曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using a GPS Navigation. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed.
Figure 7-36 Flight Plan Overview0369121518212427303303691215182124273033SalinaVOR(SLN)KMKCLamarVOR(LAA)03691215182124273033HaysVOR(HYS)KCOSV 244V 4V 24403691215182124273033TopekaVOR(TOP)
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 399
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Departureeparture
Climbing to the Selected Altitude and flying an assigned heading:
1) Before takeoff:
a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet.
b) Push the GA Switch to activate Takeoff Mode. The flight director Command Bars establish a pitch up attitude to follow.
c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level.
2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used).
a) Press the VS Key to activate Vertical Speed and Roll Hold modes and arm Selected Altitude Capture Mode.
The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/DN Wheel or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed Reference.
3) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4.
Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading.
4) 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.
At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft.
400 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Figure 7-37 DepartureSelected Altitude of 12,000 MSL1234HDG ModeVS ModeALT ModeTO ModeTO ModeKMKC
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 401
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Intercepting a VOR Radial
During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used. In this scenario, VOR Navigation Mode is used for navigation to the first VOR waypoint in the flight plan.
Intercepting a VOR radial:
1) Arm VOR Navigation Mode:
a) Tune the VOR frequency.
b) Press the CDI Softkey to set the navigation source to VOR.
c) Use the CRS1 or CRS2 Knob to set the Selected Course to the desired value, 255°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly the Selected Heading, 290°.
d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode.
2) As the aircraft nears the Selected Course, the flight director transitions from Heading Select to VOR Navigation Mode and the ‘VOR’ annunciation flashes green. The autopilot begins turning to intercept the Selected Course.
3) The autopilot continues the turn until the aircraft is established on the Selected Course.
Figure 7-38 Intercepting a VOR Radial03691215182124273033HDG Mode, VOR ArmedVOR NAV ModeV 4SalinaVOR(SLN)123Hdg290o255o
402 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna Citation Mustang G1000 Integrated Flight Dec(142)