Garmin Columbia 350/400- User Manual

Garmin Columbia 350/400

Garmin Columbia 350/400– User Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

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Table of Contents:

  • 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; Heading Input; INDEX
  • Page 13 – The purpose of this Cockpit Reference Guide is
  • Page 14 – MFD Only
  • Page 18 – Softkey OFF; INSET; Figure 1-4 PFD Softkey Flow Chart – 1
  • Page 19 – PFD; Figure 1-5 PFD Softkey Flow Chart – 2; METRIC
  • Page 20 – Figure 1-6 PFD Softkey Flow Chart – 3
  • Page 21 – Figure 1-7 MFD Softkeys
  • Page 22 – Figure 1-8 Page Group Icon
  • Page 23 – DATABASE UPDATES; Aviation Database Update; Figure 1-10 Database Update Prompt; ENT; Figure 1-11 Database Update Confirmation; Terrain and Obstacle Database Updates; These databases are not stored internally in the MFD; TOPO
  • Page 24 – Figure 1-12 Power-Up Splash Screen Window
  • Page 25 – SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 26 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 27 – 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 28 – Figure 2-7 Altimeter; Altitude Select Bug; Set the Selected Altitude Bug:; Turn the; Knobs 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 29 – 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 30 – HORIZONTAL SITUATION INDICATOR; Arc HSI; • Localizer – Diamond; Lateral; Turn Rate Indicator and Heading Trend Vector
  • Page 31 – Figure 2-15 Standard-Rate Turn Indication; Course Pointer; Figure 2-16 Course Pointer; Bearing Pointers and Information Windows; Figure 2-17 HSI with Bearing Information
  • Page 32 – Figure 2-19 BRG2 Information Window; Navigation Source; When using GPS as the navigation source, the following; The; OBS; Softkey is only displayed when
  • Page 33 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; The Engine Instrument Display is displayed on the left; Figure 3-1 Engine Instrument Display
  • Page 34 – SYSTEM; Trim
  • Page 35 – ENGINE LEANING ASSIST DISPLAY; Engine Leaning for the Columbia 350; The Columbia 350 Airplane Flight Manual; Leaning for Best Power; Indicates First; ) Lean the mixture until one of the cylinder’s
  • Page 36 – Leaning for Best Economy; Indicates Last; Peak temperature and continue
  • Page 37 – The Columbia 400 Airplane Flight Manual; Selecting the
  • Page 38 – FUEL CALCULATIONS; Figure 3-6 EIS Display - Fuel Calculations Group; gallons of usable fuel.; DEC FUEL
  • Page 39 – TRANSPONDER; The NAV/COM controls and frequency boxes are
  • Page 40 – Figure 4-2 Frequency Fields
  • Page 41 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; Auto-tuning on the PFD; NRST; Auto-tuning on the MFD; FMS
  • Page 42 – STBY; Figure 4-8 Ground Mode; Reply Status; Figure 4-9 Reply Indication; Code Selection
  • Page 43 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 44 – COM RADIO SELECTION; Figure 5-2 Transceivers; SPLIT COM FUNCTION; Split COM performance is affected by the; MARKER BEACON RECEIVER; Figure 5-4 Marker Beacon Annunciators on the PFD
  • Page 45 – HI SENS; Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Table 5-1 ICS Isolation Modes; PILOT; Figure 5-7 ICS Isolation
  • Page 46 – INTERCOM SQUELCH CONTROL
  • Page 47 – SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; MODE ANNUNCIATIONS
  • Page 48 – Figure 6-3 PFD AFCS Display; OVERSPEED PROTECTION; Figure 6-4 Overspeed Annunciation; AP; Figure 6-5 Autopilot Engaged Annunciation
  • Page 49 – 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; Figure 6-9 Loss of VOR Signal; PITCH AXIS MODES; AFCS Key
  • Page 50 – Figure 6-10 Pitch Hold Mode; CWS
  • Page 51 – Figure 6-11 Altitude Hold Mode
  • Page 52 – Figure 6-12 Vertical Speed Hold Mode
  • Page 53 – toward; FLC; Figure 6-13 Flight Level Change Mode
  • Page 54 – GO AROUND; Pressing the CWS button while Glideslope; APR
  • Page 55 – Mode annunciations for active roll axis modes are; Figure 6-15 Roll Hold Mode
  • Page 56 – Figure 6-16 Heading Select Mode; HDG
  • Page 57 – NAV; Figure 6-17 Navigation Mode; Navigation Mode Armed
  • Page 58 – The Approach mode acquires and tracks the selected; While using Approach mode, the; See the Example Procedures Using AFCS section for
  • Page 59 – EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of procedures; Figure 6-19 Flight Plan Overview
  • Page 60 – Figure 6-20 Departure
  • Page 61 – Changing the HSI mode cancels Navigation; During climb-out, the autopilot continues to fly the; CDI; Figure 6-21 Intercepting a VOR
  • Page 62 – Figure 6-22 Transition to GPS Flight Plan
  • Page 63 – While flying the GPS leg from Panoche VORTAC to; Knob, set the Selected Altitude; Key to activate Flight Level; Figure 6-23 FLC Descent; ) Reduce power to allow descent in Flight Level
  • Page 64 – Figure 6-24 ILS Approach to KFAT
  • Page 65 – As a result of the calculations being
  • Page 67 – 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 68 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 69 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page
  • Page 70 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page
  • Page 71 – Figure 7-8 VOR Information Page; Select the VOR Information Page; The numeric keypad is functional in the; 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 72 – Figure 7-10 Nearest Airports Window
  • Page 73 – 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 74 – Figure 7-13 Nearest VOR Page; NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page
  • Page 75 – NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page; NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 76 – • If the aircraft is within two nautical miles of an
  • Page 77 – 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 78 – 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 79 – 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 80 – 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
  • Page 81 – Figure 8-13 Store Flight Plan Confirmation
  • Page 82 – INVERT AND ACTIVATE A STORED
  • Page 83 – Figure 8-15 Trip Planning Page; Starting WPT; The Page Mode must be set to MANUAL
  • Page 84 – : An active flight plan or Direct-to must be; NOTE; : VNAV is advisory only and cannot be; Create a Vertical Navigation Profile
  • Page 85 – 0) With the ‘TARGET ALTITUDE’ field highlighted,; Knobs to select; Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU
  • Page 87 – 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 88 – Figure 9-4 Select Arrival Transition; Not all approaches in the database are approved for GPS; Load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure
  • Page 89 – Figure 9-7 Selecting an Approach Transition; Activate An Approach in the Active Flight Plan
  • Page 91 – SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD DISPLAYS; Figure 10-1 Page Menu
  • Page 92 – 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 93 – XM Weather is not intended to
  • Page 94 – Figure 10-9 Weather Data Link Page
  • Page 96 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group will; Weather Product Age; The age for each of the enabled products is displayed
  • Page 97 – 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 98 – Refer to the Ryan 9900BX pilot’s guide for a detailed; Displaying Traffic on the Traffic Map Page; Figure 10-12 Traffic Map Page
  • Page 99 – Figure 10-13 TAS Traffic on Navigation Map; Traffic Advisory; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Color
  • Page 100 – Figure 10-15 Obstacle Symbols; Displaying Terrain on the TAWS Page
  • Page 101 – Black; Enable/Disable Aviation Data; ) While the TAWS Page is displayed, press the; Figure 10-19 TAWS Page Menu
  • Page 102 – TAWS System; Enroute
  • Page 103 – Figure 10-20 PDA Alerting; Figure 10-21 Excessive Descent Rate; Negative Climb Rate After Takeoff; Don’t Sink; “Five-Hundred” Aural Alert
  • Page 104 – ) With the Navigation Map displayed, select the; Softkey. Terrain and; Figure 10-22 TAWS Symbols; When the Navigation Map Page is displayed, and a
  • Page 105 – Alert Type
  • Page 106 – The following system status annunciations may also be; Alert Annunciations; Figure 10-24 Alert Annunciation on the TAWS Page; Alert Annunciation; Figure 10-25 Alert Annunciation on the PFD
  • Page 107 – SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary display mode can also be manually; The Columbia 350/400 Airplane Flight
  • Page 108 – 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 109 – SECTION 12 – ANNUNCIATIONS; ALERTS; The Airplane Flight Manual supersedes
  • Page 110 – ALERT LEVEL DEFINITIONS
  • Page 111 – AIRCRAFT ALERTS; See the Airplane Flight Manual for information; WARNING Alerts
  • Page 112 – OXYGEN ON; Message Advisory Alerts; CO GUARDIAN MESSAGES
  • Page 113 – The following alert annunciations appear in the AFCS; Condition; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
  • Page 115 – When an LRU or an LRU function fails, a large red
  • Page 116 – System Annunciation
  • Page 117 – A red ‘X’ may be the result of an LRU or an LRU; Figure 12-6 G1000 System Failure Annunciations; ADVISORIES; This section describes various G1000 system message
  • Page 118 – Message
  • Page 119 – Alerts Window Message
  • Page 122 – GEA 71 Message Advisories
  • Page 123 – GRS 77 Message Advisories
  • Page 126 – BACKUP PATH
  • Page 127 – Signal augmentation 5-3
  • Page 132 – © 2006 Garmin Ltd. or its subsidiaries
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Integrated Flight Deck

Cockpit Reference Guide

Columbia

350/400

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Summary

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the Columbia 350/400 RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00567-00 Production release. Revision Date of Revision Affected Pages Description A B 3/066/06 i-Index-4i-Index-4 Production releaseAdded Columbia 350 parameters, TAWS changes, and S...

Page 8 - Blank Page

Garmin G1000 Cockpit Reference Guide for the Columbia 350/400 RR-2 RECORD OF REVISIONS Blank Page

Page 9 - TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW

Garmin G1000 Cockpit Reference Guide for the Columbia 350/400 i TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW .................................... 1-1 1.1 PFD/MFD Controls ................................................... 1-2 1.2 GCU 476 Controls .......................................................

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