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Garmin Cessna Caravan G1000 User Manual

Manual is about: Integrated Flight Deck

Summary of Cessna Caravan G1000

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    Hawker beechcraft c90a/gt.

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A copyright © 2007 garmin ltd. Or its subsidiaries. All rights reserved. This manual reflects the operation of system software version 0636.00 or later for the hawker beechctaft c90a/gt. Some differences in operation may b...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt i limited warranty limited warranty this garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, garmin will, at its sole option, repa...

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A ii warnings, cautions, and notes warning: navigation and terrain separation must not be predicated upon the use of the terrain function. The g1000 terrain proximity feature is not intended to be used as a primary refere...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt iii warnings, cautions, and notes warning: the garmin g1000, as installed in the hawker beechcraft c90a/gt aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monit...

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A iv warnings, cautions, and notes caution: the garmin g1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized garmin service center. Unauthorized repairs or modifications could void...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt v revision information record of revisions part number revision date page range description 190-00663-00 a 9/21/07 i – i-6 initial release.

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A vi table of contents section 1 system overview 1.1 system description ..............................................1-1 1.2 line replaceable units (lru) ..............................1-2 1.3 g1000 controls ................

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt vii table of contents 4.5 additional audio panel functions ....................4-32 power-up ................................................................4-32 mono/stereo headsets .......................................

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A viii table of contents 6.3 stormscope wx-500 series ii (optional) .........6-50 setting up stormscope on the navigation map ..........6-50 selecting the stormscope page .................................6-54 6.4 terrain ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt ix table of contents appendices annunciations and alerts ..............................................A-1 comparator annunciations .........................................A-4 reversionary sensor annunciations ...........

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    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A x table of contents b lank p age.

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-1 system overview section 1 system overview 1.1 system description this section provides an overview of the g1000 integrated flight deck as installed in the hawker beechcraft c90a/gt. The g1000 system is an integrated...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-2 system overview 1.2 line replaceable units (lru) • gdu 1040a (2) – each unit is configured as a pfd that features a 10.4-inch lcd with 1024 x 768 resolution. The unit installed on the left/pilot side is designated as...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-3 system overview • gdc 74b (2) – processes data from the pitot/static system as well as the oat probe. This unit provides pressure altitude, airspeed, vertical speed and oat information to the g1000 system, and it co...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-4 system overview • gma 1347d (2) – integrates nav/com digital audio, intercom system and marker beacon controls, and is installed in dual configuration on the outboard side of pfd1 and pfd2. This unit also enables the...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-5 system overview • gcu 475 (1) – provides the flight management system (fms) controls for the mfd through an rs-232 digital interface. • gmc 710 (1) – provides the controls for the gfc 700 afcs through an rs-232 digi...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-6 system overview gdu 1040a (pfd #1) gdu 1040a (pfd #2) gdu 1500 (mfd) gia 63w #2 gsa 80 (yaw) gsa 80 (roll) gsa 80 (pitch) gsa 81 (pitch trim) grs 77 #1 gia 63w #1 gmc 710 gmu 44 #1 gea 71 #2 gea 71 #1 gdc 74b #1 gtp...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-7 system overview 1.3 g1000 controls note: the audio panel (gma 1347d) and afcs controls (gmc 710) are described in the cns & audio panel and afcs sections respectively. The g1000 system controls are located on the pf...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-8 system overview the following list provides an overview of the controls located on the pfd bezel (see figure 1-2). 1 nav vol/id knob – controls nav audio volume level. Press to toggle the morse code identifier audio ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-9 system overview controls associated with the mfd the controls for the mfd (gdu 1500) are located on both the mfd bezel and the mfd control unit (gcu 475). The bottom portion of the mfd bezel features 12 softkeys tha...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-10 system overview 6 joystick – changes the map range when rotated. Activates the map pointer when pressed. 7 alphanumeric keys – allow the user to enter data quickly, without having to select individual characters wi...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-11 system overview 4 fd key – activates/deactivates the flight director in the default pitch and roll modes. If the autopilot is engaged, the fd key is disabled. 5 xfr key – switches the autopilot between the pilot-sid...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-12 system overview audio panel controls figure 1-5 audio panel controls (gma 1347d) 17 18 15 13 11 9 20 7 5 3 1 22 14 2 16 4 6 8 10 12 24 23 21 19 note: when a key is selected, a triangular annunciator above the key i...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-13 system overview 5 com3 mic – selects an optional transmitter for transmitting (if installed). Com3 is simultaneously selected when this key is pressed allowing received audio from the optional receiver to be heard....

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-14 system overview 1.4 secure digital cards note: refer to the appendices for instructions on updating the aviation database. Note: ensure that the g1000 system is powered off before inserting the sd card. The gdu 104...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-15 system overview note: see the pilot’s operating handbook and faa approved airplane flight manual (afm/poh) for specific procedures concerning avionics power application and emergency power supply operation. The g100...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-16 system overview 1.6 system operation the displays are connected together via multiple data busses, thus allowing for high-speed communication. As shown in figure 1-1, each gia 63w is connected to the on-side pfd. T...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-17 system overview figure 1-10 reversionary mode (manual) reversionary mode can be activated manually by pressing the dedicated display backup button at the bottom of the audio panel (see figure 1-11 and refer to the ...

  • Page 30: Air Data

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-18 system overview in addition to using internal sensors, the grs 77 ahrs uses gps information, magnetic field data and air data to assist in attitude/heading calculations. In normal mode, the ahrs relies upon gps and ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-19 system overview air data input failure a failure of the air data input has no effect on ahrs output while ahrs is operating in normal mode. A failure of the air data input while the ahrs is operating in reversionar...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-20 system overview softkey function the softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-21 system overview sensor displays softkeys for selecting the #1 and #2 ahrs and air data computers adc1 selects the #1 air data computer adc2 selects the #2 air data computer ahrs1 selects the #1 ahrs ahrs2 selects t...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-22 system overview alt selects mode c – altitude reporting mode (transponder replies to identification and altitude interrogations) gnd manually selects ground mode, the transponder does not allow mode a and mode c rep...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-23 system overview figure 1-18 sensor softkeys select the back softkey to return to the top level softkeys. Back adc2 adc1 ahrs1 ahrs2 alerts alerts (optional) figure 1-19 pfd configuration softkeys select the back sof...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-24 system overview figure 1-20 xpdr softkeys select the back softkey to return to the top-level softkeys. Select the back softkey to return to the previous level softkeys. Alerts alerts alerts (optional) mfd softkeys ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-25 system overview figure 1-21 mfd softkeys map dcltr topo back terrain dcltr-2 dcltr-3 dcltr-1 select the back softkey on this level to return to the top softkey level. Nexrad xm ltng shw chrt chklist (optional) airw...

  • Page 38

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-26 system overview selecting the gps receiver for which data may be reviewed 1) use the fms knob to select the aux - gps status page. 2) to change the selected gps receiver: a) press the desired gps softkey. Or : a) p...

  • Page 39

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-27 system overview each satellite is represented by an oval containing the pseudo-random noise (prn) number (i.E., satellite identification number). Satellites whose signals are currently being used are represented by ...

  • Page 40

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-28 system overview predicting raim availability at a selected waypoint 1) select the gps status page. 2) if necessary, select the raim softkey. 3) press the fms knob. The ‘waypoint’ field is highlighted. 4) turn the sm...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-29 system overview • ‘compute raim?’—raim has not been computed for the current waypoint, time, and date combination • ‘computing availability’—raim calculation in progress • ‘raim available’—raim is predicted to be a...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-30 system overview navigating the page menu window 1) press the menu key to display the page menu window. 2) turn the fms knob to scroll through a list of available options (a scroll bar appears to the right of the wi...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-31 system overview the mfd displays information in four main page groups; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the fms knob 1) turn the l...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-32 system overview figure 1-27 waypoint pages airport information pages waypoint pages (wpt) airport information pages - airport information (info softkey) - departure information (dp softkey) - arrival information (s...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-33 system overview figure 1-29 nearest pages nearest pages (nrst) nearest airports nearest intersections nearest ndb nearest vor nearest user waypoints nearest frequencies nearest airspaces in addition to the main pag...

  • Page 46

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-34 system overview the procedure pages may be accessed at any time on the mfd by pressing the proc key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate procedure loading ...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-35 system overview restoring system setup defaults: 1) select the aux - system setup page. 2) press the dflts softkey; or press the menu key, highlight ‘restore defaults’, and press the ent key. Figure 1-32 system set...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-36 system overview d ate /t ime the g1000 obtains the current universal coordinated time (utc) date and time directly from the gps satellite signals (shown on the aux - gps status page, figure 1-22). System time (disp...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-37 system overview p ilot p rofiles system settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the mfd power-up splash screen (figure 1-8). The g1000 c...

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    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-38 system overview 8 ) with ‘create’ highlighted, press the ent key to create the profile or : use the large fms knob to select ‘create and activate’ and press the ent key to activate the new profile. 9) to cancel the p...

  • Page 51

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-39 system overview d isplay u nits units in which various quantities are displayed on the g1000 screens are listed on the system setup page. The navigation angle reference, the temperature units, and the position unit...

  • Page 52

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-40 system overview a rrival a lerts the arrival alert box on the system setup page allows arrival alerts to be turned on/off and the alert trigger distance set. An arrival alert can be set to notify the pilot with a m...

  • Page 53

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-41 system overview system status page the system status page displays the status and software version numbers for all detected system lrus. Pertinent information on all system databases is also displayed. Active lrus ...

  • Page 54

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-42 system overview utility page for flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the aux - utility page. The timers available include a stopwatch-like generic timer, a tota...

  • Page 55

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-43 system overview setting the generic timer (pfd): 1) press the tmr/ref softkey. 2) turn the large fms knob to select the timer field (hh/mm/ss). 3) use the fms knob to enter the desired time and press the ent key. 4)...

  • Page 56

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-44 system overview figure 1-40 timers (mfd aux - utility page) the flight timer can be set to count up from zero starting at system power-up or from the time that the aircraft lifts off; the timer can also be reset to ...

  • Page 57

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-45 system overview resetting the departure time 1) use the fms knob to select the aux - utility page. 2) press the menu key. 3) use the fms knob to highlight ‘reset departure time’ and press the ent key. T rip s tatis...

  • Page 58

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-46 system overview s cheduler the g1000’s scheduler feature can be used to enter and display reminder messages (e.G., “change oil”, “switch fuel tanks”, “overhaul”) in the alerts window on the pfd. Messages can be set...

  • Page 59

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-47 system overview 9) for event-based messages: a) use the fms knob to enter the desired date (dd-mmm-yyy) and press the ent key. B) press the ent key again or use the large fms knob to move the cursor to the next fiel...

  • Page 60

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 1-48 system overview 1.8 display backlighting the pfd and mfd display backlighting, the pfd and mfd bezel, and the audio panel keys can be adjusted manually in one of two ways: • using the individual dimmer bus control ...

  • Page 61

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-1 flight instruments section 2 flight instruments warning: in the event that the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup instruments. Note: the automatic flight contro...

  • Page 62

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-2 flight instruments 9 8 17 14 12 1 18 21 5 6 2 4 3 16 11 15 19 13 7 10 20 22 1 nav frequency box 2 airspeed indicator 3 ground speed 4 true airspeed 5 current heading 6 horizontal situation indicator ( hsi) 7 outside...

  • Page 63

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-3 flight instruments 2 3 4 6 1 8 7 11 12 14 9 13 10 5 1 traffic annunciation 2 selected heading 3 wind data 4 inset map 5 dme information window (optional) 6 bearing information windows 7 minimum descent altitude/ deci...

  • Page 64

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-4 flight instruments 2.1 flight instruments airspeed indicator note: refer to the pilot’s operating handbook (poh) and faa approved airplane flight manual (afm) for speed criteria and vspeed values. The airspeed indic...

  • Page 65

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-5 flight instruments vspeeds can be changed and their flags along the right of the airspeed scale turned on/off. By default, all vspeed values are reset and all flags turned off when power is cycled. Figure 2-5 vspeed r...

  • Page 66

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-6 flight instruments changing vspeeds and turning vspeed flags on/off: 1) press the tmr/ref softkey. 2) turn the large fms knob to highlight the desired vspeed. 3) use the small fms knob to change the vspeed in 1-kt in...

  • Page 67

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-7 flight instruments attitude indicator attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The attitude indicator displays the pitch, roll, and slip/skid information....

  • Page 68

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-8 flight instruments figure 2-11 aircraft symbol for cross-pointer command bars the horizon line is part of the pitch scale. Above and below the horizon line, major pitch marks and numeric labels are shown for every 1...

  • Page 69

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-9 flight instruments altimeter the altimeter displays 600 feet of barometric altitude values at a time on a rolling number gauge using a moving tape. Numeric labels and major tick marks are shown at intervals of 100 f...

  • Page 70

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-10 flight instruments a magenta altitude trend vector extends up or down the left of the altitude tape, the end resting at the approximate altitude to be reached in 6 seconds at the current vertical speed. The trend v...

  • Page 71

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-11 flight instruments if the barometric altimeter settings differ between pfds by more than 0.02 in hg, the readouts turn yellow. The settings can be synchronized from the pfd setup menu. Once the settings are synchro...

  • Page 72

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-12 flight instruments vertical deviation note: the glidepath indicator is only shown for aircraft with gia 63w integrated avionics units when waas is available. The vertical deviation indicator (vdi; figure 2-16) uses...

  • Page 73

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-13 flight instruments horizontal situation indicator (hsi) the horizontal situation indicator (hsi) displays a rotating compass card in a heading-up orientation. Letters indicate the cardinal points and numeric labels...

  • Page 74

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-14 flight instruments the arc hsi is a 140˚ expanded section of the compass rose. The arc hsi contains a course pointer, to/from indicator, a sliding deviation indicator (the to/from and deviation indicators are combi...

  • Page 75

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-15 flight instruments navigation angles (track, heading, course, bearing) are corrected to the computed magnetic variation (‘mag var’) or referenced to true north (denoted ‘t’), set on the aux - system setup page. Whe...

  • Page 76

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-16 flight instruments turn rate indicator the turn rate indicator is located directly above the rotating compass card. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. ...

  • Page 77

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-17 flight instruments when a bearing pointer is displayed, its associated information window is also displayed. The bearing information windows (figure 2-25) are displayed to the lower sides of the hsi and show: • bea...

  • Page 78

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-18 flight instruments course deviation indicator (cdi) note: if a heading change of greater than 105˚ with respect to the course is made, the cdi on the arc hsi switches to the opposite side of the deviation scale and...

  • Page 79

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-19 flight instruments changing navigation sources: 1) select the cdi softkey to change from gps to vor1 or loc1. This places the light blue tuning box over the nav1 standby frequency in the upper left corner of the pf...

  • Page 80

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-20 flight instruments if the same vor/loc navigation source is selected on both pfds, the navigation source annunciation turns yellow on both displays (unless synchronized). Once the cdis are synchronized (cdi sync tu...

  • Page 81

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-21 flight instruments gps steering guidance is still provided after the cdi automatically switches to loc until loc capture, up to the final approach fix (faf) for an ils approach, or until gps information becomes inv...

  • Page 82

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-22 flight instruments figure 2-31 automatic cdi scaling 0.3 nm missed approach approach 2.0 nm enroute (oceanic if >200 nm from nearest airport) 1.0 nm 1.0 nm terminal 1.0 nm terminal 0.3 nm departure cdi full-scale d...

  • Page 83

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-23 flight instruments figure 2-32 typical lnav and lnav+v approach cdi scaling 1.0 nm 2 nm 350 ft angle set by system 0.3 nm faf cdi full-scale deflection cdi scale is set to the smaller of 0.3 nm or an angle set by t...

  • Page 84

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-24 flight instruments obs mode note: vnv is inhibited while automatic waypoint sequencing has been suspended. Enabling omni-bearing selector (obs) mode suspends the automatic sequencing of waypoints in a gps flight pla...

  • Page 85

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-25 flight instruments enabling/disabling obs mode while navigating a gps flight plan: 1) select the obs softkey to select obs mode. 2) turn the crs knob to select the desired course to/from the waypoint. Press the crs ...

  • Page 86

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-26 flight instruments 2.2 supplemental flight data note: selecting the dflts softkey (a second-level pfd softkey) turns off metric altimeter display, the inset map, and wind data display. In addition to the flight inst...

  • Page 87

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-27 flight instruments wind data wind direction and speed in knots can be displayed in a window to the upper left of the hsi. When the window is selected for display, but wind information is invalid or unavailable, the...

  • Page 88

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-28 flight instruments vertical navigation (vnv) indications when a vnv flight plan has been activated, vnv indications (vnv target altitude, rvsi, vdi) appear on the pfd in conjunction with the “tod within 1 minute” me...

  • Page 89

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-29 flight instruments 2.3 pfd annunciations and alerting functions the following annunciations and alerting functions are displayed on the pfd. Refer to appendix a for more information on alerts and annunciations. G10...

  • Page 90

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-30 flight instruments warnings are time-critical and require immediate attention. A flashing warning softkey annunciation and aural tone (single chime every two seconds) indicate the presence of a warning. The aural to...

  • Page 91

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-31 flight instruments marker beacon annunciations marker beacon annunciations are displayed on the pfd to the left of the selected altitude. Outer marker reception is indicated in blue, middle in yellow, and inner in ...

  • Page 92

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-32 flight instruments taws annunciations (optional) terrain awareness and warning system (taws) annunciations appear on the pfd to the upper left of the altimeter. Refer to the hazard avoidance section and appendix a ...

  • Page 93

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-33 flight instruments low altitude annunciation note: the low altitude annunciation is available only for aircraft with gia 63w integrated avionics units when waas is available. This annunciation is not shown for syst...

  • Page 94

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-34 flight instruments setting the barometric minimum descent altitude/decision height and bug: 1) select the tmr/ref softkey. 2) turn the large fms knob to highlight the ‘minimums’ field (figure 2-49). 3) turn the smal...

  • Page 95

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 2-35 flight instruments 2.4 abnormal operations abnormal gps conditions the annunciations listed in table 2-4 can appear on the hsi when abnormal gps conditions occur; see figure 2-50 for examples. Refer to the flight m...

  • Page 96

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 2-36 flight instruments unusual attitudes when the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the horizon are displayed on the attitude indicator, starting at 50˚ above...

  • Page 97

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 3-1 engine indication system section 3 engine indication system the g1000 engine indication system (eis) displays critical engine and fuel flow parameters on the left side of the multi function display (mfd) during norma...

  • Page 98

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 3-2 engine indication system 3.1 eis display 1 interstage turbine temperature (itt) displays interstage turbine temperature in degrees celsius (°c) 2 torque (ft-lb) displays torque in foot-pounds 3 tachometer (prop rpm)...

  • Page 99

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 3-3 engine indication system figure 3-2 eis display c90a/gt baseline configuration 8 5 4 3 2 1 6 7.

  • Page 100

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 3-4 engine indication system note: the gauges displayed and the values shown in this section are taken from the hawker beechcraft c90a/gt baseline configuration. Refer to the pilot’s operating handbook (poh) and faa appr...

  • Page 101

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 3-5 engine indication system tachometer (rpm) the tachometer is located beneath the torque gauge and displays the propeller speed in revolutions per minute (rpm) from 0 to 2500. A propeller overspeed is indicated if the...

  • Page 102

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 3-6 engine indication system turbine speed the turbine speed gauge is located beneath the tachometer. Turbine speed is indicated as a percentage of the maximum operating speed (rpm) from 0 to 110%. Figure 3-8 turbine sp...

  • Page 103

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 3-7 engine indication system oil pressure the oil pressure gauge is located beneath the fuel flow gauge. Oil pressure is displayed in pounds per square inch (psi) from 0 to 200 psi. Safe operating pressure is more than ...

  • Page 104

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 3-8 engine indication system 3.2 eis display in reversionary mode in the event of pfd1, pfd2 or mfd failure, the display backup button must be pressed to enter reversionary (or backup) mode. Reversionary mode is a mode ...

  • Page 105

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 3-9 engine indication system reversionary display the eis reversionary mode display gauges are the same as normal mode, except they have a different shape and share one title (i.E. Itt, fflow) for each pair of gauges. N...

  • Page 106

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 3-10 engine indication system b lank p age.

  • Page 107

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-1 audio panel and cns section 4 audio panel and cns 4.1 overview the communication/navigation/surveillance (cns) system includes the audio panels, communication radios, navigation radios, and mode s transponders. The system ...

  • Page 108

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-2 audio panel and cns pfd controls and frequency display figure 4-1 pfd controls, nav/com frequency tuning boxes, and dme tuning window 12 2 1 6 8 7 3 4 5 9 10 11.

  • Page 109

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-3 audio panel and cns 1 nav vol/id knob – controls nav audio volume level. Press to turn the morse code identifier audio on and off. Volume level is shown in the nav frequency field as a percentage. 2 nav frequency transfer ke...

  • Page 110

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-4 audio panel and cns audio panel controls figure 4-2 audio panel controls 17 18 15 13 11 9 20 7 5 3 1 14 2 16 4 6 8 10 12 22 24 23 21 19 note: when a key is selected, a triangular annunciator above the key is illuminated. 1...

  • Page 111

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-5 audio panel and cns 6 com3 – reserved for optional com radio. 7 pa – selects the passenger address system. The selected com transmitter is deselected when the pa key is pressed. 8 tel – not used in beechcraft c90a/gt aircr...

  • Page 112

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-6 audio panel and cns 4.2 com operation com transceiver selection and activation note: during pa mode, the com mic annunciator is extinguished and the com active frequency color changes to white, indicating that neither com ...

  • Page 113

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-7 audio panel and cns transmit/receive indications during com transmission, a white tx appears by the active com frequency replacing the frequency transfer arrow. On the audio panel, when the active com is transmitting, the ...

  • Page 114

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-8 audio panel and cns selecting the radio to be tuned press the small com knob to transfer the frequency tuning box and frequency transfer arrow between the upper and lower radio frequency fields. Figure 4-6 switching com tun...

  • Page 115

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-9 audio panel and cns auto-tuning the com frequency com frequencies can be automatically tuned from the following: • nearest airports window (pfd) • wpt – airport information page • nrst – nearest airports page • nrst – near...

  • Page 116

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-10 audio panel and cns auto-tuning from the mfd frequencies can be automatically loaded into the com frequency box from pages in the nrst or wpt page group by highlighting the frequency and pressing the ent key (figures 4-9,...

  • Page 117

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-11 audio panel and cns or : 1) press the menu key on the mfd control unit (figure 4-9) to display the page menu (figure 4-10). 2) turn the large fms knob to scroll through the menu options. 3) press the ent key to place the ...

  • Page 118

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-12 audio panel and cns on the wpt - airport information page, the cursor can be placed on the frequency field by pressing the fms knob and scrolling through the list. The frequency is transferred to the com standby field with...

  • Page 119

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-13 audio panel and cns com frequencies can also be auto-tuned from the nrst – nearest airspaces, nrst – nearest frequencies, and nrst – nearest airports pages on the mfd in a similar manner using the appropriate softkeys or ...

  • Page 120

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-14 audio panel and cns frequency spacing the g1000 com radios can tune either 25-khz spacing (118.000 to 136.975 mhz) or 8.33-khz spacing (118.000 to 136.990 mhz) for 760-channel or 3040-channel configuration. When 8.33-khz c...

  • Page 121

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-15 audio panel and cns automatic squelch automatic squelch quiets unwanted static noise when no audio signal is received, while still providing good sensitivity to weak com signals. To disable automatic squelch, press the vo...

  • Page 122

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-16 audio panel and cns 4.3 nav operation nav radio selection and activation the nav frequency box is composed of four fields; two standby fields and two active fields. The active frequencies are on the right side and the standb...

  • Page 123

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-17 audio panel and cns nav radios are selected for listening by pressing the corresponding keys on the audio panel. Pressing the nav1, nav2, adf, or dme key selects and deselects the navigation radio source. Selected audio c...

  • Page 124

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-18 audio panel and cns selecting the radio to be tuned press the small nav knob to transfer the frequency tuning box and frequency transfer arrow between the upper and lower radio frequency fields. Figure 4-20 switching nav t...

  • Page 125

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-19 audio panel and cns auto-tuning a nav frequency from the mfd nav frequencies can be selected and loaded from the following mfd pages: • wpt – airport information • wpt – vor information • nrst – nearest airports • nrst – ...

  • Page 126

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-20 audio panel and cns or : 1) when on the nrst pages, press the menu key on the mfd control unit to display the page menu. 2) turn the large fms knob to scroll through the menu options. 3) press the ent key to place the cur...

  • Page 127

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-21 audio panel and cns in the example shown, the vor list is selected with the vor softkey or from the page menu. The fms knob or ent key is used to scroll through the list. The cursor is placed on the frequency with the fre...

  • Page 128

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-22 audio panel and cns while enroute, nav frequencies can also be auto-tuned from the nrst – nearest airports, wpt – airport information, wpt – vor information, and nrst – nearest frequencies pages on the mfd in a similar ma...

  • Page 129

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-23 audio panel and cns auto-tuning nav frequencies on approach activation note: the primary nav frequency is auto-tuned upon loading a vor or ils/localizer approach. Note: when an ils/loc approach has been activated in gps m...

  • Page 130

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-24 audio panel and cns marker beacon receiver note: the marker beacon indicators operate independently of marker beacon audio and cannot be turned off. The marker beacon receiver is used as part of the ils. The marker beacon...

  • Page 131

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-25 audio panel and cns dme tuning note: when another auxiliary window is turned on, the dme tuning window is replaced on the pfd. Note: when turning on the g1000 for use, the system remembers the last frequency used for dme ...

  • Page 132

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-26 audio panel and cns 4.4 gtx 33 mode s transponders the gtx 33 mode s transponders provide mode a, mode c, and mode s interrogation and reply capabilities. Selective addressing or mode select (mode s) capability includes t...

  • Page 133

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-27 audio panel and cns figure 4-30 transponder softkeys (pfd) selecting the back softkey returns to the top-level softkeys. Alerts alerts back bksp ident 7 6 5 4 3 2 1 0 stby on alt vfr code ident back xpdr ident selecting t...

  • Page 134

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-28 audio panel and cns ground mode ground mode is normally selected automatically when the aircraft is on the ground. The transponder powers up in the last mode it was in when shut down. Ground mode can be overridden by sele...

  • Page 135

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-29 audio panel and cns altitude mode (automatic or manual) altitude mode is automatically selected when the aircraft becomes airborne. Altitude mode may also be selected manually by selecting the alt softkey. If altitude mod...

  • Page 136

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-30 audio panel and cns entering a transponder code entering a transponder code with softkeys: 1) select the xpdr softkey to display the transponder mode selection softkeys. 2) select the code softkey to display the transpond...

  • Page 137

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-31 audio panel and cns vfr code the vfr code can be entered either manually or by selecting the xpdr softkey, then the vfr softkey. When the vfr softkey is selected, the pre-programmed vfr code is automatically displayed in ...

  • Page 138

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-32 audio panel and cns 4.5 additional audio panel functions power-up the audio panels perform a self-test during power-up. During the self-test all audio panel annunciator lights illuminate for approximately two seconds. Onc...

  • Page 139

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-33 audio panel and cns intercom pressing the intr com key on either audio panel selects and deselects the intercom on both audio panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and...

  • Page 140

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-34 audio panel and cns passenger address (pa) system a passenger address system is provided by pressing the pa key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the int...

  • Page 141

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-35 audio panel and cns clearance recorder and player the audio panels contain a digital clearance recorder that records up to 2.5 minutes of the selected com radio signal. Recorded com audio is stored in separate memory bloc...

  • Page 142

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-36 audio panel and cns 4.6 audio panels preflight procedure note: if the flight crew is using headsets that have a high/low switch or volume control knob, verify that the switch is in the high position and the volume control ...

  • Page 143

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-37 audio panel and cns setting the audio panels during preflight: 1) verify that the intr com key is selected. 2) verify that the man sq annunciator is extinguished. 3) turn the mstr knob (master volume control) on both audio...

  • Page 144

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-38 audio panel and cns 4.7 abnormal operation abnormal operation of the g1000 includes equipment failures of the g1000 components and failure of associated equipment, including switches and external devices. Stuck microphone...

  • Page 145

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-39 audio panel and cns pfd failure, dual system if pfd1 fails, com1 and nav1 display a red x on both remaining displays. Nav1 is unavailable. Com1 automatically tunes 121.500 mhz, but the frequency is not shown. The com1 eme...

  • Page 146

    190-00663-00 rev. A garmin g1000 pilot’s guide for the beechcraft c90a/gt 4-40 audio panel and cns audio panel fail-safe operation if there is a failure of both audio panels, a fail-safe circuit connects the pilot’s headset and microphone directly to the com1 transceiver and the copilot’s headset di...

  • Page 147

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-1 flight management section 5 flight management 5.1 introduction the g1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of the pilot’s guide explains flight management...

  • Page 148

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-2 flight management figure 5-1 gps navigation information on the pfd location of: - direct to window - flight plan window - procedures window - nearest airports window inset map navigation status box navigation mode f...

  • Page 149

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-3 flight management navigation status box the navigation status box located at the top of the pfd contains two fields displaying the following information: pfd navigation status box • active flight plan leg (e.G., ‘d-> ...

  • Page 150

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-4 flight management 4) turn the small fms knob to display and scroll through the data options list. 5) select the desired data. 6) press the ent key. Pressing the dflts softkey returns any field to its default setting....

  • Page 151

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-5 flight management • north up (north up) aligns the top of the map display to north (default setting). • track up (trk up) aligns the top of the map display to the current ground track. • desired track up (dtk up) al...

  • Page 152

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-6 flight management figure 5-5 map setup menu window - map group orientation field map group selection 4) turn the small fms knob to select the desired orientation. 5) select the ent key to select the new orientation....

  • Page 153

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-7 flight management auto zoom auto zoom allows the g1000 to change the map display range to the smallest range clearly showing the active waypoint. Auto zoom can be overridden by adjusting the range with the joystick,...

  • Page 154

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-8 flight management figure 5-7 map setup menu window - map group, auto zoom auto zoom: off, mfd only, pfd only, all on manual range override expiration time maximum look forward time minimum look forward time configuri...

  • Page 155

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-9 flight management map panning map panning allows the pilot to: • view parts of the map outside the displayed range without adjusting the map range • highlight and select locations on the map • review information for...

  • Page 156

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-10 flight management when the map pointer is placed on an object, the name of the object is highlighted (even if the name was not originally displayed on the map). When any map feature or object is selected on the map...

  • Page 157

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-11 flight management when the map pointer crosses an airspace boundary, the boundary is highlighted and airspace information is shown at the top of the display. The information includes the name and class of airspace,...

  • Page 158

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-12 flight management reviewing information for an airport, navaid, or user waypoint: 1) place the map pointer on a waypoint. 2) press the ent key to display the waypoint information page for the selected waypoint. 3) ...

  • Page 159

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-13 flight management viewing airspace information for a special-use or controlled airspace: 1) place the map pointer on an open area within the boundaries of an airspace. 2) press the ent key to display an options men...

  • Page 160

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-14 flight management measuring bearing and distance distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be calculated using the ‘measure bearing and distance’ sele...

  • Page 161

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-15 flight management topography all navigation maps can display various shades of topography colors representing land elevation, similar to aviation sectional charts. Topographic data can be displayed or removed as de...

  • Page 162

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-16 flight management figure 5-15 navigation map setup menu - topo data setup topo data on/off topo data range the topographic data range is the maximum map range on which topographic data is displayed. Note: since the...

  • Page 163

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-17 flight management figure 5-16 navigation map - topo scale maximum displayed elevation minimum displayed elevation aircraft altitude (msl) ground elevation at pointer location (only visible when pointer is displayed...

  • Page 164

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-18 flight management map symbols this section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol can be turned on or off, and the maximum range to display each symbol ca...

  • Page 165

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-19 flight management aviation symbols the following items are configured on the aviation menu: aviation symbols (text label size can be none, small, medium (med), or large (lrg) symbol default range (nm) maximum range ...

  • Page 166

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-20 flight management symbol setup all pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) press the menu ke...

  • Page 167

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-21 flight management 7) press the ent key to accept the selected range. 8) press the fms knob to return to the navigation map page. Figure 5-19 navigation map setup menu - land group setup maximum display range text l...

  • Page 168

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-22 flight management map declutter the declutter feature allows the pilot to progressively step through four levels of removing map information. The declutter level is displayed in the dcltr softkey and next to the de...

  • Page 169

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-23 flight management table 5-3 lists the items displayed at each declutter level. The ‘x’ represents map items displayed for the various levels of declutter. Item no declutter declutter-1 declutter-2 declutter-3 fligh...

  • Page 170

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-24 flight management airways this airways discussion is based upon the north american airway structure. The airway structure in places other than north america vary by location, etc. And are not discussed in this book...

  • Page 171

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-25 flight management airways may be displayed on the map at the pilot’s discretion using either a combination of airway softkey presses, or menu selections using the menu key from the navigation map page. The airway r...

  • Page 172

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-26 flight management the following range items are configurable on the airways menu: airway type symbol default range (nm) maximum range (nm) low altitude airway (low alt airway) 200 500 high altitude airway (hi alt ai...

  • Page 173

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-27 flight management figure 5-25 navigation map setup menu -track vector, wind vector, nav range ring, fuel range ring setup track vector - on/off - look ahead time fuel range - on/off - fuel reserve time wind vector ...

  • Page 174

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-28 flight management nav range ring the nav range ring shows the direction of travel (ground track) on a rotating compass card. The range is determined by the map range. The range is 1/4 of the map range (e.G., 37.5 n...

  • Page 175

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-29 flight management fuel range ring the map can display a fuel range ring which shows the remaining flight distance. A dashed green circle indicates the selected range to reserve fuel. A solid green circle indicates t...

  • Page 176

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-30 flight management 5.3 waypoints waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are used for all phases of flight planning and navigation. Communication and nav...

  • Page 177

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-31 flight management figure 5-30 waypoint information window - duplicate identifier duplicate message identifier with duplicates duplicate waypoints airports note: ‘north up’ orientation on the airport information page ...

  • Page 178

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-32 flight management figure 5-31 airport information page airport/runway diagram navigation map showing selected airport runway information - designation - length/width/surface - lighting available airport information...

  • Page 179

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-33 flight management view a destination airport: from the airport information page press the menu key. Select ‘view destination airport’. The destination airport is displayed. The airport frequencies box uses the desc...

  • Page 180

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-34 flight management pressing the ent key displays the pfd airport information window for the highlighted airport. Pressing the ent key again returns to the nearest airports window with the cursor on the next airport ...

  • Page 181

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-35 flight management figure 5-34 nearest airport page nearest airport navigation map showing nearest airport runway information - designation/surface - length/width nearest airports - id/type - bearing/distance com/na...

  • Page 182

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-36 flight management viewing runway information for a specific airport: 1) with the nearest airports page displayed, press the rnwy softkey; or press the menu key, highlight ‘select runway window’; and press the ent ke...

  • Page 183

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-37 flight management intersections note: the vor displayed on the intersection information page is the nearest vor, not necessarily the vor used to define the intersection. The intersection information page is used to ...

  • Page 184

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-38 flight management the nearest intersections page can be used to quickly find an intersection close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to ...

  • Page 185

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-39 flight management ndb s the ndb information page is used to view information about ndbs. In addition to displaying a map of the currently selected ndb and surrounding area, the page displays ndb information in four...

  • Page 186

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-40 flight management the nearest ndb page can be used to quickly find a ndb close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest ndbs in t...

  • Page 187

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-41 flight management vor s the vor information page can be used to view information about vor and ils signals (since ils signals can be received on a nav receiver), or to quickly auto-tune a vor or ils frequency. Loca...

  • Page 188

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-42 flight management 4) press the ent key. 5) press the fms knob to remove the flashing cursor. The nearest vor page can be used to quickly find a vor station close to the aircraft. Also, a nav frequency from a selected...

  • Page 189

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-43 flight management user waypoints the g1000 can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any map page (except pfd inset map, aux-trip planning page, or procedure pages) ...

  • Page 190

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-44 flight management figure 5-43 nearest user waypoint page selected user waypoint navigation map showing selected user waypoint nearest user wpt list - identifier - bearing/distance from aircraft position user waypoin...

  • Page 191

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-45 flight management 6) press the ent key to accept the new waypoint. 7) press the fms knob to remove the flashing cursor. Figure 5-44 user waypoint information page menu creating user waypoints from map pages: 1) pres...

  • Page 192

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-46 flight management renaming user waypoints: 1) highlight a user waypoint in the user waypoint list. Press the rename softkey, or press the menu key and select ‘rename user waypoint’ 2) enter a new name. 3) press the...

  • Page 193

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-47 flight management deleting user waypoints deleting a single user waypoint 1) highlight a user waypoint in the user waypoint list, or enter a waypoint in the user waypoint field. 2) press the delete softkey or press ...

  • Page 194

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-48 flight management 5.4 airspaces the g1000 can display the following types of airspaces: class b/tma, class c:tca, class d, restricted, moa (military), other airspace, air defense interdiction zone (adiz), and tempo...

  • Page 195

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-49 flight management the nearest airspaces page, airspace alerts window, and airspace alerts on the pfd provide additional information about airspaces and the location of the aircraft in relationship to them. The airs...

  • Page 196

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-50 flight management figure 5-46 system setup page - airspace alerts dflts softkey airspace alerts box - airspace altitude buffer - alert on/off (default settings shown) map ranges for the airspace boundaries are sele...

  • Page 197

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-51 flight management the nearest airspaces page can be used to quickly find airspaces close to the flight path. In addition, a selected frequency associated with the airspace can be loaded from the nearest airspaces pag...

  • Page 198

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-52 flight management pressing the pfd alerts softkey displays the message window on the pfd. The following airspace alerts are displayed in the message window: message comments inside arspc – inside airspace. The airc...

  • Page 199

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-53 flight management 5.5 direct-to-navigation the direct-to method of navigation, initiated by pressing the direct-to key on either the mfd or pfd, is quicker to use than a flight plan when the desire is to navigate to...

  • Page 200

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-54 flight management figure 5-49 direct-to window - pfd direct-to point info - identifier/symbol/city - facility name activation command direct-to point info - bearing/distance - desired course vnv constraints - altitu...

  • Page 201

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-55 flight management 2) turnthe small fms knob counter-clockwise to display a list of flight plan waypoints (the fpl list is populated only when navigating a flight plan). 3) select the desired waypoint. 4) press the en...

  • Page 202

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-56 flight management 4) press the ent key. The cursor is now displayed on ‘activate?’. 5) press the ent key again to activate the direct-to. Direct-to destinations may also be selected by using the pointer on the navi...

  • Page 203

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-57 flight management when navigating a direct-to, the g1000 sets a direct great circle course to the selected destination. The course to a destination can also be manually selected using the course field (‘course’) on ...

  • Page 204

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-58 flight management removing a vnv altitude constraint: 1) press the direct-to key to display the direct-to window. 2) press the menu key. 3) with ‘clear vertical constraints’ highlighted, press the ent key. Figure 5...

  • Page 205

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-59 flight management 5.6 flight planning flight planning on the g1000 consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals,...

  • Page 206

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-60 flight management the following could cause the airway update to fail: • airway identifier, entry waypoint or exit waypoint not found in the new database. • airway entry/exit waypoint is not an acceptable waypoint f...

  • Page 207

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-61 flight management active flight plan comment figure 5-54 active flight plan window on pfd active flight plan leg active flight plan waypoint list - waypoint id - desired track to waypoint - distance to waypoint - a...

  • Page 208

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-62 flight management 3) turn the small fms knob to display the waypoint information window. (turning it clockwise displays a blank waypoint information window, turning it counter-clockwise displays the waypoint inform...

  • Page 209

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-63 flight management adding waypoints to an existing flight plan waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the desired point of insertion, enter the waypoi...

  • Page 210

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-64 flight management adding a waypoint to a stored flight plan: 1) on the flight plan catalog page, press the fms knob to activate the cursor. 2) highlight the desired flight plan. 3) press the edit softkey; or press th...

  • Page 211

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-65 flight management creating and adding user waypoints to the active flight plan: 1) press the joystick to activate the panning function on the active flight plan page and pan to the map location of the desired user w...

  • Page 212

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-66 flight management 4) turn the small fms knob one click clockwise and select the ld airwy softkey, or press the menu key and select “load airway”. The select airway page is displayed. The ld airwy softkey or the “lo...

  • Page 213

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-67 flight management figure 5-61 active flight plan page - airway inserted inserted airway header - airway identifier: [airway identifier].[exit waypoint identifier] (e.G., v4.Sln) restrictions on adding airways some air...

  • Page 214

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-68 flight management adding procedures to a stored flight plan the g1000 allows the pilot to insert pre-defined instrument procedures from the navigation database into a flight plan. The procedures are designed to facil...

  • Page 215

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-69 flight management departure (dp) a departure procedure (dp) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. The route is defined by selection of a de...

  • Page 216

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-70 flight management figure 5-64 departure loading page - selecting transition departure airport selected departure departure transition points available selected runway selected departure end point preview of selecte...

  • Page 217

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-71 flight management arrival (star) a standard terminal arrival (star) is loaded at the destination airport in the flight plan. Only one arrival can be loaded at a time in a flight plan. The route is defined by selection...

  • Page 218

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-72 flight management figure 5-67 arrival loading page - selecting the transition destination airport selected arrival transitions available with dbry1 arrival waypoint sequence preview of selected arrival selected tra...

  • Page 219

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-73 flight management approach (appr) an approach procedure (appr) can be loaded at any airport that has an approach available. Only one approach can be loaded at a time in a flight plan. The route for a selected approa...

  • Page 220

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-74 flight management figure 5-70 approach loading page - selecting the transition destination airport selected approach transitions available with selected approach approach waypoint sequence preview of selected appro...

  • Page 221

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-75 flight management viewing information about a stored flight plan: 1) press the fpl key on the mfd to display the active flight plan page. 2) turn the small fms knob clockwise one click to display the flight plan cat...

  • Page 222

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-76 flight management sort flight plans the stored flight plans can be sorted alphanumerically based on the flight plan name (comment) assigned to each flight plan. Sorting by comment (flight plan name): 1) press the fpl k...

  • Page 223

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-77 flight management 3) select the copy softkey; or press the menu key, highlight ‘copy flight plan’, and press the ent key. The ‘copy to flight plan xx?’ window is displayed. 4) with ‘ok’ highlighted, press the ent k...

  • Page 224

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-78 flight management deleting flight plan items individual waypoints, entire airways, and entire procedures can be deleted from a flight plan. Some waypoints in the final approach segment (such as the faf or map) can no...

  • Page 225

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-79 flight management 3) press the fms knob to activate the cursor and turn the fms knob to highlight the flight plan to be edited. 4) select the edit softkey; or press the menu key, select ‘edit flight plan’ and press ...

  • Page 226

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-80 flight management 6) press the ent key. The ‘remove from flight plan?’ window is displayed. 7) with ‘ok’ highlighted, press the ent key. To cancel the request, press the clr key, or highlight ‘cancel’ and press the ...

  • Page 227

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-81 flight management figure 5-73 along track offset along track offset waypoint and distance along track offset waypoint and distance from flight plan waypoint entering an along track offset distance: 1) press the fpl...

  • Page 228

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-82 flight management parallel track the parallel track (ptk) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the current flight plan. When parallel track is activated, the course line...

  • Page 229

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-83 flight management figure 5-75 parallel track window offset direction offset distance activation prompt figure 5-76 parallel track active parallel track waypoints - tifto-p - top-p - sln-p - hys-p - laa-p activating...

  • Page 230

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-84 flight management active leg is the first leg of the departure procedure. Attempting to activate parallel track with these conditions results in the message ‘parallel track unavailable invalid route geometry’. If an...

  • Page 231

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-85 flight management cancelling parallel track: 1) press the fpl key to display the active flight plan page (mfd) or the active flight plan window (pfd) 2) press the menu key, highlight ‘parallel track’, and press the...

  • Page 232

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-86 flight management figure 5-80 active flight plan page - new active leg new active flight plan leg confirmation window inverting a flight plan any flight plan may be inverted (reversed) for navigation back to the orig...

  • Page 233

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-87 flight management flight plan views information about flight plans can be viewed in more than one way. The active flight plan can be configured to show cumulative distance over the length of the flight plan or the dist...

  • Page 234

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-88 flight management figure 5-82 active flight plan - wide vs. Narrow view wide softkey, narrow softkey, leg-leg softkey, cum softkey active flight plan narrow view active flight plan wide view collapsing airways the ...

  • Page 235

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-89 flight management figure 5-83 expanded/collapsed airways q3.Fepot airway collapsed view expanded view collapsing/expanding the airways in the active flight plan: 1) press the fpl key to display the active flight pla...

  • Page 236

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-90 flight management 5.7 vertical navigation note: the g1000 supports vertical navigation for all lateral leg types except for ca, ci, fa, fm, ha, hm, pi, va, vd, vi, vr, and vm. Vertical constraints are not retained ...

  • Page 237

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-91 flight management disabling vnv guidance: 1) press the fpl key to display the active flight plan page on the mfd. 2) press the cncl vnv softkey; or press the menu key, highlight ‘cancel vnv’, and press the ent key....

  • Page 238

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-92 flight management activating a vertical navigation direct-to: 1) press the fpl key to display the active flight plan page on the mfd. 2) turn the fms knob to highlight the desired waypoint. Note: the selected waypo...

  • Page 239

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-93 flight management white text light blue text light blue subdued text large text altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is pro...

  • Page 240

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-94 flight management an altitude constraint is invalid if: • meeting the constraint requires the aircraft to climb • meeting the constraint requires the maximum flight path angle (6° down) or maximum vertical speed (-6...

  • Page 241

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-95 flight management reverting a manually entered altitude constraint back to the navigation database value: 1) press the fpl key to display the active flight plan page on the mfd. 2) press the fms knob, and turn to h...

  • Page 242

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-96 flight management 5.8 procedures the g1000 can access the whole range of instrument procedures available. Departures (dps), arrivals (stars), and non-precision and precision approaches (appr) are stored within the ...

  • Page 243

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-97 flight management figure 5-87 departure selection departure airport departure preview available procedure actions departure choices loaded procedures procedure loading page selection softkeys figure 5-88 departure ...

  • Page 244

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-98 flight management viewing available departures at an airport: 1) from the airport information page (first page in the wpt group), select the dp softkey. The departure information page is displayed, defaulting to the...

  • Page 245

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-99 flight management arrivals a standard terminal arrival (star) can be loaded at any airport that has one available. Only one arrival can be loaded at a time in a flight plan. If an arrival is loaded when another arri...

  • Page 246

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-100 flight management figure 5-90 arrival loading loaded arrival selected arrival procedure loading page selection softkeys viewing available arrivals at an airport: 1) from the airport information page (first page in ...

  • Page 247

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-101 flight management removing an arrival from the active flight plan when plans change while flying ifr, arrivals can be easily removed from the active flight plan. Removing an arrival from the active flight plan: 1) p...

  • Page 248

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-102 flight management maintaining a constant vertical glidepath similar to an ils glideslope on approach. This guidance is displayed on the g1000 pfd in the same location as the ils glideslope using a magenta diamond....

  • Page 249

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-103 flight management figure 5-91 approach selection destination airport approach preview available procedure actions approach choices loaded procedures figure 5-92 approach loading loaded approach selected approach l...

  • Page 250

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-104 flight management viewing available approaches at an airport: 1) from the airport information page (first page in the wpt group), select the apr softkey. The departure information page is displayed, defaulting to t...

  • Page 251

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-105 flight management in many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the destination airport. Later, if vectored to final, use the steps above to select ‘activat...

  • Page 252

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-106 flight management course to fix in a missed approach procedure, the fix immediately following the map (in this case ‘6368 ft ’) is not part of the published procedure. It is simply a fix that defines a leg which guid...

  • Page 253

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-107 flight management 5.9 trip planning the g1000 allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or bas...

  • Page 254

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-108 flight management • calibrated airspeed (calibrated as) - the primary source is from the air data system, and the secondary source of information is gps ground speed. • indicated altitude (ind altitude) - the prim...

  • Page 255

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-109 flight management fuel statistics the fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. Some of the calculated trip statistics are dashed when the sel...

  • Page 256

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-110 flight management figure 5-96 trip planning page - waypoint mode selected leg(s) not available selected starting and ending waypoints selected flight plan not available selecting automatic or manual page mode: sel...

  • Page 257

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-111 flight management weight planning note: all weight planning page data fields display data rounded to the nearest 10 pounds or 5 kilograms. Figure 5-97 weight planning page a/c payload calculator basic empty weight ...

  • Page 258

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-112 flight management entering the individual passenger weight: 1) press the fms knob to activate the cursor and highlight the passenger weight field. 2) turn the small fms knob to enter the average passenger weight. 3...

  • Page 259

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-113 flight management weight caution and warning conditions if the zero fuel weight is greater than the maximum allowable zero fuel weight, then the zero fuel weight is displayed in amber. If the aircraft weight is gr...

  • Page 260

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-114 flight management 5.10 raim prediction raim (receiver autonomous integrity monitoring) is a gps receiver function that performs a consistency check on all tracked satellites. Raim ensures that the available satell...

  • Page 261

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-115 flight management 4) enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ent key to accept the waypoint entry. 5) turn the fms kn...

  • Page 262

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-116 flight management figure 5-99 sbas display - active sbas softkey (displays sbas selection) sbas selection box - waas enable/disable raim softkey (displays raim prediction) sbas status.

  • Page 263

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-117 flight management enabling/disabling sbas: 1) select the aux-gps status page. 2) press the fms knob. The sbas selection ‘waas’ field is highlighted. 3) press the ent key to disable sbas. Press the ent key again to ...

  • Page 264

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-118 flight management 5.11 navigating a flight plan the following discussion is an example of navigating a flight plan with the waas capable gps system while the g1000 provides vertical guidance through descents. A lat...

  • Page 265

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-119 flight management 3) atc now assigns routing to join v4. A heading of 290º is assigned to intercept v4. The aircraft turns to heading 290° as seen in figure 5-102. Figure 5-102 assigned heading of 290º 4) enter v4...

  • Page 266

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-120 flight management b) the desired entry point for v4 (top) must be entered. Turn the large fms knob to highlight the desired flight plan insertion point (sln) as shown in figure 5-103. When the v4 entry point (top) ...

  • Page 267

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-121 flight management d) press the ent key. Top is inserted into the flight plan as in figure 5-105. Figure 5-105 top inserted into the flight plan e) with sln still highlighted as in figure 5-105, turn the small fms k...

  • Page 268

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-122 flight management h) press the ent key. The list of available exits for v4 is now displayed as in figure 5-107. Figure 5-107 list of available exits for v4 i) if necessary, turn either fms knob to select the desir...

  • Page 269

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-123 flight management l) v4 is now loaded into the flight plan as shown in figure 5-109. Figure 5-109 v4 is loaded in the flight plan 5) making v4 the active leg of the flight plan. A) press the fms knob to activate the...

  • Page 270

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-124 flight management d) verify the displayed leg is the desired leg and press the ent key. Note in figure 5-111, the magenta arrow in the flight plan window and magenta line on the map indicating v4 is now the active ...

  • Page 271

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-125 flight management 7) as the cdi approaches center, the aircraft turns onto the active leg as seen in figure 5-112. Figure 5-112 turn on to active leg 8) at sln, victor airway 244 (v244) is intercepted. Turn prompt...

  • Page 272

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-126 flight management 9) as seen in figure 5-114, v244 is now the active flight plan leg. Figure 5-114 v244 now active leg.

  • Page 273

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-127 flight management 10) at lamar vor (laa) v263 is intercepted. See figure 5-115. Figure 5-115 hys to laa leg active 11) atc grants clearance to proceed direct to the opshn intersection to begin the arrival procedur...

  • Page 274

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-128 flight management d) turn the large fms knob to place the cursor in the vnv altitude field as shown in figure 5-117. Figure 5-117 enter vnv altitude e) an altitude of 10,000 feet is entered as requested by atc. F) ...

  • Page 275

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-129 flight management h) press the ent key twice to activate the direct-to. Note, in figure 5-119, the magenta arrow indicating the direct- to opshn after the offset waypoint for opshn. The preceding offset waypoint i...

  • Page 276

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-130 flight management b) ‘select approach’ should be highlighted as shown in figure 5-120. Figure 5-120 proceudures window c) press the ent key. A list of available approaches for the destination airport is displayed ...

  • Page 277

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-131 flight management e) press the ent key. A list of available transitions for the selected approach is displayed as in figure 5-122. Figure 5-122 list of available transitions f) turn either fms knob to select the d...

  • Page 278

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-132 flight management 13) note the altitude constraints associated with each of the approach waypoints as seen in figure 5-124. These altitudes are loaded from the database and are displayed as light blue text, indica...

  • Page 279

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-133 flight management 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 sp...

  • Page 280

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-134 flight management 15) as seen in figure 5-126, the aircraft is approaching tod. Note the target vertical speed required to reached the selected altitude. The vertical deviation indicator (vdi) and the required ver...

  • Page 281

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-135 flight management 16) upon reaching tod, a descent vertical speed is established which places the vsi pointer in line with the rvsi as shown in figure 5-128. Figure 5-128 vdi & rvsi showing correctly established d...

  • Page 282

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-136 flight management 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 5-130. Initiate the turn and maneuver the aircraft on a trac...

  • Page 283

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-137 flight management 19) after passing opshn, the next leg of the arrival turns magenta as shown in figure 5-131. The magenta arrow in the flight plan list now indicates the opshn to fsher leg of the arrival procedure...

  • Page 284

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-138 flight management figure 5-132 approaching pynon.

  • Page 285

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-139 flight management 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...

  • Page 286

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-140 flight management 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 5-135 descendi...

  • Page 287

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-141 flight management 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 scalin...

  • Page 288

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-142 flight management 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 5-137. Fi...

  • Page 289

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-143 flight management 25) upon reaching the map, it is decided to execute a missed approach. Automatic waypoint sequencing is suspended past the map. Select the susp softkey on the pfd to resume automatic waypoint seq...

  • Page 290

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-144 flight management 26) the aircraft continues climbing to “at or above” 10,000 feet at mogal. A holding pattern is established at the mahp (mogal) as shown in figure 5-139. Figure 5-139 establishing the holding pat...

  • Page 291

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 5-145 flight management 5.12 abnormal operation this section discusses the dead reckoning mode of operation and the subsequent indications. Note: dead reckoning mode only functions in enroute (enr) or oceanic (ocn) phas...

  • Page 292

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 5-146 flight management figure 5-141 dead reckoning mode - gps derived data shown in yellow distance & bearing gps navigation lost message dead reckoning annunciaion dead reckoning annunciation subdued aircraft symbol n...

  • Page 293

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-1 hazard avoidance section 6 hazard avoidance the g1000 hazard avoidance features are designed to provide advisory information of potential hazards to flight safety associated with weather, terrain, and air traffic. Thi...

  • Page 294

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-2 hazard avoidance 6.1 xm satellite weather note: xm satellite weather data provides information for avoiding hazardous weather. It is not meant for use to penetrate hazardous weather. Xm satellite weather is provided...

  • Page 295

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-3 hazard avoidance select info softkey to display xm information page weather products (available products for service class indicated in green) select lock softkey to lock subscription information figure 6-2 xm infor...

  • Page 296

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-4 hazard avoidance using xm satellite weather products the primary map for viewing xm weather data is the weather data link page in the map page group. This is the only g1000 map display capable of showing information...

  • Page 297

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-5 hazard avoidance this table shows the weather product symbols, the expiration time and the refresh rate. The refresh rate represents the interval at which xm satellite radio broadcasts new signals that may or may no...

  • Page 298

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-6 hazard avoidance this table shows which xm products can be displayed (indicated with a ‘+’ symbol) on specific maps. Weather product pfd inset map navigation map p age w eather data link page w eather information pag...

  • Page 299

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-7 hazard avoidance weather softkeys on the weather data link page softkeys control the display of weather information on most mfd pages and the pfd inset map (the figure shows the weather product softkeys for the weath...

  • Page 300

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-8 hazard avoidance setting up and customizing the weather data link page: 1) select the weather data link page with the fms knob. 2) on the weather data link page press the menu key. 3) select the weather setup option...

  • Page 301

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-9 hazard avoidance maps other than the weather data link page use settings based on those selected for the navigation map page. Setting up and customizing weather data for the navigation map page: 1) select the naviga...

  • Page 302

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-10 hazard avoidance each active weather product has an associated legend which can be displayed on the weather data link page. Viewing legends for displayed weather products 1) select the weather data link page with t...

  • Page 303

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-11 hazard avoidance nexrad note: nexrad cannot be displayed at the same time as map topography and/or terrain. Wsr-88d, or nexrad (next-generation radar), is a network of 158 high-resolution doppler radar systems that...

  • Page 304

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-12 hazard avoidance displaying nexrad weather information: 1) select the map softkey (for the pfd inset map, select the inset softkey). This step is not necessary on the weather data link page. 2) select the nexrad so...

  • Page 305

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-13 hazard avoidance r eflectivity reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the nexrad display directly correlate to the level of detected reflectivity. Reflectivity as it ...

  • Page 306

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-14 hazard avoidance the following may cause abnormalities in displayed nexrad radar images: • ground clutter • strobes and spurious radar data • sun strobes (when the radar antenna points directly at the sun) • interf...

  • Page 307

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-15 hazard avoidance displaying echo tops information: 1) select the weather data link page with the fms knob. 2) select the echo tops softkey. To display the echo tops legend, select the legend softkey when echo tops ...

  • Page 308

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-16 hazard avoidance cloud tops note: cloud tops and echo tops cannot be displayed at the same time. Cloud tops data depicts cloud top altitudes as determined from satellite imagery. Figure 6-15 cloud tops data display...

  • Page 309

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-17 hazard avoidance xm lightning note: xm lightning and optional l-3 stormscope® wx-500 lightning are mutually exclusive. Lightning data shows the approximate location of cloud-to-ground lightning strikes. A strike ic...

  • Page 310

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-18 hazard avoidance displaying xm lightning information: 1) select the map softkey (for the pfd inset map, select the inset softkey). This step is not necessary on the weather data link page. 2) select the xm ltng sof...

  • Page 311

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-19 hazard avoidance displaying cell movement information: 1) select the map softkey (for the pfd inset map, select the inset softkey). This step is not necessary on the weather data link page. 2) select the nexrad sof...

  • Page 312

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-20 hazard avoidance displaying sigmets and airmets: 1) select the weather data link page with the fms knob. 2) select the sig/air softkey. 3) to view the text of the sigmet or airmet, press the range knob and move the...

  • Page 313

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-21 hazard avoidance metars and tafs note: atmospheric pressure reported for metars is given in hectopascals (hpa), except in the united states, where it is reported in inches of mercury (in hg). Temperatures are repor...

  • Page 314

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-22 hazard avoidance 5) press the fms knob or the clr key to return to the weather data link page. Or : 1) select the weather information page. (the first rectangular page in the waypoint page group.) 2) select the wx s...

  • Page 315

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-23 hazard avoidance surface analysis and city forecast note: surface analysis and city forecast data are displayed only within the installed aviation database service area. Surface analysis and city forecast informati...

  • Page 316

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-24 hazard avoidance to display the surface analysis and city forecast legend, select the legend softkey when surface analysis and city forecast are selected for display. Figure 6-27 surface analysis legend freezing le...

  • Page 317

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-25 hazard avoidance displaying freezing level information: 1) select the weather data link page with the fms knob. 2) select the more wx softkey. 3) select the frz lvl softkey. To display the freezing level legend, se...

  • Page 318

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-26 hazard avoidance figure 6-30 winds aloft at 27,000 feet to display the winds aloft legend, select the legend softkey when winds aloft is selected for display. Figure 6-31 winds aloft data with legend.

  • Page 319

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-27 hazard avoidance county warnings county data provides specific public awareness and protection weather warnings from the national weather service (nws). This can include information on fires, tornadoes, severe thunde...

  • Page 320

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-28 hazard avoidance cyclone the cyclone weather product shows the current location of cyclones (hurricanes) and their projected tracks. Figure 6-34 cyclone data selected for display cyclone displaying cyclone (hurrica...

  • Page 321

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-29 hazard avoidance 6.2 airborne color weather radar system description the garmin gwx 68 airborne color weather radar is a four-color digital pulsed radar with 6.5 kilowatts of output power. It combines excellent ran...

  • Page 322

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-30 hazard avoidance nexrad and airborne weather radar both airborne weather radar and nexrad measure weather reflectivity in decibels (db). A decibel is a logarithmic expression of the ratio of two quantities. Airborne...

  • Page 323

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-31 hazard avoidance radar signal attenuation the phenomenon of radar signal attenuation affects the operation of weather radar. When the radar signal is transmitted, it is progressively absorbed and scattered, making ...

  • Page 324

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-32 hazard avoidance radar signal reflectivity p recipitation precipitation or objects more dense than water, such as the surface of the earth or solid structures, are detected by the weather radar. The weather radar d...

  • Page 325

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-33 hazard avoidance g round r eturns the intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (angle of incidence) and the reflective properties of that target. Th...

  • Page 326

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-34 hazard avoidance safe operating distance the following information establishes a minimum safe distance from the antenna for personnel near operating weather radar. The minimum safe distance is based on the fcc’s ex...

  • Page 327

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-35 hazard avoidance practical application using the basic tilt setup with the antenna tilt set as previously described, any displayed target return should be scrutinized when flying at altitudes between 2,000 and 30,00...

  • Page 328

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-36 hazard avoidance weather mapping and interpretation weather display interpretation when evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates shown in t...

  • Page 329

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-37 hazard avoidance along squall lines (multiple cells or clusters of cells in a line) individual cells may be in different stages of development. Areas between closely spaced, intense targets may contain developing c...

  • Page 330

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-38 hazard avoidance in areas of multiple heavy cells, use the vertical scan feature along with antenna tilt management to examine the areas. Remember to avoid shadowed areas behind targets. Figure 6-44 the blind alley...

  • Page 331

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-39 hazard avoidance hail shafts are associated with the same radar target return characteristics as tornados. U-shaped cloud edges three to seven miles across can also indicate hail. These target returns appear quite ...

  • Page 332

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-40 hazard avoidance displaying weather on the weather radar page: 1) select the weather radar page in the map page group with the fms knob. 2) select the mode softkey. 3) while on the ground, select the standby softke...

  • Page 333

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-41 hazard avoidance vertically scanning a storm cell: note: vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant adjustment of the bearing line. 1) while in the horizontal s...

  • Page 334

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-42 hazard avoidance figure 6-48 vertical scan display a djusting a ntenna t ilt a ngle in order to make an accurate interpretation of a storm cell, the radar beam should be pointed at the wet part of the weather cell ...

  • Page 335

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-43 hazard avoidance adjusting antenna tilt on the vertical scan display: 1) select the tilt softkey to activate the cursor in the tilt field and display the tilt line. If the tilt line is not displayed, press the menu ...

  • Page 336

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-44 hazard avoidance a djusting g ain warning: changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. Remember to return the gain setting t...

  • Page 337

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-45 hazard avoidance s ector s can 1) while in horizontal scan mode, select the brg softkey to display the bearing line and place the cursor in the bearing field. If the bearing line is not displayed, press the menu key...

  • Page 338

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-46 hazard avoidance figure 6-52 40˚ sector scan a ntenna s tabilization 1) to activate or deactivate the antenna stabilization, select the mode softkey. 2) select the stab on softkey to activate antenna stabilization ...

  • Page 339

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-47 hazard avoidance w eather a ttenuated c olor h ighlight (watch™) while in horizontal scan mode, this feature can be used as a tool to determine areas of possible inaccuracies in displayed intensity due to weakening...

  • Page 340

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-48 hazard avoidance w eather a lert the weather alert feature indicates the presence of heavy precipitation between the ranges of 80 and 320 nm regardless of the currently displayed range. Weather alert targets appear...

  • Page 341

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-49 hazard avoidance ground mapping and interpretation a secondary use of the weather radar system is for the presentation of terrain. This can be a useful tool for verifying aircraft position. A picture of the ground ...

  • Page 342

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-50 hazard avoidance 6.3 stormscope wx-500 series ii (optional) note: the stormscope system is not intended for hazardous thunderstorm penetration. Weather information on the g1000 mfd is approved for weather avoidance...

  • Page 343

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-51 hazard avoidance 6) press the ent key. 7) press the fms knob to return to the navigation map page (figure 6-58). The following options are available (figure 6-57): • strmscp ltng – turns the display of stormscope d...

  • Page 344

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-52 hazard avoidance cell and strike mode on the navigation map on the navigation map, cell mode identifies cells of lightning activity (figure 6-58). Stormscope identifies clusters of electrical activity that indicate c...

  • Page 345

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-53 hazard avoidance manually clearing stormscope data on the navigation map: 1) press the menu key. 2) select ‘clear stormscope lightning’. 3) press the ent key. Figure 6-59 navigation map page options menu zoom range...

  • Page 346

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-54 hazard avoidance selecting a stormscope range on the navigation map: 1) press the menu key. 2) select ‘map setup’. 3) select the ‘weather’ group. 4) press the ent key. 5) turn the large fms knob to select ‘strmscp ...

  • Page 347

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-55 hazard avoidance changing between ‘cell’ and ‘strike’ mode: 1) select the stormscope page. 2) press the mode softkey. The cell and strike softkeys are displayed. 3) press the cell softkey to display ‘cell’ data or ...

  • Page 348

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-56 hazard avoidance changing the viewing mode between 360˚ and 120˚: 1) select the stormscope page. 2) press the view softkey. The 360 and arc softkeys are displayed. 3) press the 360 softkey to display a 360˚ viewing...

  • Page 349

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-57 hazard avoidance 6.4 terrain awareness & warning system (taws) warning: do not use taws information for primary terrain avoidance. Taws is intended only to enhance situational awareness. Note: the data contained in...

  • Page 350

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-58 hazard avoidance displaying taws data taws uses yellow (caution) and red (warning) to depict terrain and obstacles with heights greater than 200 feet above ground level, agl. Alerts are given relative to aircraft a...

  • Page 351

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-59 hazard avoidance terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings and cautions are issued are shown when terrain is selected for display and the map ran...

  • Page 352

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-60 hazard avoidance taws page the taws page is specialized to show terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. Aviation data (ai...

  • Page 353

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-61 hazard avoidance figure 6-67 taws page, 360º view yellow terrain (caution - terrain between 100’ and 1000’ below the aircraft altitude) red terrain (warning - terrain above or within 100’ below the aircraft altitud...

  • Page 354

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-62 hazard avoidance taws alerts alerts are issued when flight conditions meet parameters that are set within taws software algorithms. Taws alerts typically employ a caution or a warning alert severity level, or both. ...

  • Page 355

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-63 hazard avoidance figure 6-71 taws pull up alert annunciation on the mfd alert annunciation potential impact point.

  • Page 356

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-64 hazard avoidance taws inhibit pda and flta aural and visual alerts can be manually inhibited. Use caution when inhibiting taws as the system should be enabled when appropriate. When taws is inhibited, the alert ann...

  • Page 357

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-65 hazard avoidance alert type pfd/mfd alert annunciation mfd pop-up alert aural message excessive descent rate warning (edr) “pull up” reduced required terrain clearance warning (rtc) * or “terrain, terrain; pull up,...

  • Page 358

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-66 hazard avoidance excessive descent rate alert the purpose of the excessive descent rate (edr) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an e...

  • Page 359

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-67 hazard avoidance forward looking terrain avoidance the forward looking terrain avoidance (flta) alert is used by taws and is composed of: • r educed r equired t errain c learance and r educed r equired o bstacle c ...

  • Page 360

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-68 hazard avoidance premature descent alerting a premature descent alert (pda) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway. Pda alerting begins when t...

  • Page 361

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-69 hazard avoidance negative climb rate after takeoff alert (ncr) the negative climb rate (ncr) after takeoff alert (also referred to as “altitude loss after takeoff”) provides alerts when the system determines the ai...

  • Page 362

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-70 hazard avoidance system status during g1000 power-up, taws conducts a self-test of its aural and visual annunciations. The system test can also be manually initiated. An aural alert is issued at test completion. Ta...

  • Page 363

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-71 hazard avoidance 6.5 traffic information service (tis) warning: the traffic information service (tis) is intended for advisory use only. Tis is intended to help the pilot locate traffic visually. It is the responsibi...

  • Page 364

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-72 hazard avoidance a non-threat advisory, shown as an open white diamond, indicates that an intruding aircraft is at greater than ±1200 feet relative altitude or the distance is beyond 5 nm. A proximity advisory indi...

  • Page 365

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-73 hazard avoidance displaying traffic data traffic information can be displayed on the following maps when tis is operating: • pfd inset map • navigation map page • traffic map page • trip planning page • nearest pages...

  • Page 366

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-74 hazard avoidance customizing traffic display on the navigation map page: 1) select the navigation map page. 2) press the menu key. 3) with map setup highlighted, press the ent key (figure 6-79). 4) turn the small fm...

  • Page 367

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-75 hazard avoidance traffic map page the traffic map page is specialized to show surrounding tis traffic data in relation to the aircraft’s current position and altitude, without clutter from the basemap. Aircraft orien...

  • Page 368

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-76 hazard avoidance tis alerts when the number of tas on the traffic map page increases from one scan to the next, the following occur: • a single “traffic” voice alert is generated. • a traffic annunciation appears to ...

  • Page 369

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-77 hazard avoidance muting the “traffic not available” voice alert: 1) select the traffic map page. 2) select the tna mute softkey. The status is displayed in the upper left corner of the traffic map page. Or : 1) press ...

  • Page 370

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-78 hazard avoidance figure 6-84 tis power-up test failure no data received from transponder system test failed the traffic mode is annunciated in the upper left corner of the traffic map page. When the aircraft is on th...

  • Page 371

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-79 hazard avoidance switching between tis modes: 1) select the traffic map page. 2) select the standby or operate softkey to switch between modes. The mode is displayed in the upper left corner of the traffic map page. ...

  • Page 372

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-80 hazard avoidance 6.6 l-3 skywatch hp (sky899) tas (optional) note: tis is disabled when traffic advisory system (tas) is installed. Refer to the skywatch®hp (sky899) pilot’s guide for a detailed discussion of the sk...

  • Page 373

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-81 hazard avoidance operation the unit must be in operating mode for traffic to be displayed. The ability to switch from standby to operating mode on the ground is especially useful for scanning the airspace around the...

  • Page 374

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-82 hazard avoidance figure 6-86 traffic map page operating mode altitude mode traffic advisory, aircraft is 400’ below, climbing off scale traffic “non-bearing” traffic (bearing undetermined), distance 8.0 nm, 1100’ above...

  • Page 375

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-83 hazard avoidance 2) select the traffic softkey. Traffic is now displayed on the map as shown in the figure. Proximity traffic figure 6-87 tas traffic on navigation map traffic advisory ta off scale banner non-bearing tr...

  • Page 376

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-84 hazard avoidance the navigation map page setup menu also controls the display of traffic. The setup menu controls the map range settings. Traffic data symbols and labels can be decluttered from the display. If a map ...

  • Page 377

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-85 hazard avoidance customizing the traffic display on the navigation map page: 1) select the navigation map page. 2) press the menu key. 3) with map setup highlighted, press the ent key (figure 6-88). 4) turn the smal...

  • Page 378

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-86 hazard avoidance tas alerts note: refer to the sky899 documentation for information on alerts generated by the tas equipment. When the number of tas on the traffic map page increases from one scan to the next, the f...

  • Page 379

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 6-87 hazard avoidance if the unit fails, an annunciation as to the cause of the failure is shown in the center of the traffic map page. Traffic map page annunciation description no data data is not being received from the...

  • Page 380

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 6-88 hazard avoidance b lank p age.

  • Page 381

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-1 afcs section 7 automatic flight control system 7.1 afcs overview note: the approved pilot’s operating handbook (poh) and faa approved airplane flight manual (afm) always supersedes this pilot’s guide. The gfc 700 is...

  • Page 382

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-2 afcs afcs control unit the afcs control unit is positioned above the mfd, and has the following controls: 1 hdg key selects/deselects heading select mode 2 apr key selects/deselects approach mode 3 nav key selects/d...

  • Page 383

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-3 afcs additional afcs controls the following afcs controls are located separately from the afcs control unit: ap/yd disc trim intrpt switch (autopilot disconnect/trim interrupt) disengages the autopilot, yaw damper, ...

  • Page 384

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-4 afcs 7.2 flight director operation the flight director function provides pitch and roll commands to the afcs and displays them on the pfds. With the flight director active, the aircraft can be hand-flown to follow the ...

  • Page 385

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-5 afcs afcs status box flight director mode annunciations are displayed on the pfds when the flight director is active. Flight director selection and autopilot and yaw damper statuses are shown in the center of the afc...

  • Page 386

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-6 afcs flight director modes flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.E., press on, press off). In the abs...

  • Page 387

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-7 afcs command bars upon activation of the flight director, command bars are displayed in magenta on the pfds as single cues or cross pointers. The aircraft symbol (in yellow) changes to accommodate the command bar for...

  • Page 388

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-8 afcs 7.3 vertical modes table 7-2 lists the vertical modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for altitude hold, vertical speed,...

  • Page 389

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-9 afcs pitch hold mode (pit) when the flight director is activated (the fd key is pressed) or switched (the xfr key is pressed), pitch hold mode is selected by default. Pitch hold mode is indicated as the active vertic...

  • Page 390

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-10 afcs selected altitude capture mode (alts) selected altitude capture mode is automatically armed with activation of the following modes: • pitch hold • vertical speed • flight level change • go around • vertical pa...

  • Page 391

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-11 afcs altitude hold mode (alt) altitude hold mode can be activated by pressing the alt key; the flight director maintains the current aircraft altitude (to the nearest 10 feet) as the altitude reference. The flight di...

  • Page 392

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-12 afcs vertical speed mode (vs) in vertical speed mode, the flight director acquires and maintains a vertical speed reference. Current aircraft vertical speed (to the nearest 100 fpm) becomes the vertical speed refere...

  • Page 393

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-13 afcs flight level change mode (flc) note: the selected altitude should be set before selecting flight level change mode. Flight level change mode is selected by pressing the flc key. This mode acquires and maintain...

  • Page 394

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-14 afcs changing the airspeed reference the airspeed reference (shown in both the afcs status box and above the airspeed indicator) may be adjusted by: • using the nose up/dn wheel • pressing the cws button, hand-flyin...

  • Page 395

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-15 afcs vertical navigation modes (vpth, altv) note: vnv is disabled when parallel track or dead reckoning mode is active. Note: the selected altitude takes precedence over any other vertical constraints. Vertical nav...

  • Page 396

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-16 afcs vertical path tracking mode (vpth) note: if another vertical mode key is pressed while vertical path tracking mode is selected, vertical path tracking mode reverts to armed. Note: pressing the cws button while...

  • Page 397

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-17 afcs in conjunction with the “tod [top of descent] within 1 minute” annunciation in the pfd navigation status box and the “vertical track” voice message, vnv indications (vnv target altitude, vertical deviation, an...

  • Page 398

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-18 afcs when a descent leg is captured (i.E., vertical deviation becomes valid), vertical path tracking becomes active and tracks the descent profile (figure 7-15). An altitude capture mode (‘alts’ or ‘altv’) is armed ...

  • Page 399

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-19 afcs a utomatic r eversion to p itch h old m ode several situations can occur while vertical path tracking mode is active which cause the flight director to revert to pitch hold mode: • vertical deviation exceeds 20...

  • Page 400

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-20 afcs vnv target altitude capture mode (altv) note: armed vnv target altitude and selected altitude capture modes are mutually exclusive. However, selected altitude capture mode is armed implicitly (not annunciated)...

  • Page 401

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-21 afcs glidepath mode (gp) note: pressing the cws button while glidepath mode is active does not cancel the mode. The autopilot guides the aircraft back to the glidepath upon release of the cws button. Glidepath mode...

  • Page 402

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-22 afcs glideslope mode (gs) note: pressing the cws button while glideslope mode is active does not cancel the mode. The autopilot guides the aircraft back to the glideslope upon release of the cws button. Glideslope ...

  • Page 403

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-23 afcs takeoff (to) and go around (ga) modes go around and takeoff modes are coupled pitch and roll modes and are annunciated as both the vertical and lateral modes when active. In these modes, the flight director com...

  • Page 404

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-24 afcs 7.4 lateral modes the following table relates each gfc 700 lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding go around and takeoff modes. La...

  • Page 405

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-25 afcs roll hold mode (rol) note: if roll hold mode is activated as a result of a mode reversion, the flight director rolls the wings level. When the flight director is activated or switched, roll hold mode is selected...

  • Page 406

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-26 afcs heading select mode (hdg) heading select mode is activated by pressing the hdg key. Heading select mode acquires and maintains the selected heading. The selected heading is shown by a light blue bug on the hsi...

  • Page 407

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-27 afcs navigation mode (gps, vor, loc) note: the selected navigation receiver must have a valid vor or loc signal or active gps course for the flight director to enter navigation mode. Pressing the nav key selects nav...

  • Page 408

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-28 afcs changing the selected course if the navigation source is vor or localizer or obs mode has been enabled when using gps, the selected course is controlled using the crs knob corresponding to the selected flight d...

  • Page 409

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-29 afcs approach mode (gps, vapp, loc) note: the selected navigation receiver must have a valid vor or loc signal or active gps course for the flight director to enter approach mode. Approach mode is activated when the...

  • Page 410

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-30 afcs loc approach mode allows the autopilot to fly a loc/ils approach with a glideslope. When loc approach mode is armed, glideslope mode is also armed automatically. Loc captures are inhibited if the difference bet...

  • Page 411

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-31 afcs backcourse mode (bc) note: when making a backcourse approach, set the selected course to the localizer front course. Backcourse mode captures and tracks a localizer signal in the backcourse direction. The mode...

  • Page 412

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-32 afcs 7.5 autopilot and yaw damper operation note: refer to the poh/afm for specific instructions regarding emergency procedures. The hawker beechcraft c90a/gt autopilot and yaw damper operate the flight control surfa...

  • Page 413

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-33 afcs engagement note: autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use the cws button to disengage the pitch and roll servos while the autopilot remains active. When the a...

  • Page 414

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-34 afcs disengagement the autopilot is manually disengaged by pushing the ap key on the afcs control unit, the ga switch, or the mept arm switch. Manual autopilot disengagement is indicated by a five-second flashing yel...

  • Page 415

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-35 afcs 7.6 example flight plan note: the following example flight plan and diagrams (not to be used for navigation) in this section are for instructional purposes only and should be considered not current. Numbered po...

  • Page 416

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-36 afcs departure 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...

  • Page 417

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-37 afcs figure 7-37 departure selected altitude of 12,000 msl 1 2 3 4 hdg mode vs m ode alt mode to mode to mo d e kmkc.

  • Page 418

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-38 afcs 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 co...

  • Page 419

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-39 afcs flying a flight plan/gps course note: changing the navigation source cancels navigation mode and causes the flight director to revert back to roll hold mode (wings rolled level). As the aircraft closes on salin...

  • Page 420

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-40 afcs descent while flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to kcos. Three methods are presented for descent: • flight level change descent – flight level cha...

  • Page 421

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-41 afcs vertical path tracking descent to vnv target altitude: 1) select vnv flight control: a) press the vnv key to arm vertical path tracking mode. The white annunciation ‘vpth’ appears. B) using the alt sel knob, se...

  • Page 422

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-42 afcs non-path descent using flight level change mode: 1) using flight level change mode, command a non-path descent to an intermediate altitude above the next vnv flight plan altitude. A) using the alt sel knob, set...

  • Page 423

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-43 afcs figure 7-42 non-path descent habuk vnav target altitude of 10,000 msl vnav target altitude of 9,000 msl alt mode planned descent path selected altitude of 9,400 msl alt mode vpth mode 1 2 3 flc mode 4 vpth mod...

  • Page 424

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-44 afcs approach flying an ils approach: 1) transition from gps navigation mode to heading select mode. A) select the runway 35l ils approach for kcos and select ‘vectors’ for the transition. Load and activate the app...

  • Page 425

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-45 afcs flying a rnav gps approach with vertical guidance: 1) arm flight director modes for a rnav gps approach with vertical guidance: a) make sure the navigation source is set to gps (use cdi softkey to change naviga...

  • Page 426

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-46 afcs go around/missed approach note: as a result of calculations performed by the system while flying the holding pattern, the display may re-size automatically and the aircraft may not precisely track the holding p...

  • Page 427

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-47 afcs 4) the autopilot flies the holding pattern after the missed approach is activated. Annunciations are displayed in the navigation status box, above the afcs status box. Figure 7-45 go around/missed approach 3 4 ...

  • Page 428

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-48 afcs 7.7 afcs annunciations and alerts afcs status alerts the annunciations in table 7-5 (listed in order of increasing priority) can appear on the pfds above the airspeed and attitude indicators. Only one annuncia...

  • Page 429

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 7-49 afcs overspeed protection note: overspeed protection is not active in alt, gs or gp modes. While pitch hold, vertical speed, flight level change, vertical path tracking, or an altitude capture mode is active, airsp...

  • Page 430

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A 7-50 afcs b lank p age.

  • Page 431

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-1 additional features section 8 additional features note: the availability of safetaxi, chartview, or flitecharts in electronic form may not preclude the requirement to carry paper charts aboard the aircraft. Refer to the g1...

  • Page 432

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-2 additional features any map page that displays the navigation view can also show the safetaxi airport layout within the maximum configured range. The following is a list of pages where the safetaxi feature can be seen: • na...

  • Page 433

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-3 additional features configuring safetaxi range: 1) while viewing the navigation map page, press the menu key to display the page menu. 2) turn the large fms knob to highlight the map setup menu option and press the ent key....

  • Page 434

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-4 additional features safetaxi cycle number and revision safetaxi database is revised every 56 days. Safetaxi is always available for use after the expiration date. When turning on the g1000, the power-up page indicates whet...

  • Page 435

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-5 additional features the safetaxi region, version, cycle, effective date, and expires date of the database cycle can also be found on the aux - system status page. Safetaxi information appears in blue and yellow text. The e...

  • Page 436

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-6 additional features the other two possible aux - system status page conditions are shown here. The effective date is the beginning date for this database cycle. Expires date is the revision date for the next database cycle...

  • Page 437

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-7 additional features 8.2 chartview chartview resembles the paper version of jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The mfd depiction shows the aircraft position on ...

  • Page 438

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-8 additional features terminal procedures charts selecting terminal procedures charts: while viewing the navigation map page, nearest airport page, or flight plan page, select the shw chrt softkey. Or : 1) press the menu key...

  • Page 439

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-9 additional features if there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner unable to display chart is then displayed. Figure 8-10 unable to display chart banner w...

  • Page 440

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-10 additional features selecting a chart: 1) while viewing the navigation map page, flight plan page, or nearest airports page, select the shw chrt softkey. The airport diagram or approach chart is displayed on the airport i...

  • Page 441

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-11 additional features selecting the chrt softkey switches between the chartview diagram and the associated map in the wpt page group. In the example shown, the chrt softkey switches between the gainesville, fl (kgnv) airpor...

  • Page 442

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-12 additional features selecting the info softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the info softkey has no effect. The aircraft position is ...

  • Page 443

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-13 additional features in the example shown in figure 8-13, the class b chart is selected. Pressing the ent key displays the charlotte class b airspace chart (figure 8-14). Figure 8-14 airport information page, class b chart...

  • Page 444

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-14 additional features selecting the star softkey displays the standard terminal arrival chart if available. Figure 8-16 arrival information page aircraft not shown icon change range and scroll through the chart with the joy...

  • Page 445

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-15 additional features selecting the wx softkey shows the airport weather frequency information, and includes weather data such as metar and taf from the xm data link receiver, when available. Weather information is availabl...

  • Page 446

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-16 additional features note: a subdued softkey label indicates the function is disabled. Recent notams applicable to the current chartview cycle are included in the chartview database. Selecting the notam softkey shows the l...

  • Page 447

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-17 additional features figure 8-20 airport information page, local notams local notam on this airport notam softkey selected selecting the notam softkey again removes the notams information. Selecting the go back softkey rev...

  • Page 448

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-18 additional features chart options selecting the chrt opt softkey displays the next level of softkeys, the chart options level (figure 8-7). Selecting the all softkey shows the entire approach chart on the screen. Entire c...

  • Page 449

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-19 additional features selecting the header softkey shows the header view (approach chart briefing strip) on the screen. Approach chart briefing strip figure 8-22 approach information page, header view selecting the plan softk...

  • Page 450

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-20 additional features selecting the profile softkey displays the approach chart descent profile strip. Approach chart descent profile strip figure 8-24 approach information page, profile view, full screen width selecting the m...

  • Page 451

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-21 additional features if the chart scale has been adjusted to view a small area of the chart, selecting the fit width softkey changes the chart size to fit the available screen width. Select fit wdth softkey to show full cha...

  • Page 452

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-22 additional features selecting the full scn softkey alternates between removing and replacing the data window to the right. Selecting additional information: 1) while viewing the airport taxi diagram, select the full scn s...

  • Page 453

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-23 additional features the full screen view can also be selected by using the page menu option. Selecting full screen on or off: 1) while viewing a terminal chart press the menu key to display the page menu options. 2) turn ...

  • Page 454

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-24 additional features day/night view chartview can be displayed on a white or black background for day or night viewing. The day view offers a better presentation in a bright environment. The night view gives a better prese...

  • Page 455

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-25 additional features figure 8-30 arrival information page, day view figure 8-31 arrival information page, night view.

  • Page 456

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-26 additional features chartview cycle number and expiration date chartview database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. Chart...

  • Page 457

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-27 additional features examples of four possible power-up page conditions are shown here. Chartview disables plus a date in white, indicates chart data is current. This indication for normal operation shows how long the char...

  • Page 458

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-28 additional features note: a subdued softkey label indicates the function is disabled. The chartview time critical information can also be found on the aux - system status page. The database cycle number, expires, and disa...

  • Page 459

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-29 additional features the other three possible aux - system status page conditions are shown here. The expires date, in yellow, is the revision date for the next database cycle. The disables date, in yellow, is the date tha...

  • Page 460

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-30 additional features 8.3 flitecharts flitecharts resemble the paper version of national aeronautical charting office (naco) terminal procedures charts. The charts are displayed with high-resolution and in color for applicab...

  • Page 461

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-31 additional features terminal procedures charts selecting terminal procedures charts: while viewing the navigation map page, nearest airport page, or flight plan page, select the shw chrt softkey. Or : 1) press the menu ke...

  • Page 462

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-32 additional features if there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner unable to display chart is then displayed. Figure 8-38 unable to display chart banner ...

  • Page 463

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-33 additional features selecting a chart: 1) while viewing the navigation map page, flight plan page, or nearest airports page, select the shw chrt softkey. The airport diagram or approach chart is displayed on the airport i...

  • Page 464

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-34 additional features selecting the chrt softkey switches between the flitecharts diagram and the associated map in the wpt page group. In the example shown, the chrt softkey switches between the gainesville, fl (kgnv) airp...

  • Page 465

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-35 additional features selecting the info softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the info softkey has no effect. Another source for additi...

  • Page 466

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-36 additional features in the example shown in figure 8-41, alternate minimums is selected. Pressing the ent key displays the ifr alternate minimums chart (figure 8-42). Figure 8-42 airport information page, alternate minimu...

  • Page 467

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-37 additional features selecting the star softkey displays the standard terminal arrival chart if available. Figure 8-44 arrival information page selecting the apr softkey displays the approach chart for the airport if avail...

  • Page 468

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-38 additional features selecting the wx softkey shows the airport weather frequency information, when available, and includes weather data such as metar and taf from the xm data link receiver. Weather information is availabl...

  • Page 469

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-39 additional features chart options selecting the chrt opt softkey displays the next level of softkeys, the chart options level (figure 8-35). Selecting the all softkey shows the entire chart on the screen. Entire chart sho...

  • Page 470

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-40 additional features selecting the fit width softkey fits the width of the chart in the display viewing area. In the example shown, the chart at close range is replaced with the full width chart. Figure 8-48 approach inform...

  • Page 471

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-41 additional features selecting the full scn softkey alternates between removing and replacing the data window to the right. Figure 8-49 airport information page, full screen and info window select full scn softkey to switc...

  • Page 472

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-42 additional features the full screen view can also be selected by using the page menu option. Selecting full screen on or off: 1) while viewing a terminal chart press the menu key to display the page menu options. 2) turn ...

  • Page 473

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-43 additional features day/night view flitecharts can be displayed on a white or black background for day or night viewing. The day view offers a better presentation in a bright environment. The night view gives a better pre...

  • Page 474

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-44 additional features figure 8-52 approach information page, day view figure 8-53 approach information page, night view.

  • Page 475

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-45 additional features flitecharts cycle number and expiration date flitecharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. Flite...

  • Page 476

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-46 additional features examples of four possible power-up page messages are shown here. Flitecharts expires plus a date in white, indicates the chart database is current. Chart data is out of date! In yellow, indicates chart...

  • Page 477

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-47 additional features note: a subdued softkey label indicates the function is disabled. Flitecharts time critical information can also be found on the aux - system status page. The flitecharts database region, cycle number,...

  • Page 478

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-48 additional features the other three possible aux - system status page conditions are shown here. The expires date, in yellow, is the revision date for the next database cycle. The disables date, in yellow, is the date tha...

  • Page 479

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-49 additional features 8.4 xm radio entertainment (optional) note: refer to the hazard avoidance section for information about xm weather products. The optional xm radio entertainment feature of the gdl 69a data link receive...

  • Page 480

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-50 additional features note: the lock softkey on the xm information page (auxiliary page group) is used to save gdl 69a activation data when the xm services are initially set up. It is not used during normal xm radio operati...

  • Page 481

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-51 additional features using xm radio the xm radio page provides information and control of the audio entertainment features of the xm satellite radio. Selecting the xm radio page: 1) turn the large fms knob to select the au...

  • Page 482

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-52 additional features active channel and channel list the active channel box on the xm radio page displays the currently selected channel that the xm radio is using. The channels list box of the xm radio page shows a list o...

  • Page 483

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-53 additional features category the category box of the xm radio page displays the currently selected category of audio. Categories of channels such as jazz, rock, or news can be selected to list the available channels for a...

  • Page 484

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-54 additional features presets up to 15 channels from any category can be assigned a preset number. The preset channels are selected by selecting the presets and more softkeys. Then the preset channel can be selected directl...

  • Page 485

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-55 additional features 8.5 scheduler the scheduler feature can be used to enter and display reminder messages (e.G., hot section inspection or phase 1 maintenance check) in the alerts window on the pfd. Messages can be set t...

  • Page 486

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-56 additional features 9) for event-based messages: a) use the fms knob to enter the desired date (dd-mm-yy) and press the ent key. B) press the ent key again or use the large fms knob to move the cursor to the next field. C)...

  • Page 487

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-57 additional features 8.6 abnormal operation gdl 69/69a data link receiver troubleshooting some quick troubleshooting steps listed below can be performed to find the possible cause of a failure. • ensure the owner/operator o...

  • Page 488

    Garmin g1000 pilot’s guide for the beechcraft c90a/gt 190-00663-00 rev. A 8-58 additional features if a failure still exists, the following messages may provide insight as to the possible problem: message message location description check antenna xm radio page - active channel field data link receiv...

  • Page 489

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-1 appendix a annunciations and alerts note: the pilot’s operating handbook and faa approved airplane flight manual (afm/poh) supersedes information found in this document. The g1000 alerting system conveys alerts usin...

  • Page 490

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-2 appendix a • audio alerting system: the g1000 system issues audio alert tones when specific system conditions are met. See the alert level definitions section for more information. The annunciation tone may be tested ...

  • Page 491

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-3 appendix a alert level definitions the g1000 alerting system, as installed in hawker beechcraft c90a/gt aircraft, uses three alert levels. • warning: this level of alert requires immediate attention. Warning alert t...

  • Page 492

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-4 appendix a voice alerts the following audio alerts are announced by the system using a voice of male or female gender (see the aux - system setup page for the default configured voice gender; contact a garmin-authori...

  • Page 493

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-5 appendix a reversionary sensor annunciations reversionary sensor selection is annunciated in the reversionary sensor window, as shown in figure a-2. These annunciations reflect reversionary sensors selected on one or...

  • Page 494

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-6 appendix a figure a-3 g1000 system messages messages window alerts softkey annunciation system annunciation red ‘x’ figure a-4 g1000 system failure annunciations gdc 74b air data computer gtx 33 transponder or gia 6...

  • Page 495

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-7 appendix a note: upon power-up, certain windows remain invalid as g1000 equipment begins to initialize. All windows should be operational within one minute of power-up. If any window continues to remain flagged, the ...

  • Page 496

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-8 appendix a system annunciation comment gps information is either not present or is invalid for navigation use. Note that ahrs utilizes gps inputs during normal operation. Ahrs operation may be degraded if gps signal...

  • Page 497

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-9 appendix a mfd & pfd message advisories (cont.) message comments mfd1 config – mfd1 configuration error. Config service req’d. The mfd configuration settings do not match backup configuration memory. The g1000 system sh...

  • Page 498

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-10 appendix a database message advisories (cont.) message comments mfd1 db err – mfd1 terrain database error exists. The mfd and/or pfd detected a failure in the terrain database. Ensure that the terrain card is prope...

  • Page 499

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-11 appendix a database message advisories (cont.) message comments mfd1 db err – mfd1 safe taxi database error exists. The mfd and/or pfd detected a failure in the safe taxi database. Ensure that the data card is prop...

  • Page 500

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-12 appendix a gma 1347d message advisories message comments gma1 fail – gma1 is inoperative. The audio panel self-test has detected a failure. The audio panel is unavailable. The g1000 system should be serviced. Gma2 ...

  • Page 501

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-13 appendix a gia 63w message advisories (cont.) message comments hw mismatch – gia hardware mismatch. Gia1 communication halted. A gia mismatch has been detected, where only one is waas capable. The g1000 system shou...

  • Page 502

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-14 appendix a gia 63w message advisories (cont.) message comments gps1 service – gps1 needs service. Return unit for repair. A failure has been detected in the gps1 and/or gps2 receiver. The receiver may still be avai...

  • Page 503

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-15 appendix a gtx 33 message advisories message comments xpdr1 config – xpdr1 config error. Config service req’d. The transponder configuration settings do not match those of backup configuration memory. The g1000 system ...

  • Page 504

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-16 appendix a grs 77 message advisories (cont.) message comments ahrs mag db – ahrs magnetic model database version mismatch. The #1 ahrs and #2 ahrs magnetic model database versions do not match. Ahrs1 srvc – ahrs1 m...

  • Page 505

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-17 appendix a gdc 74b message advisories message comments adc1 alt ec – adc1 altitude error correction is unavailable. Gdc1 or gdc2 is reporting that the altitude error correction is unavailable. The g1000 system shou...

  • Page 506

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-18 appendix a gwx 68 message advisories message comments gwx config – gwx config error. Config service req’d. Gwx 68 configuration settings do not match those of the gdu configuration. The g1000 system should be serviced....

  • Page 507

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-19 appendix a miscellaneous message advisories (cont.) message comments arspc near – airspace near and ahead. Special use airspace is near and ahead of the aircraft position. Arspc near – airspace near – less than 2 n...

  • Page 508

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-20 appendix a afcs alerts figure a-5 afcs system status field system status field the following alert annunciations appear in the afcs system status field on the pfd. Condition annunciation description pitch failure pi...

  • Page 509

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt a-21 appendix a taws alerts annunciations appear on both pfds and the mfd. Pop-up alerts appear only on the mfd. Alert type pfd/mfd taws page annunciation mfd map page pop-up alert aural message excessive descent rate w...

  • Page 510

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A a-22 appendix a taws system status annunciations alert type pfd/mfd taws page annunciation mfd pop-up alert aural message taws system test fail none “taws system failure” taws alerting is disabled none none no gps posit...

  • Page 511

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt b-1 appendix b sd card use the g1000 system uses secure digital (sd) cards to load and store various types of data. For basic flight operations, sd cards are required for database storage as well as jeppesen aviation and...

  • Page 512

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A b-2 appendix b 4) after the update completes, the pfd starts in normal mode. 5) turn the g1000 system off and remove the sd card. 6) repeat steps 1 through 4 for the other pfd and the mfd. The mfd and pfd databases are ...

  • Page 513

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt b-3 appendix b the obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is very important to no...

  • Page 514

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A b-4 appendix b figure b-4 database information on the splash screen 3) acknowledge the power-up page agreement by pressing the ent key or the right most softkey. 4) turn the large fms knob to select the aux page group o...

  • Page 515

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt c-1 appendix c acc accuracy act, actv active, activate adc air data computer adf automatic direction finder adi attitude direction indicator af arc to fix afcs automatic flight control system afm airplane flight manual a...

  • Page 516

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A c-2 appendix c course the line between two points to be followed by the aircraft. Course to steer the recommended direction to steer in order to reduce course error or stay on course. Provides the most efficient heading ...

  • Page 517

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt c-3 appendix c ent enter epe estimated position error epu estimated position uncertainty err error esa enroute safe altitude estimated position error a measure of horizontal gps position error derived by satellite geome...

  • Page 518

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A c-4 appendix c gtx garmin transponder ha hold terminating at altitude hdg heading heading the direction an aircraft is pointed, based upon indications from a magnetic compass or a properly set directional gyro. Hf hold ...

  • Page 519

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt c-5 appendix c loc localizer loi loss of integrity (gps) lon longitude lpv localizer performance with vertical guidance lru line replacement unit lt left ltng lightning lvl level m middle marker m meter mag magnetic mag...

  • Page 520

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A c-6 appendix c ptk parallel track ptt push-to-talk pwr power qty quantity r right, right runway rad radial raim receiver autonomous integrity monitoring ram random access memory ref reference rem remaining (fuel remaini...

  • Page 521

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt c-7 appendix c tf track between two fixes tfr temporary flight restriction t hdg true heading tis traffic information system tit turbine inlet temperature tke track angle error tma terminal maneuvering area tmr/ref timer...

  • Page 522

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A c-8 appendix c b lank p age.

  • Page 523

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt d-1 appendix d frequently asked questions if a particular aspect of g1000 operational capability is not addressed by these commonly asked questions or in the index, contact garmin (see the copyright page or back cover f...

  • Page 524

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A d-2 appendix d for raim to work correctly, the gps receiver must track at least five satellites. A minimum of six satellites is required to allow raim to eliminate a single corrupt satellite from the navigation solution....

  • Page 525

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt d-3 appendix d normal (obs not activated) • automatic sequencing of waypoints • manual course change on hsi not possible • always navigates ‘to’ the active waypoint • must be in this mode for final approach course obs • ...

  • Page 526

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A d-4 appendix d w hen does the cdi scale change ? When set to ‘auto’ (default), the gps cdi scale automatically adjusts to the desired limits based upon the current phase of flight (figure 2-31, 2-32, 2-33, table 2-2). • ...

  • Page 527

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt d-5 appendix d w hy does the hsi not respond like a vor when obs mode is active ? Unlike a vor, the cdi scale used on gps equipment is based on the crosstrack distance to the desired course, not on the angular relations...

  • Page 528

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A d-6 appendix d b lank p age.

  • Page 529

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt e-1 appendix e airport item symbol unknown airport non-towered, non-serviced airport towered, non-serviced airport non-towered, serviced airport towered, serviced airport restricted (private) airport heliport navaids it...

  • Page 530

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A e-2 appendix e miscellaneous item symbol artcc frequency or fss frequency default map pointer elevation pointer wind vector measuring pointer overzoom indicator terrain proximity or taws enabled traffic enabled user wayp...

  • Page 531

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt e-3 appendix e terrain avoidance colors and symbols terrain color terrain location red (warning...

  • Page 532

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A e-4 appendix e hazard avoidance features this table identifies the symbols displayed in the lower right corner of pfd or mfd maps to indicate which hazard avoidance features are activated for display. Feature symbol taws...

  • Page 533

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt i-1 index a activate a flight plan -------------------------------------5-76 active channel --------------------------------------------8-52 active frequency ------------------------------------ 4-6, 4-16 adf audio ----...

  • Page 534

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A i-2 index command bars ----------------------------------------2-7, 7-7 communication (com) frequency box ----------------- 2-2 comparator ------------------------------------------------- a-4 comparator window --------...

  • Page 535

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt i-3 index go around mode --------------------------7-23, 7-46–7-47 groundspeed ----------------------------------------------1-45 ground mapping ------------------------------------------6-49 grs 77 --------------------...

  • Page 536

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A i-4 index oil pressure (oil psi) -------------------------------------- 3-2 omni bearing selector (obs) ----------------------- d-2–d-3 other statistics --------------------------------- 5-107, 5-109 outside air tempera...

  • Page 537

    190-00663-00 rev. A garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt i-5 index topo data --------------------------------- 5-15, 5-16, 5-25 topo scale -----------------------------------------------5-17 top of descent --------------------------------- 5-133, 5-134 track -----------------...

  • Page 538

    Garmin g1000 pilot’s guide for the hawker beechcraft c90a/gt 190-00663-00 rev. A i-6 index b lank p age.