Garmin MOONEY M20TN - Manual

Garmin MOONEY M20TN

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Table of Contents:

  • Page 4 – Use of the Stormscope
  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – Blank Page
  • Page 9 – TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
  • Page 10 – ii; SECTION 7: NAVIGATION
  • Page 11 – iii; SECTION 9: PROCEDURES
  • Page 12 – iv; Index
  • Page 13 – The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
  • Page 14 – MFD Only
  • Page 16 – FD; Softkey OFF; INSET
  • Page 17 – PFD; Figure 1-3 PFD Softkey Flow Chart – 1; Figure 1-4 PFD Softkey Flow Chart – 2
  • Page 18 – METRIC; Figure 1-5 PFD Softkey Flow Chart – 3; OBS
  • Page 19 – Figure 1-6 MFD Softkeys
  • Page 20 – Figure 1-7 Page Group Icon
  • Page 21 – SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 22 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 23 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer at Vne; Speed Ranges; ON; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
  • Page 24 – Figure 2-7 Altimeter; Altitude Select Bug; To set the Selected Altitude Bug:; Turn the; Knob to set the Altitude Select; ALT; Knob sets the hundreds and; ALT; Knob sets the thousands. This; Altitude Trend Vector; BARO; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Barometric Minimum Descent Altitude
  • Page 25 – Figure 2-9 Barometric Minimum Descent Altitude; INDICATOR; Figure 2-10 Marker Beacon and Vertical Deviation; VERTICAL SPEED INDICATOR; Figure 2-11 Vertical Speed Indicator; VS
  • Page 26 – HORIZONTAL SITUATION INDICATOR; Figure 2-12 Horizontal Situation Indicator; Arc HSI; When the Arc HSI is displayed, the BRG1; Turn Rate Indicator and Heading Trend Vector; Figure 2-14 Standard-Rate Turn Indication
  • Page 27 – Figure 2-15 Arc CDI and Compass Rose CDI; Bearing Pointers and Information Windows; Figure 2-16 HSI with Bearing Information
  • Page 28 – Figure 2-19 DME Information Window; Navigation Source; The; Softkey is only displayed when
  • Page 29 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; Figure 3-1 M20R Default Engine Page; LEAN ENGINE DISPLAY; Figure 3-2 M20R LEAN Engine Page; Cylinder Select
  • Page 30 – ENGINE SYSTEM DISPLAY; RST; Fuel calculations do not use the aircraft; Rudder Trim Indicator
  • Page 31 – TRANSPONDER; The Nav/Com controls and frequency windows are
  • Page 32 – Figure 4-2 Frequency Fields
  • Page 33 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME
  • Page 34 – Figure 4-8 Radio Tuning Window; Auto-tuning on the PFD; FMS
  • Page 35 – STBY; Figure 4-11 Ground Mode; Reply Status; Figure 4-12 Reply Indication; Code Selection; Flight ID Reporting
  • Page 37 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 38 – COM RADIO SELECTION; Figure 5-2 Transceivers; SPLIT COM FUNCTION; Split COM performance is affected by; MARKER BEACON RECEIVER; Figure 5-4 Marker Beacon Signal Indicator Lights on the PFD
  • Page 39 – HI SENS; Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Table 5-1 ICS Isolation Modes; PILOT; Figure 5-7 ICS Isolation
  • Page 40 – INTERCOM SQUELCH CONTROL
  • Page 41 – SECTION 6: AUTOMATIC FLIGHT; The information in this section is not
  • Page 42 – MODE ANNUNCIATIONS; Mode annunciations are displayed on the PFD. Figure; Figure 6-3 PFD AFCS Display; OVERSPEED PROTECTION; An overspeed annunciation (flashing inverse video) is; Figure 6-4 Overspeed Annunciation; When an overspeed caution occurs, reduce engine
  • Page 43 – Figure 6-5 Autopilot Engaged Annunciation; Autopilot Engaged; Automatic Disengagement; Figure 6-6 Automatic Disconnect Annunciation; Automatic Disconnect; Manual Disengagement; Figure 6-7 Manual Disconnect Annunciation; Manual Disconnect; Figure 6-8 CWS Annunciation; Control Wheel Steering
  • Page 44 – In general, a flashing yellow mode annunciation; Figure 6-9 Loss of VOR Signal; PITCH AXIS MODES; Mode annunciations for active pitch axis modes are
  • Page 45 – AP; Figure 6-10 Pitch Hold Mode; CWS
  • Page 46 – Figure 6-11 Altitude Hold Mode; If the Selected Altitude is captured during; Button after the Selected Altitude is
  • Page 47 – Figure 6-12 Vertical Speed Hold Mode
  • Page 48 – toward; FLC; Figure 6-13 Flight Level Change Mode
  • Page 49 – GA; Pressing the CWS button while Glideslope; APR
  • Page 50 – Mode annunciations for active roll axis modes are; Figure 6-15 Roll Hold Mode
  • Page 51 – Figure 6-16 Heading Select Mode; HDG
  • Page 52 – NAV; When making a backcourse approach, set; Navigation Mode Armed
  • Page 53 – The Approach Mode acquires and tracks the selected; The Glideslope Mode is automatically; See the Example Procedures Using AFCS section for
  • Page 54 – EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of procedures; Figure 6-19 Flight Plan Overview
  • Page 55 – Figure 6-20 Departure
  • Page 56 – After climbout, the autopilot continues to fly the aircraft; CDI; Figure 6-21 Intercepting a VOR
  • Page 57 – ) The aircraft is currently tracking inbound on the; Figure 6-22 Transition to GPS Flight Plan; Key to reactivate the
  • Page 58 – ) In preparation for the approach to KFAT, set; Key. ‘FLC’ is annunciated; Figure 6-23 FLC Descent; ) As the aircraft reaches the selected altitude,
  • Page 59 – Figure 6-24 ILS Approach to KFAT
  • Page 61 – SECTION 7 – NAVIGATION; The following discussions pertain to the Multi Function; NAVIGATION MAP PAGE; Select the MAP Page Group; The map display should only be; Direct-to Navigation from the MFD
  • Page 62 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 63 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page
  • Page 64 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page
  • Page 65 – Figure 7-8 VOR Information Page; Select the VOR Information Page; USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-9 Nearest Airports Page; Nearest Airport Information on the MFD
  • Page 66 – Figure 7-10 Nearest Airports Window
  • Page 67 – NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page; Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page
  • Page 68 – Figure 7-13 Nearest VOR Page
  • Page 69 – NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page
  • Page 70 – NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 71 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 72 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Window on the PFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page
  • Page 73 – ACTIVATE A FLIGHT PLAN LEG; Figure 8-5 Activate Flight Plan Leg Confirmation; STOP NAVIGATING A FLIGHT PLAN; Figure 8-6 Delete Flight Plan; INVERT ACTIVE FLIGHT PLAN; Figure 8-8 Invert Flight Plan
  • Page 74 – CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD; Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the; LOAD A DEPARTURE; See the Procedures section for a discussion on loading
  • Page 75 – Figure 8-13 Store Flight Plan Confirmation
  • Page 76 – INVERT AND ACTIVATE A STORED
  • Page 77 – Figure 8-15 Trip Planning Page; Starting WPT; The Page mode must be set to MANUAL
  • Page 78 – : An active flight plan or Direct-to must be; NOTE; : VNAV is advisory only and cannot be; Create a Vertical Navigation Profile
  • Page 79 – 0) With the ‘TARGET ALTITUDE’ field highlighted,; Knob to select the target altitude.; ENT; Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU
  • Page 81 – SECTION 9 – PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Load and Activate An Arrival Procedure; Figure 9-3 Select Arrival
  • Page 82 – Figure 9-4 Select Arrival Transition; Not all approaches in the database are approved for GPS; Load and/or Activate an Approach Procedure
  • Page 83 – Figure 9-6 Selecting an Approach Procedure; Activate An Approach in the Active Flight Plan
  • Page 85 – SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 86 – At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page
  • Page 87 – XM Weather is not intended to
  • Page 88 – Figure 10-9 Weather Data Link Page
  • Page 90 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group will; Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 91 – If the G1000 is configured to use the; Displaying Traffic on the Traffic Map Page; If data is not received for a period longer than 6 seconds,; Figure 10-11 Traffic Map Page; Displaying Traffic on the Navigation Map; alert “Traffic” is given.
  • Page 92 – SKYWATCH TRAFFIC ADVISORY; Refer to the SkyWatch pilot’s guide for a detailed; Figure 10-12 Traffic Map Page
  • Page 93 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 94 – Figure 10-15 Obstacle Symbols
  • Page 95 – Displaying Terrain on the TAWS Page
  • Page 96 – Red; Enable/Disable Aviation Data; Figure 10-19 TAWS Page Menu; TAWS Inhibit; Flying VFR into an area where unique terrain exists
  • Page 97 – A system test is automatically performed at power-up.; ) While the TAWS Page is displayed, press the; Enroute
  • Page 98 – Figure 10-20 PDA Alerting Threshold; Figure 10-21 Excessive Descent Rate; Don’t Sink
  • Page 99 – Potential Impact Points; Figure 10-22 TAWS Symbols; “Five-Hundred” Aural Alert; ) With the Navigation Map displayed, press the; Softkey. Terrain and obstacle
  • Page 100 – Alert Type
  • Page 101 – The following system status annunciations may also be issued.; Alert Annunciations; Figure 10-24 Alert Annunciation on the TAWS Page; Alert Annuciation; Figure 10-25 Alert Annunciation on the PFD
  • Page 103 – SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary Mode can also be manually activated by; Th e M o o n e y M 2 0 M / M 2 0 R / M 2 0 T N
  • Page 104 – When a COM tuning failure is detected by the system,; Figure 11-2 Extreme Pitch Indication; If heading is lost, strikes and/or cells must be cleared; Figure 11-3 Loss of Hazard Functions
  • Page 105 – SECTION 12 – ANNUNCIATIONS; ALERTS
  • Page 106 – ALERT LEVEL DEFINITIONS; The G1000 Alerting System, as installed in Mooney; Figure 12-2 ADVISORY Softkey; The following alerts are configured specifically for; Voice Alerts; Voice Alert; Message Advisory Alerts; Alerts Window Message; PFD FAN FAIL
  • Page 107 – The following alert annunciations appear in the AFCS; Condition; Figure 12-3 AFCS System Status Field; System Status Field
  • Page 109 – When an LRU or an LRU function fails, a large red
  • Page 110 – System Annunciation
  • Page 111 – Audio Alerts; Audio Alert
  • Page 112 – A red ‘X’ may be the result of an LRU or an LRU; Figure 12-4 G1000 System Failure Annunciations; ADVISORIES; This section describes various G1000 system message; This section provides information
  • Page 113 – Message
  • Page 115 – GIA 63 Message Advisories
  • Page 117 – GEA 71 Message Advisories
  • Page 118 – GRS 77 Message Advisories
  • Page 119 – HDG FAULT; GDL 69 Message Advisories; GDC1 CONFIG
  • Page 121 – BACKUP PATH
  • Page 123 – INDEX; Signal augmentation 5-3
  • Page 125 – System message advisories 12-8
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Integrated Flight Deck

Cockpit Reference Guide

Mooney M20M,

M20R, & M20TN

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Summary

Page 4 - Use of the Stormscope

Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN WARNINGS, CAUTIONS, & NOTES . WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference ...

Page 7 - RECORD OF REVISIONS; Part Number

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 manualAdded WX 500 StormscopeAdded XM WeatherAdded ADF/DMEAdded extended range fuel tanksChanges in EIS softkey labels 190-00450-02 Added TAWS-BAdd...

Page 8 - Blank Page

Garmin G1000 Cockpit Reference Guide for the Mooney M20M, M20R, & M20TN RR-2 RECORD OF REVISIONS Blank Page

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