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3. Garmin G1000 Pc Trainer For Cessna Nav Iii Download Mac

Garmin G1000 PC Trainer for Cessna NAV III by Garmin 010-10596-13 - The G1000 Trainer simulates the behavior of the G1000 system interface and provides you with a safer environment to learn the basics. 010-10596-06 010-10596-09 version 9 10 12 010-10596-12 010-10596-13 - Pilot Supplies at a Pilot Shop.

WARNING: The Garmin G1000, as installed in Cessna Nav III aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Nav III Cessna - Garmin G1000 NXi PC Trainer for Cessna NAV III PART NUMBER: 010-12675. G1000 PC Trainer for Cessna NAV III, Ver 13.02. Manufacturer/Supplier: Garmin SKU: 010-10596-13 All products sold include a CanWest Aerospace Certificate of Conformity.

Overview

Cessna NAVIII G1000 Trainer is a Shareware software in the category Miscellaneous developed by ASTURIAS GARMIN.

The latest version of Cessna NAVIII G1000 Trainer is currently unknown. It was initially added to our database on 04/24/2008.

Cessna NAVIII G1000 Trainer runs on the following operating systems: Mac.

Cessna NAVIII G1000 Trainer has not been rated by our users yet.

Write a review for Cessna NAVIII G1000 Trainer!

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Summary of Contents for Garmin G1000

• Page 1 Integrated Flight Deck Pilot’s Training Guide..
• Page 2 Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

• Page 3: Table Of Contents

  Flight and Ground Instruction ..............1 Level of Knowledge Attained ..............1 Ground Lesson 1.............3 INTRODUCTION AND GARMIN INTEGRATED FLIGHT DECK SYSTEM OVERVIEW .....3 Exercise 1.1:................. 3 Terminology and Review of Pertinent Federal Aviation Regulations........3 Exercise 1.2: Component Review .............6 Ground Lesson 2.............9..
• Page 4 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS)........45 Exercise 13.1: Flight Director and Autopilot Operation ..........45 Appendix..............47 CONSIDERATIONS ON USING THE GARMIN INTEGRATED FLIGHT DECK TO ENHANCE THE AERONAUTICAL DECISION MAKING (ADM) PROCESS AND SINGLE-PILOT RESOURCE MANAGEMENT (SRM)...47 GIFD Pilot’s Training Guide..

• Page 5: Introduction

  INTRODUCTION GARMIN Integrated Flight Deck (GIFD) The GIFD is a completely integrated avionics system, designed to fit a broad range of aircraft models. It is an all-glass fight deck that presents flight instrumentation, location, navigation, communication, and identification data on large-format, high-resolution displays. The digital data presentation on the GIFD puts all flight-critical information literally at the pilot’s fingertips.
• Page 6 BLANK PAGE GIFD Pilot’s Training Guide 190-00368-05 Rev. B..

• Page 7: Ground Lesson 1

  INTRODUCTION AND GIFD SYSTEM OVERVIEW Objectives Upon completion of this lesson, the pilot should be able to do the following: • Describe the basic components of the Garmin Integrated Flight Deck • Describe the communication between GIFD components Resources • GIFD Pilot’s Guide •..
• Page 8 • APV Approach with vertical guidance is an International Civil Aviation Organization (ICAO) term referring to specific ICAO criteria adopted in May 2000. This approach classification allows stabilized descent using vertical guidance without the accuracy required for traditional precision approach procedures. The US has developed criteria for lateral/vertical navigation (LNAV/VNAV) and LPV approach procedures that meet this approach classification.
• Page 9 5. When filling a flight plan, what suffix is used for a current Global Positioning System (GPS) database with WAAS? “/G” is the suffix used for GPS flight plans. 6. What are the position accuracy improvements with the WAAS? TSO-C129a systems: •..

• Page 10: Exercise 1.2: Component Review

  An Automatic Flight Control System provides pitch/roll steering guidance and sends commands to an autopilot to operate the flight control surfaces. 2. Describe the function of the following components of the Garmin Integrated Flight Deck: • GRS 77 The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading information to the Primary Flight Display (PFD) and the primary Integrated Avionics Unit (IAU;..
• Page 11 3. What is the primary interface used between the GIFD components? Digital, uni-directional Ethernet buses using a proprietary Garmin protocol are the primary communication links between Line Replaceable Units (LRUs).
• Page 12 BLANK PAGE GIFD Pilot’s Training Guide 190-00368-05 Rev. B..

• Page 13: Ground Lesson 2

  Ground Lesson 2 TRANSITION TO THE PRIMARY FLIGHT DISPLAY (PFD) Objectives Upon completion of this lesson, the pilot should be able to read, understand, and interpret the six primary flight instruments displayed on the PFD that indicate airspeed, attitude, altitude, vertical speed, turn rate/coordination, and heading.

• Page 14: Exercise 2.2: Instrumentation Depiction

  Exercise 2.2: Instrumentation Depiction Assume that the aircraft is flying with the following indications and fill in the appropriate fields on the sketch with this data. Note that some data is not displayed for certain GIFD installations. • Airspeed = 140 KIAS •..

• Page 15: Ground Lesson 3

  Ground Lesson 3 POWER-UP, SELF-TEST, CHECKLIST Objectives Upon completion of this lesson, the pilot should be able to correctly identify proper alignment of the AHRS/ADC, complete a system self-test, and verify the database data. Resources • GIFD Pilot’s Guide • GIFD PC-based Simulator Exercise 3.1: System Initialization 1.
• Page 16 9. A pilot is planning a fight to KAPA (Centennial Airport, Denver, CO) from KCOU (Columbia, MO). When arriving at the aircraft, the pilot notices that the Jeppesen database is out of date by 3 cycles (84 days). • Can the pilot make the flight under Instrument Flight Rules (IFR)? Yes, but one cannot file “/G”..

• Page 17: Ground Lesson 4

  MFD/PFD Control Unit (GCU). 3. Which Garmin LRU failure will cause the GIFD to lose Mode C/S capability? If an Air Data Computer (GDC 74) fails, the GTX 33 Transponder will lose the pressure altitude source, leaving it to operate in Mode A only.

• Page 18: Exercise 4.2: Practice (optional)

  Exercise 4.2: Practice (Optional) Using the GIFD PC-based Simulator, review the start-up process and verify the Jeppesen database effective dates. Also, practice entering various transponder codes and changing the operating mode using the PFD softkeys. GIFD Pilot’s Training Guide 190-00368-05 Rev. B..

• Page 19: Ground Lesson 5

  Ground Lesson 5 COM RADIO AND AUDIO PANEL OPERATION Objectives Upon completion of this lesson, the pilot should be comfortable manually and automatically tuning and selecting communication frequencies, while properly configuring the selections on the GMA 1347 Audio Panel. Resources •..

• Page 20: Exercise 5.2: Practice (optional)

  Exercise 5.2: Practice (Optional) Using the GIFD PC-based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below. 2. Enter the transponder code “3470” and set the transponder to ‘ALT’ mode. 3.

• Page 21: Exercise 5.3: Audio Panel Operation

  Exercise 5.3: Audio Panel Operation 1. Which key should be pressed on the Audio Panel (GMA 1347) to monitor a COM radio frequency without transmitting? Press the COM Key for the selected radio (COM1 or COM2) to monitor the desired communication radio.
• Page 22 BLANK PAGE GIFD Pilot’s Training Guide 190-00368-05 Rev. B..

• Page 23: Ground Lesson 6

  Ground Lesson 6 NAVIGATION Objectives Upon completion of this lesson, the pilot should be able to navigate using ground-based NAVAIDs and GPS while manually tuning VOR/LOC/ILS frequencies and creating GPS direct-tos and flight plans. Resources • GIFD Pilot’s Guide • GIFD PC-based Simulator Exercise 6.1: Land-based Navigational Aids 1.
• Page 24 7. With the NAV radio receiving the tuned VOR station, the corresponding Bearing Information Window displays the distance to bearing. What source provides the distance information? The GPS-derived great circle distance is displayed (note that this is not a DME distance).

• Page 25: Exercise 6.2: Practice (optional)

  Exercise 6.2: Practice (Optional) Using the GIFD PC-based Simulator, power up the system and configure the GIFD as needed for the following IFR clearance out of KAPA (Centennial Airport, Denver, CO): “N12345 is cleared to the Goodland, KS, airport, via the Thurman VOR, Byers VOR, then direct.

• Page 26: Exercise 6.3: Gps Navigation

  Exercise 6.3: GPS Navigation 1. Can a direct-to/flight plan be created using GPS on both the PFD and the MFD or must one or the other be used (if so, which one)? Either display can be used for creating a GPS direct-to or flight plan; the data automatically cross-fills to the other display.

• Page 27: Exercise 6.4: Practice (optional)

  Exercise 6.4: Practice (Optional) Using the GIFD PC based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below. 2. Enter the transponder code “1252” and set the transponder to ‘ALT’ mode. 3.

• Page 28: Exercise 6.5: Instrument Approaches

  Exercise 6.5: Instrument Approaches 1. When first selecting an approach, what is the default option that appears when the PROC Key is pressed? “Select Approach” is the first option displayed when the PROC Key is pressed. 2. What is the difference in how the HSI presents data between selecting Vectors-to-Final or an Initial Approach Fix during an instrument approach? When Vectors-to-Final is selected, the HSI sets the inbound approach course automatically and it can be intercepted in the same way it would when getting vectors to a..
• Page 29 9. What key must be pressed to add a departure procedure (DP or SID) and/or arrival procedure (AP or STAR) to a flight plan? Pressing the PROC Key gives access to a list of options that includes adding a departure or arrival procedure.

• Page 30: Exercise 6.6: Practice (optional)

  Exercise 6.6: Practice (Optional) Using the GIFD PC-based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below. 2. Enter the transponder code “5455” and set the transponder to ‘ALT’ mode. 3.

• Page 31: Exercise 6.7: Vertical Navigation (vnav)

  Exercise 6.7: Vertical Navigation (VNAV) 1. Where does one go to program a VNAV flight plan on the GIFD? In the flight plan, assign VNAV target altitudes to programmed waypoints for enroute and descent phases of flight. Altitudes may also be loaded from the database. The calculates Tent (TOD) and Bottom Of Decent (BOD) based on ground speed.

• Page 32: Exercise 6.8: Charts

  Exercise 6.8: Charts 1. How does one view the Safe-Taxi diagram on the MFD as well as on the PFD? The Safe-Taxi diagram can be viewed by enabling it in the Navigation Map Setup: On the MFD, press and hold down the CLR Key. This returns the MFD to the default MAP –..

• Page 33: Ground Lesson 7

  Ground Lesson 7 MULTI FUNCTION DISPLAY (MFD) OPERATION Objectives Upon completion of this lesson, the pilot should be able to locate, use, and configure data on the MFD during flight operations. Resources • GIFD Pilot’s Guide • GIFD PC-based Simulator Exercise 7.1: MFD Configuration and Controls 1.
• Page 34 8. Which page should be accessed in order to change the navigation data field options at the top of the MFD display? The AUX - System Setup Page provides options for changing the navigation information displayed in the MFD Navigation Data Box. 9.

• Page 35: Ground Lesson 8

  Ground Lesson 8 PRIMARY FLIGHT DISPLAY (PFD) OPERATION Objectives Upon completion of this lesson, the pilot should be able to configure and interpret data presented on the PFD during all phases of flight operations. Resources • GIFD Pilot’s Guide • GIFD PC-based Simulator Exercise 8.1: PFD Configuration and Controls 1.
• Page 36 9. Where is the control for the Altimeter barometric pressure setting located? The BARO Knob is located on the right-hand side of the PFD (in some installations, exists as the large outer knob of the CRS/BARO Knob). 10. What are the ranges of viewable tape in the Altimeter and Airspeed Indicator? The Altimeter has 600 feet viewable at a time;..

• Page 37: Ground Lesson 9

  Ground Lesson 9 EMERGENCY PROCEDURES Objectives Upon completion of this lesson, the pilot should be able to determine the types of emergencies with associated component failures and take appropriate action during emergencies or failures. Resources • GIFD Pilot’s Guide • GIFD PC-based Simulator Exercise 9.1: Emergencies and Failure Modes 1.
• Page 38 6. During a cross country flight, an AHRS failure occurs (failure indicated by a red “X” over the Attitude Indicator). Note: the aircraft is equipped with a GFC 700 AFCS. • Aside from the backup Attitude Indicator, what items can be used to ensure safe flight? •..

• Page 39: Ground Lesson 10

  Terrain Awareness. TAWS also provides aural alerts and additional pop-up visual alerts. 3. List the types of alerts that Garmin TAWS-B offers. 1. Forward Looking Terrain Avoidance (FLTA) 2. Forward Looking Obstacle Avoidance (FLOA) 3.
• Page 40 6. During which phase of flight is PDA active? PDA functions only during descent to land. 7. The NCR is only active during the departure phase of the flight. What condition(s) must exist to activate this alert? 1. Height above the terrain must be less than 700 feet. 2.

• Page 41: Ground Lesson 11

  Ground Lesson 11 TRAFFIC OPERATION Objectives Upon completion of this lesson, the pilot should be able to accurately interpret traffic data while both incorporating this information into the aeronautical decision making (ADM) process and understanding the limitations of these systems. Resources •..
• Page 42 7. When a Traffic Advisory is issued, is one allowed to deviate from the ATC assigned instructions? No, the traffic display is intended to assist the pilot in visual acquisition of these aircraft in VMC. TIS is not intended to be used as a collision avoidance system and does not relive the pilot responsibility to “see and avoid”..

• Page 43: Ground Lesson 12

  Ground Lesson 12 WEATHER OPERATION Objectives Upon completion of this lesson, the pilot should be able to understand and interpret weather information displayed in the cockpit. The pilot will be able to use this supporting information to enhance the decision-making process before and during the flight. Resources •..
• Page 44 3. List all XM Weather Products and their corresponding update rates. NEXRAD 5 min Cloud Tops 15 min Cell Movement 12 min County Warnings 5 min METARs 12 min AIRMETs 12 min TAFs 12 min SIGMETs 12 min Lightning 5 min Echo Tops 7.5 min TFRs..
• Page 45 10. A pilot is on a VFR flight from KXYZ to KABC. Currently, the altitude is 9,500 feet, 50 miles from KABC. Weather is predicted to be MVFR at the destination airport. Using the MFD, describe the steps that must be taken to receive a METAR and/or TAF at the destination airport.

• Page 46: Exercise 12.2: Lightning Detection

  Exercise 12.2: Lightning Detection 1. When flying an aircraft with a WX-500 Stormscope installed, where can the lightning data be displayed? Stormscope information can be shown on the PFD Inset Map and on the MFD Navigation Map and Stormscope pages. 2.

• Page 47: Exercise 12.3: Weather Radar

  Exercise 12.3: Weather Radar 1. Does the GWX 68 Airborne Weather Radar allow you to operate while on the ground? Yes, however, a caution will appear alerting the pilot to follow all safety precautions. WARNING: Begin transmitting only when it is safe to do so. If it is desired to transmit while the aircraft is on the ground, no personnel or objects should be within 11 feet of the antenna.
• Page 48 BLANK PAGE GIFD Pilot’s Training Guide 190-00368-05 Rev. B..

• Page 49: Ground Lesson 13

  GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) Objectives Upon completion of this lesson, the pilot should be able to understand the operation of the Garmin Automatic Flight Control System (AFCS) and use the autopilot throughout various phases of flight. Resources •..
• Page 50 7. When the go-around control is pressed, what flight director and autopilot functions can be expected? Pressing the go-around control engages the flight director in the wings level, nose up attitude and the autopilot disengages automatically. 8. List several ways the autopilot can be disengaged. When there is a system failure, automatic disengagement occurs.

• Page 51: Appendix

  DECK TO ENHANCE THE AERONAUTICAL DECISION MAKING (ADM) PROCESS AND SINGLE-PILOT RESOURCE MANAGEMENT (SRM) The Garmin Integrated Flight Deck has brought a number of improvements in cockpit technology to General Aviation (GA) aircraft. These improvements range from longer life and greater reliability of the primary instruments to a simplified pilot interface.

• Page 52: Flight Planning

  emergency. Nonetheless, it is imperative that the pilot double-check all autopilot inputs in order to avoid mode confusion and monitor them to ensure that the intended operation is taking place. If equipped with a GFC 700 AFCS, it is also important for pilots to understand the capabilities and limitations of the system.
• Page 53 WEATHER AWARENESS In this discussion so far, the focus has been on SRM. Now, attention will be turned to leveraging the various data inputs from the on-board weather sensors, datalinks, traffic awareness, and terrain awareness functions. Proper understanding of both the operation of these various tools and their integration with the pilot’s aeronautical decision making (ADM) process can bring significant safety gains to the GA feet.
• Page 54 TRAFFIC AWARENSS Traffic Collision and Avoidance Systems (TCAS) represent another technological advance that has been made in the area of traffic avoidance. Originally developed for large commercial aircraft, TCAS technology is now starting to trickle down features and capabilities to the GA feet. For example, the GTX 33 Mode-S Transponder can be used as an optional component in GIFD- equipped aircraft and brings Traffic Information Service (TIS) data directly to the cockpit.
• Page 55 FINAL THOUGHTS In conclusion, as GA aircraft and pilots transition to 21st-century technology, the Garmin Integrated Flight Deck provides a number of safety-enhancing benefits. Although automation in the cockpit should be embraced, both its positive and negative impacts on the safety of flight should be recognized and understood.
• Page 56 BLANK PAGE GIFD Pilot’s Training Guide 190-00368-05 Rev. B..
• Page 57 Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown Business Park Southampton, SO40 9RB, U.K.

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Summary of Contents for Garmin G1000

Garmin G1000 Pc Trainer For Cessna Nav Iii Download Mac

• Page 1 G1000 pilot’s training guide..
• Page 2 Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 3: Copyright

  Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants per- mission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage..

• Page 4: Table Of Contents

  Purpose Flight and Ground Instruction Level of Knowledge Attained Ground Lesson 1 ...................3 Introduction and G1000 System Overview Exercise 1.1: Terminology and Review of Pertinent Federal Aviation Regulations Exercise 1.2: Component Review Ground Lesson 2 ...................5 Transition to the Primary Flight Display (PFD) Exercise 2.1: Instrumentation Layout..

• Page 5: Table Of Contents

  Procedure 11 ...................42 Flying the Vectors Approach Appendix ....................44 The G1000 Integrated Avionics System and Considerations of Its Use to Enhance the Aeronautical Decision Making (ADM) Process and Single-pilot Resource Management (SRM). 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..
• Page 6 TABLE OF CONTENTS This page intentionally left blank Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 7: Introduction

  G1000 Integrated Cockpit System The G1000™ is a completely integrated avionics system designed to fit a broad range of aircraft models. It is an all-glass flight deck that presents flight instrumentation, location, navigation, communication and identification data on large-format, high-res- olution displays.
• Page 8 INTRODUCTION This page intentionally left blank Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 9: Ground Lesson 1

  INTRODUCTION AND G1000 SYSTEM OVERVIEW Objectives Upon completion of this lesson, the pilot should be able to do the following: • Describe the basic components of the G1000 Integrated Avionics System • Describe the communication between G1000 components Resources •..

• Page 10: Exercise 1.2: Component Review

  1. Define the following equipment abbreviations and acronyms: • AHRS • ADC • TIS • Terrain 2. Describe the function of the following components of the G1000 Integrated Avionics System: • GRS 77 • GMU 74 • GIA 63 • GDU 1040 •..

• Page 11: Ground Lesson 2

  • Airspeed = 120 KIAS • True Airspeed = 120 KTAS • Altitude = 6760 ft. • Vertical Speed = 0 fpm • Heading = 95° • Altimeter Setting = 30.15” Hg 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 12: Ground Lesson 3

  4. Where can one verify the effective dates of the Jeppesen database during the initial system start-up? 5. If the Jeppesen database is not current in the G1000, can the system still be used for IFR flight? 6. A pilot is planning a flight to KAPA (Centennial Airport, Denver, CO) from KCOU (Columbia, MO). When arriving at the aircraft, the pilot notices that the Jeppesen database data is out of date by 3 cycles (84 days).

• Page 13: Ground Lesson 4

  G1000 PC-based Simulator Exercise 4.1: Operating Modes and Code Entry 1. Which transponder mode of operation does the G1000 system default to when it is first powered up if it is equipped with the Garmin mode S transponder (GTX 33)? 2.

• Page 14: Ground Lesson 5

  G1000 PC-based Simulator Exercise 5.1: COM Operation and Methods of Frequency Tuning 1. Is the active frequency being used displayed to the inside or to the outside relative to the bezel of the G1000 navigation displays (GDU 1040)? 2. In what color is the active frequency displayed? 3.

• Page 15: Exercise 5.2: Practice (optional)

  GROUND LESSONS Exercise 5.2: Practice (Optional) Using the G1000 PC-based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below. 2. Enter the transponder code “3470” and set the transponder to “ALT” mode.

• Page 16: Ground Lesson 6

  Exercise 6.2: Practice (Optional) Using the G1000 PC-based Simulator, power up the system and configure the G1000 as needed for the following IFR clear- ance out of KAPA (Centennial Airport, Denver, CO): “N12345 is cleared to the Goodland, KS, airport via the Thurman VOR, Byers VOR, then direct.

• Page 17: Exercise 6.3: Gps Navigation

  5. Describe some of the advantages of using the Flight Plan function as opposed to continuous direct-to navigation. Exercise 6.4: Practice (Optional) Using the G1000 PC based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below.

• Page 18: Exercise 6.5: Instrument Approaches

  STAR) to a flight plan? 10. When navigating in VOR1, VOR2, LOC1, or LOC2 mode, if an ILS, LOC, or VOR approach is selected, where is the frequency for the primary approach navigational aid automatically placed? Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 19: Exercise 6.6: Practice (optional)

  GROUND LESSONS Exercise 6.6: Practice (Optional) Using the G1000 PC-based Simulator, power up the system. 1. Verify the Jeppesen database effective dates and note those dates in the space provided below. 2. Enter the transponder code “5455” and set the transponder to “ALT” mode.

• Page 20: Ground Lesson 7

  8. Which page should be accessed in order to change the data field options at the top of the MFD display? 9. Which key should be pressed and held for 2 seconds to automatically and quickly return to the Navigation Map page? (exercise continued on next page) Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..
• Page 21 Weather is predicted to be MVFR with scattered rain over the entire route of flight. How would one configure the MFD to give the best presentation of data for this flight? Assume that a GDL-69 weather datalink is installed in the aircraft. 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 22: Ground Lesson 8

  9. Where is the control for the altimeter barometric pressure located? 10. How many feet of altitude and how many knots of airspeed make up the viewable portions of the altimeter and airspeed indicator, respectively? (exercise continued on next page) Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..
• Page 23 It is daytime, although visibility is limited to a few miles with cloud tops at 10,000 feet MSL. What options should be selected to display on the PFD map inset? 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 24: Ground Lesson 9

  4. Describe the service volume for the Traffic Information Service. 5. Is the terrain awareness feature in the G1000 system certified to allow deviations from ATC assigned altitudes? 6. In the terrain awareness feature, what do the colors red and yellow each represent? 7.

• Page 25: Ground Lesson 10

  Exercise 10.1: Emergencies and Failure Modes 1. If one display fails, which mode does the system automatically go into? 2. How is an AHRS failure indicated on the G1000? 3. When the AHRS and/or ADC fail, what remedial action should be taken by the pilot? 4.
• Page 26 6b. What are the next actions that should be taken concerning the completion of the flight? Note that, depending on the circumstances, the following action items may occur in a different order. 6c. When the AHRS fails, what is the other piece of information that is lost besides attitude? Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 27: Ground Lesson 11

  1. Briefly describe the theory of how weather and radio information are provided to the aircraft. 2. What types of data link weather are displayed on MFD/PFD, and what appropriate steps must be taken to get there? (exercise continued on next page) 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..
• Page 28 10. A pilot is on a VFR flight from KXYZ to KABC. Currently, the altitude is 9,500 feet, 50 miles from KABC. Weather is pre- dicted to be MVFR at the destination airport. Using the MFD, describe the steps that must be taken to receive a METAR and/or TAF at the destination airport. Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 29: Ground Lesson 12

  GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) Objectives Upon completion of this lesson, the pilot should be able to understand the operation of the Garmin Automatic Flight Control System (AFCS) and use the Autopilot throughout various phases of flight. Resources •..
• Page 30 Autopilot to follow all of the departure procedure up to the final cruising altitude? 10. Using the scenario above, configure the Autopilot to intercept an airway. Currently, the Autopilot is set to HDG mode and ALT hold mode. Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 31: Procedure 1

  An approach where there is typically no procedure turn required to get established on the inbound course to the FAF is the first example. We use GPS RWY 12 at KPRC to show how the G1000 sequences through an approach and what type of annunciation and range factor changes can be expected.
• Page 32 PROCEDURES Figure 1 Approach with No Procedure Turn Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 33: Procedure 2

  FLYING THE MISSED APPROACH As the MAP is passed, if the runway is not in view, a missed approach must be performed. The G1000 continues to give guidance along an extension of the final course segment (FAF to MAP) until manual initiation of the missed approach procedure.

• Page 34: Procedure 3

  FLYING THE PROCEDURE TURN The procedure turn portion of the approach is stored as one of the legs of the approach. For this reason the G1000 requires no special operations from the pilot (other than flying the procedure turn itself) beyond what is required for any other type of ap- proach.
• Page 35 PROCEDURES Figure 2 Flying the Procedure Turn 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 36: Procedure 4

  Press the PROC key and select the VOR DMW RWY 7 approach. From the transitions window, select “HIDOX” as the IAF. Choose ‘LOAD?’ or ‘ACTIVATE?’ Within 30 nm of KFMN, the G1000 switches from en route mode to terminal mode. The CDI range gradually transitions from 5.0 to 1.0 nm, full range deflection.

• Page 37: Flying The Dme Arc

  PROCEDURES Figure 3 Flying the DME Arc and Vectors to the DME Arc 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 38: Procedure 5

  ‘NEXT DTK 072°’ is displayed. As the waypoint approaches, the message is replaced by a turn advisory ‘TURN TO 072°’. Initiate a standard rate turn to this course heading. At 2.0 nm from the FAF (PINTO), the G1000 switches from terminal mode to 0.3 nm. CDI scaling is tightened from 1.0 to 0.3 nm, full range deflection.

• Page 39: Procedure 6

  11. As the plane approaches FIKKA from within the holding pattern, the waypoint message ‘NEXT DTK 090°’ is dis- played. 12. At 2.0 nm from the FAF, the G1000 switches from terminal mode to approach mode. CDI scaling is tightened from 1.0 to 0.3 nm, full range deflection.
• Page 40 : When the message ‘RAIM is not available’ is displayed in the Alerts Window on the PFD a missed NOTE approach must be executed. Figure 4 Flying an Approach with a Hold Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 41: Procedure 7

  Certain approach, departure and arrival procedures in the Jeppesen database contain course from fix flight plan legs. The G1000 is able to load these legs into the flight plan along with the rest of the procedure data, and to provide navigation along these legs.
• Page 42 PROCEDURES Figure 5 Course from Fix to Distance or Course from Fix to DME Distance Garmin G1000 Pilot’s Training Guide 190-00368-03 Rev. A..

• Page 43: Procedure 8

  Note that within a few seconds of pressing the SUSP softkey to release suspend mode and start the missed approach sequence, ‘SUSP’ is re-displayed above the SUSP softkey as the G1000 returns to suspend mode. This is normal when flying a course from a fix to altitude leg and indicates that automatic leg sequencing is suspended.

• Page 44: Procedure 9

  (HFD VOR). The actual desired track (DTK) depends on the ground speed and distance from the HFD VOR. Once the SUSP softkey is pressed, the G1000 automatically sequences to each waypoint along the remainder of the departure route, including the selected transition.

• Page 45: Flying A Course From Fix To Manual Sequence

  PROCEDURES Figure 6 Flying a Course from Fix to Manual Sequence 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 46: Procedure 10

  Precision approaches can be performed with the built in Nav (VOR/localizer/glideslope) receivers. Prior to reaching the FAF the CDI should be set to NAV1 or NAV2. The G1000 automatically switches the external CDI output from GPS to NAV1 or NAV2 as the final approach course is intercepted.

• Page 47: Flying The Ils Approach

  final approach course continues. Do NOT follow this extended course. If a missed approach is required, follow the missed approach procedures as published on the approach plate. Press the SUSP softkey to return to automatic sequencing of waypoints. Figure 7 Flying the ILS Approach 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 48: Procedure 11

  As the CDI needle centers, make any remaining course corrections to establish the plane on the final approach course. 10. At 2.0 nm from the FAF (GELTS), the G1000 switches from terminal mode to approach mode. The CDI scaling is tight- ened from 1.0 to 0.3 nm, full range deflection.

• Page 49: Flying The Vectors Approach

  PROCEDURES Figure 8 Flying the Vectors Approach 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..

• Page 50: Appendix

  Aviation (GA) aircraft. These improvements range from longer life and greater reliability of the primary instruments to a simpli- fied pilot interface. With the addition of new technologies, the G1000 system is capable of providing the pilot with a wider variety of information about the flight environment, thereby leading to greater situational awareness and reduced pilot workload.
• Page 51 Rather than performing continuous direct-to navigation with the GPS, taking the time on the ground to enter a full flight plan allows the G1000 to enhance the navigation experience. First, the pilot will be able to visually inspect the route of flight on the MFD map, once at altitude, so as to verify both terrain clearance (using the terrain awareness overlay) and active..
• Page 52 Originally developed for large commercial aircraft, TCAS technology is now starting to trickle down features and capabilities to the GA fleet. For example, the GTX 33 Mode-S transponder can be used as an optional component in G1000- equipped aircraft and brings Traffic Information Service (TIS) data directly to the cockpit.
• Page 53 190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide..
• Page 54 Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/1794.519944 f: 44/1794.519222 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan P: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2004, 2005 Garmin Ltd. or its subsidiaries 190-00368-03 Rev. A..