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18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5-132. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
Figure 5-132 Turn to intercept OPSHN to FSHER Leg
272 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
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19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-133. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active.
Figure 5-133 Tracking the OPSHN to FSHER Leg
20) The flight continues through the arrival procedure to PYNON (see Figure 5-134). At a point 31 nm from the destination airport, the phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI.
A descent to HABUK is in the next leg. Note the TOD point on the map. Annunciations for the upcoming turn and descent, as well as the VDI and RVSI, appear on the PFD as the flight progresses.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 273
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Figure 5-134 Approaching PYNON
274 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
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AUDIO PANEL EICAS INSTRUMENTS
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MANAGEMENT
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ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 5-135).
Figure 5-135 Approach is Now Active
Note: To manually activate the approach procedure, perform the following steps:
a) Press the PROC Key.
b) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 5-136.
c) Press the ENT Key to activate the approach.
Figure 5-136 Manually Activate Approach
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 275
Flight Management anagement
SYSTEM
OVERVIEW
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INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude is 9,000 feet upon reaching HABUK.
Figure 5-137 Descending Turn to the Initial Approach Fix (IAF)
276 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Flight Management anagement
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AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 5-138) when the final approach course becomes active.
Figure 5-138 Descending to the FAF
The descent continues through the FAF (CEGIX) using the Glidepath Indicator, as one would use a glideslope indicator, to obtain an altitude “AT” 7,800 feet at the FAF. Note the altitude restriction lines over and under (At) the altitude in the ‘ALT’ field in Figure 5-138.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 277
Flight Management anagement
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE” 6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-139.
　
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