Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN

NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the G1000 Flight Manual Supplement. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airman’s Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” CAUTION: The GDU 1040 & 1042 PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN WARNINGS, CAUTIONS, & 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 both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the Strike Display Mode. However, clusters of two or more discharge points in the Strike Display Mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system. Depictions of equipment may differ slightly from the actual equipment. NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00450-01 Reformat of manual Added WX 500 Stormscope Added XM Weather Added ADF/DME Added extended range fuel tanks Changes in EIS softkey labels 190-00450-02 Added TAWS-B Added Automatic Flight Control System Changed System Software Revision Revision Date of Revision Affected Pages Description A 12/05 i-Index-2 Initial release B 4/06 2-4 11-2 12-1 Added Altitude Alert and Barometric Minimums info. Added Hazard Displays with Loss of GPS info. Added inactive alerts info. C 6/06 3-1 – 3-2 5-1 6-1 Added M20TN Engine page descriptions Updated Section 5.3 Added note regarding M20TN autopilot D 7/06 RR-1 2-4 12-7 Corrected Revision Date Added S-TEC only info Added S-TEC only info Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN RR-2 RECORD OF REVISIONS Blank Page Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN i TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 PFD/MFD Controls................................................... 1-2 1.2 PFD Softkeys............................................................ 1-4 1.3 MFD Softkeys .......................................................... 1-7 1.4 MFD Page Groups ................................................... 1-8 1.5 Backlighting ............................................................. 1-8 SECTION 2: FLIGHT INSTRUMENTS .............................. 2-1 2.1 Airspeed Indicator.................................................. 2-3 Speed Indication ......................................................... 2-3 Speed Ranges ............................................................. 2-3 Airspeed Trend Vector ................................................. 2-3 Vspeed References ...................................................... 2-3 2.2 Attitude Indicator .................................................. 2-3 2.3 Altimeter .................................................................. 2-4 Altitude Select Bug ...................................................... 2-4 Altitude Trend Vector ................................................... 2-4 Barometric Setting Box ................................................ 2-4 Altitude Alerting .......................................................... 2-4 Barometric Minimum Descent Altitude ......................... 2-4 2.4 Vertical Deviation/Glideslope Indicator ............ 2-5 2.5 Marker Beacon Annunciations ............................ 2-5 2.6 Vertical Speed Indicator ....................................... 2-5 2.7 Horizontal Situation Indicator (HSI) ................... 2-6 Arc HSI ....................................................................... 2-6 Turn Rate Indicator and Heading Trend Vector .............. 2-6 Course Pointer ............................................................ 2-7 Course Deviation Indicator (CDI) .................................. 2-7 Bearing Pointers and Information Windows .................. 2-7 DME (optional)............................................................ 2-8 Navigation Source ....................................................... 2-8 SECTION 3: ENGINE INDICATION SYSTEM (EIS).... 3-1 3.1 Engine Display......................................................... 3-1 3.2 Lean Engine Display ............................................... 3-1 Cylinder Select ............................................................ 3-1 3.3 Engine System Display .......................................... 3-2 3.4 Flap & Trim Indications.......................................... 3-2 Rudder Trim Indicator .................................................. 3-2 Elevator Trim Indicator ................................................. 3-2 Flaps Position Indicator ............................................... 3-2 SECTION 4: NAV/COM AND TRANSPONDER ........... 4-1 4.1 Radio Status Indications ....................................... 4-3 4.2 Volume ...................................................................... 4-3 4.3 Automatic Squelch ................................................. 4-3 4.4 Quickly Activating 121.500 MHz .......................... 4-3 4.5 Optional NAV Radios ............................................. 4-3 ADF Radio (optional) ................................................... 4-3 DME Radio (optional) .................................................. 4-4 4.6 Frequency Auto-tuning ......................................... 4-4 Auto-tuning on the PFD .............................................. 4-4 Auto-tuning on the MFD ............................................. 4-4 4.7 Transponder ............................................................. 4-5 Mode Selection ........................................................... 4-5 Ground Mode (Automatic) ...................................... 4-5 Reply Status ........................................................... 4-5 Code Selection ....................................................... 4-5 Flight ID Reporting ...................................................... 4-5 SECTION 5: AUDIO PANEL ................................................ 5-1 5.1 COM Radio Selection ............................................. 5-2 5.2 Split COM Function ................................................ 5-2 5.3 Marker Beacon Receiver ....................................... 5-2 Marker Beacon Signal Sensitivity ................................. 5-3 5.4 Nav Radio Audio Selection ................................... 5-3 5.5 Intercom System (ICS) Isolation .......................... 5-3 5.6 Intercom Squelch Control ..................................... 5-4 5.7 Digital Clearance Recorder and Playback......... 5-4 SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1 6.1 Mode Annunciations .............................................. 6-2 6.2 Overspeed Protection ........................................... 6-2 6.3 AP Engagement/Disengagement ........................ 6-3 Automatic Disengagement .......................................... 6-3 Manual Disengagement .............................................. 6-3 Control Wheel Steering................................................ 6-3 6.4 Loss of Data ............................................................. 6-4 6.5 Pitch Axis Modes .................................................... 6-4 Pitch Hold Mode (PIT) ................................................. 6-5 Altitude Hold Mode (ALT) ............................................ 6-6 Vertical Speed Mode (VS) ............................................ 6-7 Flight Level Change Mode (FLC) .................................. 6-8 Go-Around Mode (GA) ................................................ 6-9 Glideslope (GS) ........................................................... 6-9 6.6 Roll Axis Modes..................................................... 6-10 Roll Hold Mode (ROL)................................................ 6-10 Heading Select Mode (HDG) ...................................... 6-11 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN ii TABLE OF CONTENTS Navigation Mode (GPS, VOR, LOC, or BC)................... 6-12 Navigation Mode Armed....................................... 6-12 Approach Mode (GPS, VAPP or LOC) .......................... 6-13 Go Around (GA) ........................................................ 6-13 6.7 Example Procedures Using AFCS ....................... 6-14 Departure ................................................................. 6-15 Intercepting a VOR Radial .......................................... 6-16 Flying a Flight Plan / GPS Course ............................... 6-17 Flight Level Change (Descent).................................... 6-18 ILS Approach ............................................................. 6-19 Go-Around / Missed Approach................................... 6-20 SECTION 7: NAVIGATION .................................................. 7-1 7.1 Navigation Map Page ............................................ 7-1 Select the MAP Page Group......................................... 7-1 7.2 Direct-to Navigation .............................................. 7-1 Direct-to Navigation from the MFD .............................. 7-1 Enter a Direct-to Destination .................................. 7-1 Select a Direct-to Destination to a Flight Plan Waypoint or Nearest Airport ................................... 7-1 To Re-center the CDI to the Destination Waypoint ... 7-2 To Manually Define the Direct-to Course ................. 7-2 Canceling Direct-to Navigation ............................... 7-2 Direct-to Navigation from the PFD ............................... 7-2 Cancelling Direct-to Navigation .............................. 7-2 7.3 Airport Information ............................................... 7-3 Select the Airport Information Page ............................. 7-3 Enter a Waypoint Facility Name or City Location ...... 7-3 Access Runway Information .................................... 7-3 Access Frequency Information ................................. 7-3 7.4 Intersection Information ...................................... 7-4 Select the Intersection Information Page ...................... 7-4 Access Information on an Intersection..................... 7-4 7.5 NDB Information..................................................... 7-4 Select the NDB Information Page ................................. 7-4 View Information on a Specific NDB........................ 7-4 7.6 VOR Information ..................................................... 7-5 Select the VOR Information Page ................................. 7-5 Access Information on a VOR .................................. 7-5 7.7 User Waypoint Information Page ....................... 7-5 7.8 Nearest Airports ..................................................... 7-5 Nearest Airport Information on the MFD ...................... 7-5 Select the Nearest Airports Page ............................. 7-5 Access Information on a Specific Airport ................. 7-6 Access Runway Information for the Selected Airport ................................................................... 7-6 Quickly Tune the COM Transceiver to a Nearby Airport Frequency ................................................... 7-6 Nearest Airports Information on the PFD ...................... 7-6 View Information on a Specific Airport in the List .... 7-6 Load an Airport COM Frequency into the Active COM ........................................................... 7-6 7.9 Nearest Intersections ............................................ 7-7 Select the Nearest Intersections Page ........................... 7-7 View Information on the Nearest Intersection.......... 7-7 7.10 Nearest NDB ............................................................ 7-7 Select the Nearest NDB Page ....................................... 7-7 Access Information on a Specific NDB ..................... 7-7 7.11 Nearest VOR ............................................................. 7-8 Select the Nearest VOR Page ....................................... 7-8 View Information on the Nearest VOR ..................... 7-8 Select and Load a VOR Frequency ........................... 7-8 7.12 Nearest User Waypoint.......................................... 7-9 Select the Nearest User Waypoint Page ........................ 7-9 Select a Nearest User Waypoint .............................. 7-9 7.13 Nearest Frequencies .............................................. 7-9 Select the Nearest Frequencies Page ............................ 7-9 Select and Load the Nearest ARTCC, FSS, or Weather Frequency ............................................. 7-9 7.14 NEAREST AIRSPACES ............................................ 7-10 Select the Nearest Airspaces Page.............................. 7-10 Airspace Alerts Box............................................... 7-10 View Additional Details for a Listed Airspace ......... 7-10 View and Quickly Load the Frequency for a Controlling Agency ............................................... 7-10 SECTION 8: FLIGHT PLANNING ...................................... 8-1 8.1 User Defined Waypoints........................................ 8-1 Select the User WPT Information Page ......................... 8-1 Create a New User Waypoint .................................. 8-1 Modify a User Waypoint ......................................... 8-1 Delete a User Waypoint .......................................... 8-1 Create User Waypoints from the Navigation Map Page ................................................................... 8-2 8.2 Viewing the Active Flight Plan ............................ 8-2 8.3 Activate a Stored Flight Plan ............................... 8-2 8.4 Activate a Flight Plan Leg .................................... 8-3 8.5 Stop Navigating a Flight Plan.............................. 8-3 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN iii TABLE OF CONTENTS 8.6 Invert Active Flight Plan ....................................... 8-3 8.7 Create a New Flight Plan ...................................... 8-4 Create a New Flight Plan Using the MFD ..................... 8-4 Create a New Flight Plan Using the PFD ...................... 8-4 8.8 Load a Departure ................................................... 8-4 8.9 Load an Arrival ........................................................ 8-5 8.10 Load an Approach .................................................. 8-5 8.11 Remove a Departure, Arrival, or Approach from a Flight Plan ................................................... 8-5 8.12 Store a Newly Created Flight Plan ..................... 8-5 8.13 Edit a Stored Flight Plan ....................................... 8-5 8.14 Delete a Waypoint from the Flight Plan............ 8-5 8.15 Invert and activate a Stored Flight Plan ........... 8-6 8.16 Copy a Flight Plan .................................................. 8-6 8.17 Delete a Flight Plan ............................................... 8-6 8.18 Graphical Flight Plan Creation ............................ 8-6 8.19 Trip Planning............................................................ 8-6 8.20 Vertical Navigation (VNAV) Page ........................ 8-8 Create a Vertical Navigation Profile .............................. 8-8 VNAV Page Menu Options ........................................... 8-9 SECTION 9: PROCEDURES ................................................ 9-1 9.1 Arrivals and Departures........................................ 9-1 Load and Activate a Departure Procedure .................... 9-1 Load and Activate An Arrival Procedure ........................ 9-1 9.2 Approaches .............................................................. 9-2 Load and/or Activate an Approach Procedure ............... 9-2 Activate An Approach in the Active Flight Plan ............. 9-3 SECTION 10: HAZARD AVOIDANCE ........................... 10-1 10.1 Customizing the Hazard Displays on the Navigation Map .................................................... 10-1 10.2 STORMSCOPE® (Optional) .................................. 10-1 Displaying Stormscope Lightning Data on the Navigation Map Page ................................................ 10-1 Stormscope Page....................................................... 10-2 10.3 XM Weather (Optional) ....................................... 10-3 Displaying METAR and TAF information on the Airport Information Page ...................................................... 10-3 Displaying Weather on the Weather Data Link Page ... 10-4 NEXRAD Limitations ............................................. 10-4 Map Panning Information – Weather Data Link Page . 10-5 Weather Products and Symbols ................................. 10-5 Weather Product Age ................................................ 10-6 10.4 Traffic Information Service (TIS) ....................... 10-7 Displaying Traffic on the Traffic Map Page................... 10-7 Displaying Traffic on the Navigation Map ................... 10-7 TIS Audio Alert .......................................................... 10-7 10.5 Skywatch Traffic Advisory System (TAS)(Optional) ...................................................... 10-8 Displaying Traffic on the Traffic Map Page................... 10-8 Displaying Traffic on the Navigation Map ................... 10-8 10.6 Terrain And Obstacle Proximity ........................ 10-9 Displaying Terrain and Obstacles on the Terrain Proximity Page .......................................................... 10-9 Displaying Terrain and Obstacles on the Navigation Map.......................................................................... 10-9 10.7 Terrain Awareness & Warning System (TAWS) Display (Optional) .............................................. 10-11 Displaying Terrain on the TAWS Page ....................... 10-11 Enable/Disable Aviation Data ................................... 10-12 TAWS Inhibit ........................................................... 10-12 Manual System Test ................................................. 10-13 Forward Looking Terrain Avoidance (FLTA) ................ 10-13 Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) ...... 10-13 Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) .......................................... 10-13 Premature Descent Alert (PDA) ................................ 10-14 Excessive Descent Rate Alert (EDR) .......................... 10-14 Negative Climb Rate After TakeoffAlert (NCR) .......... 10-14 “Five-Hundred” Aural Alert...................................... 10-15 Displaying Terrain and Obstacles on the Navigation Map........................................................................ 10-15 Pop-up Alerts .......................................................... 10-15 TAWS Alerts Summary ............................................. 10-16 Alert Annunciations ................................................. 10-17 SECTION 11: ABNORMAL OPERATION ..................... 11-1 11.1 Reversionary Mode .............................................. 11-1 11.2 Abnormal COM Operation .................................. 11-2 11.3 Unusual Attitudes ................................................. 11-2 11.4 Stormscope operation with loss of Heading Input........................................................ 11-2 11.5 Hazard Displays with Loss of GPS Position .... 11-2 SECTION 12: ANNUNCIATIONS & ALERTS .............. 12-1 12.1 Alert Level Definitions ........................................ 12-2 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN iv TABLE OF CONTENTS 12.2 M20M/M20R/M20TN Aircraft Alerts .................. 12-2 Voice Alerts ............................................................... 12-2 Message Advisory Alerts ............................................ 12-2 12.3 AFCS Alerts............................................................. 12-3 System Status Field ................................................... 12-3 12.4 TAWS ALERTS ......................................................... 12-4 TAWS System Status Annunciations ........................... 12-5 12.5 G1000 System Annunciations ............................ 12-5 Traffic Voice Alerts ..................................................... 12-7 Audio Alerts .............................................................. 12-7 12.6 G1000 System Message Advisories .................. 12-8 MFD & PFD Message Advisories................................. 12-9 Database Message Advisories .................................. 12-10 GMA 1347 Message Advisories ............................... 12-11 GIA 63 Message Advisories ..................................... 12-11 GIA 63 Message Advisories (Cont.) .......................... 12-12 GEA 71 Message Advisories .................................... 12-13 GTX 33 Message Advisories..................................... 12-14 GRS 77 Message Advisories..................................... 12-14 GMU 44 Message Advisories ................................... 12-15 GDL 69 Message Advisories..................................... 12-15 GDC 74A Message Advisories.................................. 12-15 Miscellaneous Message Advisories ........................... 12-16 Index.....................................................................................Index-1 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-1 SECTION 1 SYSTEM OVERVIEW 1-1 SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Mooney M20M, M20R, and M20TN Pilot’s Guide (190-00647-00). This guide gives the pilot abbreviated operating instructions for the Primary Flight Display (PFD), Multi Function Display (MFD), and the GMA 1347 Audio Panel System. NOTE: The pilot should read and thoroughly understand the Mooney M20M/M20R/M20TN Airplane Flight Manual Supplement (AFMS) for limitations, procedures, and operational information not contained in this Cockpit Reference Guide. The Mooney M20M/M20R/ M20TN Airplane Flight Manual Supplement always takes precedence over the information found in this guide. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-2 SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS Figure 1-1 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 17 12 13 11 10 16 15 14 20 21 19 18 26 25 24 22 23 27 MFD Only Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-3 SECTION 1 SYSTEM OVERVIEW Functionality of the PFD and MFD controls are the same with the exception of the dedicated autopilot keys located only on the MFD bezel. (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Toggle Key – Toggles the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields. (4) Heading Knob – Turn to manually select a heading on the HSI. When pressed, it synchronizes the Heading Bug with the compass lubber line. Selected Heading provides the heading reference to the Flight Director while operating in Heading Select Mode. (5) Joystick – Changes the map range when rotated. Activates the map pointer when pressed. (6) CRS/BARO Knob – The large knob sets the altimeter barometric pressure and the small knob adjusts the course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP Mode. Pressing this knob centers the CDI on the currently selected VOR. Selected Course provides course reference to the Flight Director when operating in Navigation and Approach modes. (7) Dual COM Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob toggles the tuning cursor (light blue box) between the COM1 and COM2 fields. (8) COM Frequency Toggle Key – Toggles the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121.5 MHz) in the active frequency field. (9) COM VOL/SQ Knob – Controls COM audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume level is shown in the field as a percentage. (10) Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by the identifier, chosen from the active route, or taken from the map cursor position). (11) FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. (12) CLR Key (DFLT MAP) – Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). (13) Dual FMS Knob – Used to select the page to be viewed (only on the MFD). The large knob selects a page group (MAP, WPT, AUX, NRST), while the small knob selects a specific page within the page group. Pressing the small knob turns the selection cursor ON and OFF. When the cursor is ON, data may be entered in the different windows using the small and large knobs. The large knob is used to move the cursor on the page, while the small knob is used to select individual characters for the highlighted cursor location. When the G1000 displays a list that is too long for the display screen, a scroll bar appears along the right side of the display, indicating the availability of additional items within the selected category. Press the Small FMS Knob to activate the cursor and turn the Large FMS Knob to scroll through the list. (14) MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. (15) PROC Key – Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. If a flight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARs), and approaches (IAPs) from the database and loads them into the active flight plan. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-4 SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. (17) Dual ALT Knob – Sets the reference altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds. Altitude Select is used by the Automatic Flight Control System in certain modes, in addition to the standard G1000 Altitude Alerter function. (18) AP Key – Engages/disengages the Autopilot and Flight Director in the default vertical and lateral modes. (19) FD Key – Activates/deactivates the Flight Director only. Pressing the FD Key turns on the Flight Director in the default pitch axis and roll axis modes. Pressing the FD Key again deactivates the Flight Director and removes the command bars, unless the Autopilot is engaged. If the Autopilot is engaged, the FD Key is disabled. (20) NAV Key – Selects/deselects the Navigation Mode. (21) ALT Key – Selects/deselects the Altitude Hold Mode. (22) VS Key – Selects/deselects the Vertical Speed Mode. (23) FLC Key – Selects/deselects the Flight Level Change Mode. (24) HDG Key – Selects/deselects the Heading Select Mode. (25) APR Key – Selects/deselects the Approach Mode. (26, 27) NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes. 1.2 PFD SOFTKEYS Softkey OFF Softkey ON OBS TMR/REF NRST INSET IDENT XPDR CDI PFD ALERTS ADF/DME (optional) Figure 1-2 PFD Top Level Softkeys INSET – Press to display the Inset Map in the lower left corner of the PFD. OFF – Press to remove the Inset Map. DCLTR (3) – Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR Softkey. • No declutter: All map features are visible • Declutter – 1: Declutters land data • Declutter – 2: Declutters land and SUA data • Declutter – 3: Removes everything except the active flight plan TRAFFIC – Press to display traffic on the map. TOPO – Press to display topographical data (i.e., coastlines, terrain, rivers, lakes, etc.) and elevation scale on the Inset Map TERRAIN – Press to display terrain information on the Inset Map. STRMSCP (optional) – Press to display the Stormscope lightning data on the Inset Map (within a 200 nm radius of the aircraft). NEXRAD (optional) – Press to display NEXRAD precipitation data on the Inset Map. XM LTNG (optional) – Press to display the XM® Radio lightning data on the Inset Map. BACK – Press to return to the previous level softkey configuration. ALERTS – Press to display the Alerts Window. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-5 SECTION 1 SYSTEM OVERVIEW PFD – Press to display the additional softkeys for additional configurations of the PFD. METRIC – Press to display the current and reference altitudes in meters, in addition to feet. Pressing the METRIC Softkey also changes the barometric setting to hectopascals. DFLTS – Press to reset default settings on the PFD. DME (optional) – Press to display the DME Information Window. BRG1 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the the appropriate information. INSET OFF TOPO TRAFFIC TERRAIN DCLTR DCLTR-2 DCLTR-3 DCLTR-1 NEXRAD Press the BACK or OFF softkey to return to the top level softkeys XM LTNG STRMSCP BACK ALERTS (optional) (optional) (optional) Figure 1-3 PFD Softkey Flow Chart – 1 PFD Press the STD BARO or BACK softkeys to return to the top level softkeys Press the DFLTS softkey to change the PFD metric values to standard ARC HSI 360 HSI STD BARO BACK ALERTS BRG2 BRG1 METRIC DFLTS DME (optional) Figure 1-4 PFD Softkey Flow Chart – 2 NAV1 – Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window. ADF – Displays ADF waypoint frequency in the BRG1 Information Window. OFF – Removes the BRG1 Information Window. 360 HSI – Press to display the 360° compass rose. ARC HSI – Press to display the 140° viewable arc. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-6 SECTION 1 SYSTEM OVERVIEW BRG2 (bearing) – Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the the appropriate information. NAV2 – Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window. GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF waypoint frequency in the BRG2 Information Window. OFF – Removes the BRG2 Information Window. STD BARO – Press to set the barometric pressure to 29.92 inches of mercury (1013 hPa by pressing the METRIC Softkey). BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. NRST OBS TMR/REF IDENT ALERTS XPDR STBY ON BACK VFR ALT CODE IDENT 0 1 6 3 2 4 5 7 IDENT BACK BKSP Press the BACK softkey to return to the top level softkeys Press the BACK softkey to return to the top level softkeys ALERTS ALERTS ADF/DME (optional) CDI CDI (VOR1) CDI (VOR2) GPS Figure 1-5 PFD Softkey Flow Chart – 3 OBS – Press to select OBS Mode on the CDI when navigating by GPS (only available with active leg). CDI – Press to change navigation mode on the CDI between GPS, VOR1, and VOR2. ADF/DME (optional) – Press to display the ADF/DME Tuning Window. XPDR – Press to display the transponder mode selection softkeys. STBY – Press to select Standby Mode. ON – Press to select Mode A. ALT – Press to select Altitude Reporting Mode. VFR – Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries). CODE – Press to display transponder code selection softkeys 0-7. 0 through 7 – Press numbers to enter code. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-7 SECTION 1 SYSTEM OVERVIEW BKSP – Press to remove numbers entered one at a time. BACK – Press to return to the previous level softkeys. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). BACK – Press to return to the previous level softkeys. ALERTS – Press to display the Alerts Window. IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports Window. ALERTS – Press to display the Alerts Window. Figure 1-6 MFD Softkeys BACK DEC FUEL SYSTEM ENGINE LEAN ENGINE MAP DCLTR BACK SYSTEM LEAN ENGINE ENGINE LEAN BACK SYSTEM TRAFFIC TOPO TERRAIN DCLTR-2 DCLTR-3 DCLTR-1 Press the BACK softkey on this level to return to the top softkey level BACK Press to return to the top softkey level CHKLIST ASSIST CYL SLCT EXIT EMERGCY ENGINE DCLTR MAP ENGINE CHKLIST CLR DONE The DONE softkey changes to UNDO when the checklist item is already checked STRMSCP NEXRAD XM LTNG (optional) (optional) (optional) RST FUEL INC FUEL (optional) Press the ENGINE or BACK softkey on any level to return to the default page level 1.3 MFD SOFTKEYS ENGINE – Pressing this softkey makes available the LEAN and SYSTEM softkeys which in turn access the Lean Page and the System Page, respectively. MAP – Pressing this softkey enables the following softkeys: TRAFFIC – Pressing this softkey displays/ removes Traffic on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map. TERRAIN – Pressing this softkey displays/ removes terrain and obstacle data on the Navigation Map. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 1-8 SECTION 1 SYSTEM OVERVIEW STRMSCP (optional) – Pressing this softkey displays/removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/removes precipitation data on the Navigation Map. XM LTNG (optional) – Pressing this softkey displays/removes XM Radio lightning data on the Navigation Map. BACK – Pressing this softkey displays the ENGINE and MAP top level softkeys. DCLTR (declutter) – Pressing this softkey removes map information in three levels. CHKLIST (checklist)(optional) – Pressing the CHKLIST Softkey displays the Checklist Page. 1.4 MFD PAGE GROUPS 1) Turn the Large FMS Knob until the desired page group is selected. 2) Turn the Small FMS Knob to select pages within the group. See Figure 1-7. Figure 1-7 Page Group Icon Map Page Group Waypoint Page Group Auxiliary Page Group Nearest Group Selected Page Number of Pages in Current Group 1.5 BACKLIGHTING To manually adjust the backlight for the PFD and MFD: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. 2) Press the Small FMS Knob to activate the cursor. ‘PFD DSPL > AUTO’ is now highlighted. 3) Turn the Small FMS Knob to display the selection window. 4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key. 5) With the intensity value now highlighted, turn the Small FMS Knob to select the desired backlighting. 6) Turn the Large FMS Knob to highlight ‘MFD DSPL > AUTO’ and repeat steps 3 through 5. Figure 1-8 PFD Setup Menu Window Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-1 SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated. 6 7 11 14 15 8 13 12 5 3 4 2 1 16 Figure 2-1 Default PFD Information 14 15 11 13 12 9 6 4 2 5 16 7 3 1 NAV Frequency Window Airspeed Indicator True Airspeed Box Outside Air Temperature Box Altitude Reference Box Horizontal Situation Indicator Heading Box System Time Box Transponder Status Bar Barometric Setting Box Vertical Speed Indicator Altimeter COM Frequency Window Navigation Status Bar 10 8 Slip/Skid Indicator Turn Rate Indicator 10 9 17 17 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-2 SECTION 2 FLIGHT INSTRUMENTS Figure 2-2 Additional PFD Information 4 7 8 1 3 6 2 10 Traffic Annunciation 2 4 3 1 Inset Map Selected Heading Box 5 DME Information Window BRG1 Information Window 5 6 BRG2 Information Window 8 Selected Course Box 7 Alerts Window Vertical Deviation/Glideslope Indicator Marker Beacon Annunciation 9 10 9 Figure 2-3 PFD Navigation Status Window Next Waypoint Distance to Next Waypoint Desired Track to Next Waypoint Current Track Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Figure 2-4 Airspeed Indicator Actual Airspeed Airspeed Trend Vector True Airspeed Box Speed Ranges Vspeed References Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Figure 2-5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps operating range, normal operating range, and never exceed speed (Vne). A red range is also present for low speed awareness. Refer to the Airplane Flight Manual (AFM) for airspeed limitations and indicator markings. Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Vspeed References Vspeed References are turned on or off in the Timer/References Window. Press the TMR/REF Softkey to display the widow. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. To activate the Vspeed References, display the Timer/References Window and turn the Large FMS Knob to place the cursor in the ON/OFF field. Turn the Small FMS Knob to select ON or OFF. 2.2 ATTITUDE INDICATOR The Slip/Skid Indicator is located under the roll pointer and moves laterally away from the pointer to indicate lateral acceleration. One Slip/Skid indicator displacement is equal to one ball displacement when compared to a traditional slip/skid indicator. Figure 2-6 Attitude Indicator 3 2 1 9 8 7 6 5 4 1 2 3 4 5 Roll Scale Horizon Line Aircraft Symbol Land Representation Roll Pointer 6 7 8 9 Aircraft Wing Tips Pitch Scale Sky Representation Slip/Skid Indicator Roll Scale Zero 10 10 Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-4 SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Selected Altitude Box Altitude Trend Vector Current Altitude Barometric Setting Box Figure 2-7 Altimeter Altitude Select Bug Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or, if the selected altitude is beyond the altitudes currently displayed, the bug is displayed at the top or bottom of the display (whichever is closest to the selected altitude). To set the Selected Altitude Bug: Turn the ALT Knob to set the Altitude Select Bug. The Small ALT Knob sets the hundreds and the Large ALT Knob sets the thousands. This altitude also appears in the Selected Altitude Box above the Altimeter. Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained. Barometric Setting Box To set barometric pressure, turn the BARO Knob to select the desired setting. Altitude Alerting Figure 2-8 Altitude Alerting Visual Annunciations Within 1000 ft Within 200 ft Deviation of ±200 ft (applicable to S-TEC AFCS only) Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System. An aural tone is heard when the aircraft is within 1000 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude. In addition to the preceding tones, for S-TEC AFCS equipped aircraft only, an aural tone is heard when the aircraft is within 200 feet of acquiring the selected altitude. Barometric Minimum Descent Altitude The desired barometric minimum descent altitude (MDA, or Decision Height, DH) can be set in the Timer/ References Window. Visual annunciations alert the pilot when approaching the MDA: • When the aircraft altitude descends to within 2500 feet of the MDA setting, the Barometric Minimum Box appears with the altitude in light blue text. The bug appears on the tape in light blue once in range. • When the aircraft passes through 100 feet of the MDA, the bug and text turn white. • Once the aircraft descends past the MDA, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated. Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-5 SECTION 2 FLIGHT INSTRUMENTS Within 100 ft Altitude Reached Within 2500 ft Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations Barometric Minimum Box Barometric Mini- mum Bug 2.4 VERTICAL DEVIATION/GLIDESLOPE INDICATOR The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV field. 2.5 MARKER BEACON ANNUNCIATIONS Figure 2-10 Marker Beacon and Vertical Deviation Marker Beacon Annunciation Vertical Deviation/Glideslope Indicator 2.6 VERTICAL SPEED INDICATOR Figure 2-11 Vertical Speed Indicator Vertical Speed Pointer Vertical Speed Bug Selected Vertical Speed The actual vertical speed is displayed inside the pointer. When the Flight Director is placed in Vertical Speed Mode (by pressing the VS Key) the Vertical Speed Bug is displayed. Press the NOSE UP or NOSE DN Key to adjust. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-6 SECTION 2 FLIGHT INSTRUMENTS 2.7 HORIZONTAL SITUATION INDICATOR (HSI) Figure 2-12 Horizontal Situation Indicator 8 14 9 6 5 4 3 2 1 7 13 12 11 10 Heading Bug 2 3 6 4 5 7 1 Turn Rate Indicator Navigation Source Course Deviation Indicator TO/FROM Indicator Course Pointer Rotating Compass Rose 11 10 12 13 14 9 8 OBS Mode Lateral Deviation Scale Flight Phase Aircraft Symbol Lubber Line Heading Turn Rate and Heading Trend Vector Arc HSI The HSI compass can be displayed as a 360° rose or 140° arc (see Figure 2-15) by pressing the PFD Softkey, followed by the 360 HSI or the ARC HSI Softkey. NOTE: When the Arc HSI is displayed, the BRG1 and BRG2 information windows and pointers are disabled. NOTE: If the pilot makes a heading change greater than 105˚ with respect to the course, the CDI switches to the opposite side of the deviation scale and displays reverse sensing. Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid. Figure 2-14 Standard-Rate Turn Indication Turn Rate Trend Vector (standard rate) Figure 2-13 Turn Rate Indicator and Trend Vector Half-Standard Turn Rate Tick Mark Standard Turn Rate Tick Mark Turn Rate Trend Vector (rate > 4 deg/sec) Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-7 SECTION 2 FLIGHT INSTRUMENTS Course Pointer The course pointer is a single line arrow (GPS, VOR1, and LOC1) or double line arrow (VOR2 and LOC2) which points in the direction of the set course. Lateral Deviation Scale Figure 2-15 Arc CDI and Compass Rose CDI Course Deviation TO/FROM Indicator Course Deviation Indicator (CDI) The CDI scale automatically adjusts to the current phase of flight (enroute 5.0 nm, terminal area 1.0 nm, or approach 0.3 nm). Scaling may be selected manually from the MFD System Setup Page. See Sytsem Setup in the G1000 Pilot’s Guide for more detail. Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer. Bearing 2 Pointer Bearing 1 Information Window Bearing 1 Pointer Bearing 2 Information Window Figure 2-16 HSI with Bearing Information DME Information Window Distance to Bearing Source Waypoint Identifier Bearing Source Pointer Icon Figure 2-17 BRG1 Information Window Distance to Bearing Source Waypoint Identifier Pointer Icon Bearing Source Figure 2-18 BRG2 Information Window Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 2-8 SECTION 2 FLIGHT INSTRUMENTS DME (optional) To display the DME Information Window, press the PFD Softkey followed by the DME Softkey. Figure 2-19 DME Information Window Navigation Source To change between navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1/LOC1. 2) Press the CDI Softkey again to change from VOR1/LOC1 to VOR2/LOC2. 3) Press the CDI Softkey a third time to return to GPS. When using GPS as the navigation source, the following may appear: • INTEG – GPS information is either not present or is invalid for navigation use • WARN – GPS detects a position error • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. Figure 2-20 GPS INTEG, GPS SUSP, LOC1 and VOR2 To enable/disable OBS Mode while navigating with GPS: 1) Press the OBS Softkey to select OBS Mode. 2) Turn the CRS Knob to select the desired course TO/FROM the waypoint. 3) Press the OBS Softkey again to return to normal operation. NOTE: The OBS Softkey is only displayed when navigating an active leg using GPS. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-1 SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 ENGINE DISPLAY The Mooney M20R Default Engine Page is shown in Figure 3-1. The M20TN display is similar, but shows Turbine Inlet Temperature (TIT) instead of Exhaust Gas Temperature (EGT). The M20M display is also similar to Figure 3-1, but shows TIT and Fuel Pressure (instead of EGT and Fuel Flow). In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE Softkey makes available the LEAN and SYSTEM softkeys which in turn provide access to the Lean Page and the System Page, respectively. Figure 3-1 M20R Default Engine Page Manifold Pressure Gauge RPM Gauge Ammeter Cylinder Head Temperature Indicator Oil Pressure Indicator Voltmeter Fuel Quantity Indicator Oil Temperature Indicator Fuel Flow Indicator In aircraft with the extended range 55 gallon tanks option, the fuel quantity will still show 45 gallons when full. 3.2 LEAN ENGINE DISPLAY The Mooney M20R Lean Engine Page is shown in Figure 3-2. The M20M/M20TN display is similar, but also shows Turbine Inlet Temperature (TIT). Exhaust Gas Temperature Bar Graph Cylinder Head Temperature Bar Graph EGT Readout For Selected Cylinder CHT Readout For Selected Cylinder Figure 3-2 M20R LEAN Engine Page Fuel Flow Readout Cylinder Select The CYL SLCT Softkey can be utilized to obtain information about a particular cylinder. The CYL SLCT Softkey becomes disabled when a particular cylinder turns yellow or red, until the temperature decreases and returns to normal or when the ASSIST Softkey is pressed. Pressing the ASSIST Softkey causes the first cylinder that peaks to become highlighted and information for that cylinder to be displayed. Any exceedance of default Engine Page parameters, while viewing the Lean Engine Page, will cause the display to automatically switch back to the default Engine Page. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-2 3.3 ENGINE SYSTEM DISPLAY The Mooney M20R System Engine display is shown in Figure 3-3. The M20TN display is similar, but also shows Turbine Inlet Temperature (TIT). The M20M display is also similar to Figure 3-3, but shows Fuel Pressure instead of Exhaust Gas Temperature (EGT), and also shows TIT. If desired, use the DEC FUEL, INC FUEL, and RST FUEL softkeys to adjust the amount of fuel remaining for totalizer calculations. NOTE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calculated from the last time the fuel was reset. Fuel Remaining Flap Position Figure 3-3 M20R SYSTEM Engine Page Aircraft Total Time in Service Elevator Trim Takeoff Position Rudder Trim Takeoff Position Trim Position Indicator Any exceedance of default Engine Page parameters, while viewing the System Engine Page, will cause the display to automatically switch back to the default Engine Page. 3.4 FLAP & TRIM INDICATIONS The flap and trim indicators are located on the MFD next to the engine indicating displays. Rudder Trim Indicator Actual trim position is shown using a blue inverted triangle. The ‘takeoff’ rudder trim position is shown in white. Elevator Trim Indicator Trim position is shown by a blue triangle. A white block indicates ‘takeoff’ elevator trim position. Flaps Position Indicator The Flaps Position Indicator shows the current position of the flaps. The three possible positions, up, take-off, and down, are depicted in cyan as ‘UP’, ‘T/O’, and ‘DN’, respectively. During flaps position transition, ‘///’ is displayed in the window. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-1 SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The Nav/Com controls and frequency windows are located on the Primary Flight Display and the Multi- Function Display in the same locations. NAV Controls COM Controls NAV Frequency Window COM Frequency Window Figure 4-1 G1000 VHF NAV/COM Interface (PFD) Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-2 SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Active NAV Frequency Field Active COM Frequency Field Standby COM Frequency Field Figure 4-2 Frequency Fields Selected NAV Frequency Navigation Status Window Tuning Box Tuning Box Selected COM Frequency Frequency Toggle Arrow Tuning Box Figure 4-3 Frequency Toggle Arrow and Tuning Box Figure 4-4 NAV/COM Controls Frequency Toggle Key Dual NAV Knob Dual COM Knob VOL/PUSH ID Knob VOL/PUSH SQ Knob NAV Controls COM Controls • Turn to tune in desired frequencies. • Press to change tuning box positions. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-3 SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. • TX – When a COM radio is keyed, a white TX indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ID indication appears to the left of the corresponding active NAV frequency. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. Figure 4-5 Radio Status Indications 4.2 VOLUME ‘VOLUME’ is displayed in place of the associated radio name (i.e., ‘COM1’ or ‘NAV2’) for two seconds after the volume level is last changed. The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box. Figure 4-6 COM Volume Level 4.3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COMs standby frequency, then by pressing the VOL/PUSH SQ Knob. 4.4 QUICKLY ACTIVATING 121.500 MHZ Pressing and holding the COM Frequency Toggle Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. 4.5 OPTIONAL NAV RADIOS The Tuning Window is displayed by pressing the ADF/ DME Softkey (if no ADF is installed, the softkey will be labeled DME). Figure 4-7 ADF/DME Tuning Window ADF Radio (optional) To tune the ADF: 1) From the Tuning Window, turn the Large FMS Knob to highlight the ADF tuning field. 2) Turn the Small FMS Knob to enter the first digit. 3) Turn the Large FMS Knob to select the next desired digit field. Turn the Small FMS Knob to again select the desired digit. 4) When the desired frequency is entered press the ENT Key to transfer the frequency into the active field. 5) Turn the Large FMS Knob to select the MODE field. Turn the Small FMS Knob to select ADF or BFO. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-4 SECTION 4 – NAV/COM & TRANSPONDER 6) Turn the Large FMS Knob to select the volume field if desired. Turn the Small FMS Knob to adjust the ADF volume to the desired level. 7) Press the FMS Knob to exit all the fields. DME Radio (optional) Figure 4-8 Radio Tuning Window To change the DME tuning source: 1) From the Tuning Window, turn the Large FMS Knob to highlight the DME source field. 2) Turn the Small FMS Knob to display the selection window. Turn the FMS Knob to select the desired mode and press the ENT Key. Figure 4-9 DME Selection Window 4.6 FREQUENCY AUTO-TUNING Auto-tuning on the PFD Figure 4-10 Nearest Airports Window (PFD) 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Turn the FMS Knob to highlight the desired frequency. 3) Press the ENT Key to place the frequency in the standby field of the active COM. 4) Press the Frequency Toggle Key to place the frequency in the active field. NAV frequencies are entered automatically in the NAV Window upon approach loading or approach activation. Auto-tuning on the MFD Auto-tuning on the MFD is done in much the same way as on the PFD. Use the FMS Knob to select the desired frequency on any of the information pages. Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-5 SECTION 4 – NAV/COM & TRANSPONDER 4.7 TRANSPONDER Mode Selection The STBY, ON, and ALT softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-11 Ground Mode Reply Status When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status field. Figure 4-12 Reply Indication Code Selection 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Press the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. 3) Press the appropriate digit softkeys to enter the code in the four-digit code field of the Transponder Status Bar. Five seconds after the fourth digit has been entered, the transponder code becomes activated. When entering a code, press the BKSP Softkey as needed to back up and change code digits. Following is a list of important codes: • 1200 – VFR code in the U.S. (please refer to the ICAO standards for VFR codes in other countries). • 7000 – VFR code commonly used in Europe (please refer to the ICAO standards). • 7500 – Hijack code. • 7600 – Loss of communication code. • 7700 – Emergency code. • 7777 – Military interceptor operations code (NEVER ENTER THIS CODE). • 0000 – Code for military use (in the U.S.). Flight ID Reporting If so configured, the Flight ID may be entered in the Timer/Reference window. Figure 4-13 Timer/References Window Flight ID Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 4-6 SECTION 4 – NAV/COM & TRANSPONDER Blank Page Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 5-1 SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Split COM Telephone (Unavailable) Marker Beacon/Mute Passenger Address Marker Beacon Signal Sensitivity Speaker VOL/SQ Volume/Squelch Manual Squelch Aircraft Navigation Radio Audio (ADF & DME optional, AUX unavailable) Reversionary Mode Recorded COM Audio Playback Aircraft Navigation Radio Audio Figure 5-1 Audio Panel Controls ICS Isolation VOL Annunciation SQ Annunciation Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 5-2 SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC key, press the already selected COM1 or COM2 Key before pressing the other COM MIC key. Figure 5-2 Transceivers 5.2 SPLIT COM FUNCTION NOTE: Split COM performance is affected by the distance between the antennas and the separation of the tuned frequencies. Figure 5-3 Split COM Function Pressing the COM 1/2 Key selects and deselects the split COM function. During split COM operation, the COM1, COM1 MIC, COM2, and COM2 MIC keys are active. When the COM 1/2 Key is selected, COM1 is used by the pilot for transmission and COM2 is used by the copilot. The COM1 MIC annunciator blinks when the pilot’s microphone is keyed and the COM2 MIC annunciator blinks when the copilot’s microphone is keyed. In this mode, both the pilot and the copilot can transmit simultaneously over separate radios. The pilot can still monitor NAV1, NAV2, and MKR audio as selected, but the copilot is only able to monitor COM2. 5.3 MARKER BEACON RECEIVER The marker beacon receiver is always ON. Only the marker beacon audio can be turned off. Figure 5-4 shows the marker beacon annunciators on the PFD Figure 5-4 Marker Beacon Signal Indicator Lights on the PFD Inner Marker Annunciator Outer Marker Annunciator Middle Marker Annunciator When the MKR/MUTE Key is pressed, the key annunciator is lit and the audio tone can be heard over the speaker or headsets during marker beacon reception. When the tone is active, pressing the MKR/MUTE Key once mutes the audio but does not affect the marker annunciator. The audio returns when the next marker signal is received. To turn off the marker beacon audio, press the MKR/ MUTE Key once when there is no marker indication present, or press twice when an indication is present. The key annunciator will be extinguished when the marker beacon audio is turned off. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 5-3 SECTION 5 – AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-5 Marker Beacon 5.4 NAV RADIO AUDIO SELECTION Pressing DME, ADF, NAV1, or NAV2 selects and deselects the radio source and activates the annunciator. Selected audio can be heard over the headset and the speakers. These four keys can be selected individually or together. Mode PILOT KEY ANNUNCIATOR COPLT KEY ANNUNCIATOR Pilot Hears Copilot Hears Passenger Hears ALL OFF OFF Selected radios; pilot; copilot; passengers; MUSIC 1 Selected radios; pilot; copilot; passengers; MUSIC 1 Selected radios; pilot; copilot; passengers; MUSIC 2 PILOT ON OFF Selected radios; pilot Copilot; passengers; MUSIC 1 Copilot; passengers; MUSIC 2 COPILOT OFF ON Selected radios; pilot; passengers; MUSIC 1 Copilot Selected radios; pilot; passengers; MUSIC 2 CREW ON ON Selected radios; pilot; copilot Selected radios; pilot; copilot Passengers; MUSIC 2 Table 5-1 ICS Isolation Modes Figure 5-6 Navigation Radios 5.5 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1. Figure 5-7 ICS Isolation Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN 5-4 SECTION 5 – AUDIO PANEL 5.6 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively. Figure 5-8 Volume/Squelch Control 5.7 DIGITAL CLEARANCE RECORDER AND PLAYBACK Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next memory block, and so on. Once the 2.5 minutes of recording time has been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. Powering off the unit automatically clears all recorded blocks. Figure 5-9 Playback • Pressing PLAY once plays back the latest recorded memory block, then returns to normal operation. • Pressing PLAY during playback of a memory block halts the playback of this block and plays back the preceding recorded block. The PLAY Key can be used to backtrack through the recorded memory blocks to reach and play back any desired block. • Pressing the MKR/MUTE Key during playback halts playback and returns the recorder/playback to normal operation. If a COM input signal is detected during playback, playback is halted and the new COM input signal is recorded as the latest block. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-1 SECTION 6: AUTOMATIC FLIGHT CONTROL NOTE: The information in this section is not applicable to the M20TN aircraft. Refer to the pilot’s guide for the installed autopilot system. In addition to the AFCS (Automatic Flight Control System) keys on the MFD, as discussed in the System Overview section, the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD. • AP DISC (Autopilot Disconnect) Button — Located on the pilot’s control wheel, pressing this button disengages the autopilot. Pressing it also acknowledges an autopilot disconnect. • CWS (Control Wheel Steering) Button — Located on the pilot’s control wheel, pressing and holding the CWS Button disengages the control surface servos without disengaging the autopilot. If the flight director has not been activated, pressing the CWS Button will activate the flight director in the default pitch and roll hold modes. • GA (Go Around) Button — Located on the instrument panel, the GA Button disengages the autopilot and selects the Go Around Pitch and Roll (wings level) modes. • MET (Manual Electric Trim) Switch — This switch is used to operate manual electric pitch trim. Moving both switches forward simultaneously trims the aircraft nose down. Moving both switches aft simultaneously trims the aircraft nose up. The left switch is the ARM contact and the right switch controls the up/down trim. Pressing the ARM Switch disengages the autopilot, if currently engaged. If one side of the switch is active for more than three seconds without the other side also being active, ‘PTRM’ is displayed in the AFCS System Status field on the PFD. Pressing the MET ARM Switch also acknowledges an autopilot disconnect. Figure 6-1 AFCS Keys Pressing the FD Key activates only the flight director in the default Pitch Hold/Roll modes without engaging the autopilot. Pressing the AP Key activates the flight director, and engages the autopilot. When only the flight director is engaged, pressing the FD Key disengages the flight director. Upon activation of the autopilot and/or flight director, command bars are displayed on the PFD. If the attitude information being sent to the flight director becomes invalid or unavailable, the command bars are removed from the display. Figure 6-2 Command Bars Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-2 6.1 MODE ANNUNCIATIONS Mode annunciations are displayed on the PFD. Figure 6-3 shows the AFCS Status Bar fields. Modes associated with aircraft movement about the roll axis are displayed on the left side. Modes associated with aircraft movement about the pitch axis are displayed on the right. Armed modes are displayed in white and active modes are displayed in green. Figure 6-3 PFD AFCS Display Armed Mode Active Mode Autopilot Status Mode Reference Active Mode Armed Mode System Status Field (see Annunciations & Alerts) Flight Director Command Bars AFCS Status Bar Aircraft Attitude Symbol Selected Altitude Box Roll Axis Modes Pitch Axis Modes 6.2 OVERSPEED PROTECTION An overspeed annunciation (flashing inverse video) is displayed above the airspeed tape. Figure 6-4 Overspeed Annunciation When an overspeed caution occurs, reduce engine power and/or adjust the pitch reference to slow the aircraft. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-3 6.3 AP ENGAGEMENT/DISENGAGEMENT When the key is pressed, the system engages the autopilot. If the flight director is not already active, it is also engaged when the AP Key is pressed. Autopilot engagement is displayed in the Autopilot Status field of the AFCS Status Bar. Autopilot engagement is indicated by a green ‘AP’. Figure 6-5 Autopilot Engaged Annunciation Autopilot Engaged Automatic Disengagement Automatic disengagement typically occurs due to a failure. Automatic disengagement is annunciated by a flashing ‘AP’, alternating red on white and white on red in the Autopilot Status field. Also, the autopilot disconnect aural alert will be heard. Both the annunciation and the aural alert will continue until acknowledged by pressing the AP DISC Button or the MET ARM Switch. Figure 6-6 Automatic Disconnect Annunciation Automatic Disconnect Manual Disengagement The autopilot may also be manually disengaged by pressing the AP DISC Button, the GA Button, the MET ARM Switch, or by pressing the AP Key on the MFD. Manual disengagement is annunciated by a five-second flashing yellow ‘AP’ in the Autopilot Status field and by a two-second autopilot disconnect aural alert. Figure 6-7 Manual Disconnect Annunciation Manual Disconnect Control Wheel Steering Pressing and holding the CWS Button disengages the servos from the flight control surfaces and allows manual manuevering of the aircraft. At the same time, the flight director is synchronized to the aircraft attitude during the maneuver. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white until the CWS Button is released. Figure 6-8 CWS Annunciation Control Wheel Steering Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-4 6.4 LOSS OF DATA In general, a flashing yellow mode annunciation indicates either the loss of sensor data (AHRS, ADC, or GIA) or loss of navigation data (VOR, LOC, or GPS) required to compute commands. When such a loss occurs, the system automatically reverts to the default mode for the affected axis (ROL for roll axis, PIT for pitch axis). The flashing annunciation stops when the pilot presses the affected mode button or selects another mode for the axis. If no pilot action is taken, the flashing annunciation stops after ten seconds. Figure 6-9 Loss of VOR Signal 6.5 PITCH AXIS MODES Mode annunciations for active pitch axis modes are shown in green during normal operation. Note the Go- Around Button is not located on the MFD. AFCS Key AFCS Mode Annunciation FD/AP only Pitch Hold (Default) PIT ALT Altitude Hold ALT nnnnn FT VS Vertical Speed VS nnnn FPM FLC Flight Level Change FLC nnn KT APR Glideslope (vertical com- ponent of Approach) GS GA Go Around GA The default pitch axis mode is Pitch Hold (PIT). When no other pitch axis modes are selected, this is the active pitch axis mode when the autopilot and/or flight director is engaged. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-5 Pitch Hold Mode (PIT) 1) Press the AP or FD Key. ‘PIT’ will be displayed in green in the Active Mode field of the AFCS Status Bar. The system will maintain or give command bar direction for a constant pitch attitude (pitch reference) depending on which key is pressed. Flight Director command bars maintain desired pitch reference Pitch Hold Mode is active Altitude Hold Mode is armed Figure 6-10 Pitch Hold Mode 2) Altitude Hold Mode is automatically armed with ‘ALT’ displayed white in the Armed Mode field to the right of the ‘PIT’ annunciation. 3) Pitch attitude can be adjusted in 0.5 degree increments by pressing the NOSE UP/NOSE DN keys. 4) Aircraft pitch may also be changed by pressing and holding the CWS Button to manually establish the desired pitch using the control wheel. When the CWS Button is released, the current pitch angle will be maintained. 5) If desired, enter an altitude in the Selected Altitude Box by turning the ALT Knob. As the selected altitude is reached ‘ALT’ will flash in green for 10 seconds in the Acitve Mode field, after which the annunciation stops flashing. This signals the altitude capture is complete and the selected altitude will be maintained. If only the flight director is engaged, pitch and roll commands are given to manually maintain the selected altitude. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-6 Altitude Hold Mode (ALT) 1) Press the ALT Key. The flight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode field with the current altitude displayed in the Altitude Reference field. 2) Pitch and roll commands will be given to manually maintain the current altitude. Press the AP Key to engage the autopilot for maintaining the current altitude. Figure 6-11 Altitude Hold Mode Altitude Hold Mode is active Flight Director command bars hold pitch attitude to maintain the altitude reference Altitude Reference 3) To change aircraft altitude, press and hold the CWS Button and manually maneuver to the desired altitude. Upon reaching the desired altitude, release the CWS Button. This new altitude is now displayed in the Altitude Reference field. The autopilot will now hold the aircraft at this altitude. NOTE: If the Selected Altitude is captured during CWS maneuvering, the Flight Director altitude reference is not changed. To adjust the altitude reference in this case, the pilot must again press the CWS Button after the Selected Altitude is captured. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-7 Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed. Altitude Hold Mode is automatically armed with ‘ALT’ displayed white in the Armed Mode field to the right of the ‘VS’ annunciation. 2) The Vertical Speed Bug can be adjusted in 100 fpm increments by pressing the NOSE UP/NOSE DN keys to set the desired vertical speed. The vertical speed setting will be displayed in the Selected Vertical Speed box and in the Vertical Speed Reference field in the AFCS Status Bar. Figure 6-12 Vertical Speed Hold Mode Vertical Speed Reference Bug Selected Vertical Speed Selected Altitude Altitude Hold is Armed Flight Director command bars indicating a climb at the prescribed vertical speed, to the Selected Altitude Vertical Speed Reference Vertical Speed Mode is active The Vertical Speed box is located above the VSI when the aircraft is climbing and below the VSI when descending. 3) Vertical speed may also be changed by pressing and holding the CWS Button to manually establish the desired vertical speed using the control wheel. When the CWS Button is released, the current vertical speed will be maintained. 4) A desired altitude may be entered in the Selected Altitude Box by turning the ALT Knob. With Altitude Hold Mode armed, as the selected altitude is reached ‘ALT’ will flash in green for 10 seconds in the Active Mode field, after which the annunciation stops flashing. This signals the altitude capture is complete and the selected altitude will be maintained. If only the flight director is engaged, pitch and roll commands are given to manually maintain the selected altitude. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-8 Flight Level Change Mode (FLC) 1) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select box. This altitude must be selected first because Flight Level Change Mode will only fly toward a selected altitude. 2) Press the FLC Key. The flight director is activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode field and the Airspeed Bug will appear on the Airspeed Indicator. Pitch commands are given to manually maintain airspeed. Press the AP Key to engage the autopilot for maintaining the current airspeed. Altitude Hold Mode is automatically armed with ‘ALT’ displayed white in the Armed Mode field to the right of the ‘FLC’ annunciation. 3) The Airspeed Bug can be adjusted in 1 knot increments by pressing the NOSE UP/NOSE DN keys to set the desired airspeed. The airspeed setting will be displayed in the Selected Figure 6-13 Flight Level Change Mode Altitude Hold Mode is armed Airspeed Reference Selected Airspeed Airspeed Reference Bug Flight Level Change Mode is active Selected Altitude Airspeed box above the Airspeed Indicator and in the Airspeed Reference field in the AFCS Status Bar. 4) Airspeed may also be changed by pressing and holding the CWS Button to manually establish the desired airspeed using the control wheel. When the CWS Button is released, the current airspeed will be maintained. 5) Adjust engine power to allow the autopilot to fly the aircraft at a pitch attitude which corresponds to the selected airspeed and the desired flight profile (descent or climb). 6) With Altitude Hold Mode armed, as the selected altitude is reached, ‘ALT’ will flash in green for 10 seconds in the Acitve Mode field, after which the annunciation stops flashing. This signals the altitude capture is complete and the selected altitude will be maintained at the selected airspeed. If only the flight director is engaged, pitch commands are given to manually maintain the selected altitude. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-9 Go-Around Mode (GA) Pressing the GA Button (not located on the MFD) engages the flight director in a wings level, 7 degree pitch up attitude. Go-Around Mode disengages the autopilot, and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is also allowed. If the pitch attitude is changed manually (e.g with the CWS Button or the NOSE UP/NOSE DN keys), Pitch and Roll Hold modes will automatically be selected. Flight Director command bars indicating climb Go Around Mode is active in both pitch axis & roll axis modes Autopilot disconnect annunciation flashes yellow for 5 seconds Figure 6-14 Go-Around Mode Glideslope (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 Mode is only available when the flight director has been set for approach. Glideslope Mode is automatically armed under the following conditions: • Valid localizer frequency is tuned • Horizontal Situation Indicator (HSI) is in LOC mode, with valid deviation indication • Valid glideslope deviation • APR Key is pressed Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-10 6.6 ROLL AXIS MODES Mode annunciations for active roll axis modes are shown in green during normal operation. AFCS Key AFCS Mode Annunciation FD/AP only Roll Hold (Default) ROL HDG Heading Select HDG NAV VOR Enroute Arm / Capture / Track VOR GPS Arm / Capture / Track GPS BC Arm / Capture / Track BC LOC Arm / Capture / Track; (No Glideslope) LOC APR GPS Arm / Capture / Track GPS VOR Approach Arm / Capture / Track VAPP ILS Approach Arm / Capture / Track (Glideslope Pitch Mode automatically armed) LOC GA Go Around (Wings Level) GA The default roll axis mode is Roll Hold (ROL). When no other roll axis modes are selected, this is the active roll axis mode when the autopilot and/or flight director is engaged. Roll Hold Mode (ROL) 1) Press the FD or AP Key. If the aircraft bank angle is ≥ 6 degrees when the key is pressed, Roll Hold Mode is selected by default. Roll attitude at the time of activation is maintained by the autopilot up to 25˚. If only the flight director is active, command bars indicate the proper roll attitude. If the aircraft bank angle is < 6 degrees when the key is pressed, the aircraft will be maintained at wings level. If only the flight director is active, command bars give guidance to maintain wings level. Roll Hold Mode is annunciated by ‘ROL’. Figure 6-15 Roll Hold Mode 2) A new heading can be established by pressing and holding the CWS Button and manually turning the aircraft to the desired new heading. Release the CWS Button and the aircraft will maintain wings level at approximately the new heading, but will not hold the heading. The same practice applies to holding roll attitude. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-11 Heading Select Mode (HDG) 1) Turn the HDG Knob to move the Heading Bug on the HSI to the desired heading. When the knob is turned, the Selected Heading box will appear and remain for three seconds after the knob stops moving. The selected heading will be displayed in the Selected Heading box. 2) With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode field. If the autopilot is engaged, the aircraft will begin to turn toward the selected heading. When the selected heading is reached, the aircraft will maintain this heading. If only the flight director is engaged, manually maneuver the aircraft to the command bars to aquire the selected heading. Altitude Hold Mode is active Flight Director command bars tracking Selected Heading Heading Select Mode Selected Heading Box Selected Heading Bug Figure 6-16 Heading Select Mode 3) The heading may be adjusted by turning the HDG Knob and moving the Heading Bug to a new heading. The aircraft will turn in the same direction the Heading Bug is moved. However, if the Heading Bug is moved more than 340 degrees at a time, a turn reversal will be the result. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-12 Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. The Navigation Mode acquires and tracks the selected navigation receiver on the HSI (e.g. GPS, VOR or LOC). GPS roll steering commands are followed when the HSI is in GPS Mode, and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR, LOC, or BC (backcourse) modes. Turning the CRS Knob moves the Course Pointer and displays the Selected Course box. The Selected Course is displayed in the box. The box is displayed while the knob is turning and disappears three seconds after the knob stops turning. Backcourse Mode is automatically selected when the localizer front course is greater than 105 degrees from the aircraft heading. NOTE: When making a backcourse approach, set Selected Course to the localizer front course. Figure 6-17 Navigation Mode Flight Level Change Mode is active Flight Director command bars indicating a left turn to track GPS course and a climb to intercept Selected Altitude Navigation Mode is active using GPS source GPS is active navigation receiver on the HSI. Selected Course Altitude Hold is armed Navigation Mode Armed If the CDI is not centered (deviation >1 dot) when the Navigation Mode is selected, the mode is automatically armed. The armed annunciation appears in white to the left of the active roll axis mode. See the Example Procedures Using AFCS section for more information. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-13 Approach Mode (GPS, VAPP or LOC) The Approach Mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC). This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. The Approach Mode provides greater sensitivity for VOR tracking than Navigation Mode, and allows the autopilot to fly an ILS approach with a glideslope. NOTE: The Glideslope Mode is automatically armed when LOC Mode is selected on the HSI. Glideslope is active Flight Director command bars indicating descent on localizer/ glideslope path Approach Mode is active LOC2 is the active navigation receiver on the HSI Figure 6-18 Approach Mode If the CDI is not centered (deviation >1 dot) when the Approach Mode is selected, the mode is automatically armed. The armed annunciation appears in white to the left of the active roll axis mode. See the Example Procedures Using AFCS section for more information. Go Around (GA) Go Around Mode maintains a wings level, 7 degree nose up attitude for instances where the pilot wishes to execute a missed approach or go around. Figure 6-14 depicts the Go Around Mode on the PFD. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-14 6.7 EXAMPLE PROCEDURES USING AFCS This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT). Climb to an altitude of 7,000 feet MSL and fly a heading of 070 degrees to intercept airway V107. Fly airway V107 to Panoche VORTAC (PXN) using VOR navigation, then fly airway V230 using a GPS flight plan. Prior to reaching Clovis VORTAC (CZQ), descend to 3,000 feet and load the ILS approach to R29R at KFAT. Fly the ILS approach and execute a missed approach. 0 3 6 9 12 15 18 21 24 27 30 33 0 3 6 9 12 15 18 21 24 27 30 33 070 Panoche� VORTAC (PXN) KFAT KRHV V 230 Clovis� VORTAC (CZQ) V 107 Figure 6-19 Flight Plan Overview NOTE: The diagrams in the following examples are for instructional purposes only and may not be current. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-15 Departure To Climb to Selected Altitude and Fly an Assigned Heading: 1) Upon takeoff, set the Selected Altitude to 7,000 feet, using the ALT Knob. To have the autopilot capture this altitude, select Pitch Hold, Vertical Speed, or Flight Level Change Mode. In this example, Vertical Speed Mode is used. 2) Upon reaching the desired vertical speed of 1000 fpm, press the VS Key. Altitude Hold Mode is armed automatically. 3) After reaching the minimum engage altitude and activating Vertical Speed Mode, press the AP Key, engaging the autopilot in default Roll Hold and Vertical Speed modes. Figure 6-20 Departure 1. 2. 3. 4. HDG Mode 070 VS Mode, ALT Mode Armed ALT Mode Selected Altitude of 7,000 MSL 5. 4) With the autopilot engaged in a climb, set Selected Heading to 070 degrees using the HDG Knob, then press the HDG Key. The autopilot turns the aircraft to the desired heading. 5) As the aircraft climbs to the selected altitude, the autopilot changes from Vertical Speed Mode to Altitude Hold Mode. This is annunciated by the green ‘ALT’ flashing for ten seconds. 6) Upon reaching the selected altitude, the autopilot completes the capture process and levels the aircraft. From this point, the autopilot continues to operate in Altitude Hold Mode. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-16 Intercepting a VOR Radial After climbout, the autopilot continues to fly the aircraft on a heading of 070 degrees at an altitude of 7,000 feet. Next, intercept airway V107 to Panoche VORTAC (PXN). 1) Tune the VOR frequency, then set the CDI to VOR by pressing the CDI Softkey. Set the Selected Course to 116 degrees using the CRS Knob. Note the autopilot is still in Heading Mode and continues to fly a heading of 070 degrees. 2) Press the NAV Key. This arms the Navigation Mode and the white annunciation ‘VOR’ appears to the left of the active Heading Mode. Figure 6-21 Intercepting a VOR 1. 2. 3. 296 0 3 6 9 12 15 18 21 24 27 30 33 HDG Mode, VOR Armed 070 VOR Mode V 107 Panoche� VORTAC� (PXN) 3) The system calculates the point at which the autopilot changes from Heading Mode to Navigation Mode. When the aircraft reaches this point, ‘VOR’ flashes green in the active mode field. The autopilot begins turning to intercept the selected course. 4) The autopilot continues the turn until the aircraft is established on the selected course. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-17 Flying a Flight Plan / GPS Course 1) The aircraft is currently tracking inbound on the 116 degree radial of Panoche VORTAC. Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2) With the flight plan activated, press the CDI Softkey to set the CDI to GPS. This cancels VOR Mode, and the autopilot loses the VOR signal. As a result, the VOR annunciation flashes yellow and the autopilot reverts to default Roll Hold (ROL) Mode. Flashes for ten seconds, then transitions to ROL.. 0 3 6 9 12 15 18 21 24 27 30 33 1. 2. 3. VOR Mode GPS Flight Plan Leg GPS Mode 0 3 6 9 12 15 18 21 24 27 30 33 V 230 Clovis� VORTAC (CZQ) Panoche� VORTAC (PXN) Figure 6-22 Transition to GPS Flight Plan 3) Now, press the NAV Key to reactivate the autopilot using GPS guidance. At this moment, the autopilot couples to GPS guidance and steers the aircraft toward the active flight plan leg. Once the flight plan leg is intercepted, the autopilot continues to track GPS guidance to the end of the flight plan. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-18 Flight Level Change (Descent) 1) In preparation for the approach to KFAT, set Selected Altitude to 3,000 feet using the ALT Knob. Press the FLC Key. ‘FLC’ is annunciated with the airspeed reference, which defaults to the current aircraft airspeed. Altitude Hold Mode is armed automatically. The current cruise speed of 142 knots will be used for the descent. 2) To allow the aircraft to descend, power must be reduced. The Autopilot maintains 142 knots by controlling pitch. 1. 2. 3. Cruise Altitude of 7,000 MSL Selected Altitude of 3,000 MSL ALT Hold Mode FLC Mode Figure 6-23 FLC Descent 3) As the aircraft reaches the selected altitude, the autopilot changes from Flight Level Change Mode to Altitude Hold Mode. ‘ALT’ flashes in green, indicating the selected altitude is captured. After the capture is finished, the autopilot holds the aircraft at the selected altitude. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-19 ILS Approach 1) Load the Runway 29R ILS approach for KFAT into the flight plan. ‘Vectors to Final’ is selected for the transition. Upon being given vectors from ATC, set the Selected Heading to the heading given by ATC. and press the HDG Key. The autopilot turns the aircraft to the desired heading. 2) Turn the HDG Knob to set the Heading Bug to comply with ATC vectors, as requested. Figure 6-24 ILS Approach to KFAT 00 33 66 99 1212 2 1515 5 1818 8 212121 224 27272 303030 333333 1. 2. 3. HDG Mode GPS Course 4244 122 4. 5. LOC/GS Mode HILAN KFAT Clovis (CZQ) 110 290 075 025 3) In preparation for the approach and at the pilot’s discretion, tune the localizer frequency, then set the CDI to LOC by pressing the CDI Softkey. 4) When cleared for the approach, press the APR Key. ‘LOC’ and ‘GS’ appear in white in the roll axis and pitch axis modes armed fields, respectively. The autopilot will calculate when to begin the turn to intercept the final approach course. 5) From this point, the autopilot flies the ILS. At the Decision Height, press the AP DISC Button and land the aircraft, or press the GA Button to execute a missed approach. Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-20 Go-Around / Missed Approach 1) When the decision is made to execute a missed approach, apply full power and press the GA Button. The autopilot will disconnect and the flight director command bars will establish a 7 degree nose-up climb. Note when the autopilot disconnects the ‘AP’ annunciation flashes yellow for five seconds. Manually fly the aircraft to the command bars. 2) Following the published Missed Approach Procedure, climb to the prescribed altitude. Press the AP Key, re-engaging the autopilot. To have the autopilot fly to the hold point, set the CDI to GPS by pressing the CDI Softkey. Press the SUSP Softkey to resume the sequencing of the approach legs to the Missed Approach Hold Point (MAHP). Press the NAV Key. The autopilot flies direct to Clovis VORTAC according to the loaded approach. 3) During the climb, set a desired hold altitude in the Selected Altitude Box by turning the ALT Knob. The CWS Button may be used to manually set a new pitch attitude. Doing this causes the autopilot to revert to the default Pitch Hold (PIT) Mode and Altitude Hold is armed. When the selected altitude is reached, Altitude Hold Mode will