannot be used to calculate vertical guidance by displaying the value in halftone, light blue text. [. . . ] This is often the case in mountainous regions. TIS information is collected during a single radar sweep. Collected information is then sent through the Mode S uplink on the next radar sweep. Because of this, the surveillance information is approximately five seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay. [. . . ]