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pilot’s training guide

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Summary of Contents for Garmin G1000

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G1000 pilot’s training guide…
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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…
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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.
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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…
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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…
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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.
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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…
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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 •…
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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.
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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.
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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.
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: 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.
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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.
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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…
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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.
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190-00368-03 Rev. A Garmin G1000 Pilot’s Training Guide…
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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…

Источник

G1000

Cessna

Nav III

Garmin

Справочное руководство для экипажа

В данном руководстве описывается работа программного обеспечения системы версии 0563.05 или более поздней для самолетов Cessna 172R, 172S, 182T, T182T, 206H, и T206H. При сравнении информации в этом руководстве с более ранними или более поздними версиями программного обеспечения возможны некоторые отличия в эксплуатации.

Garmin International. Inc., 1200 East 151st Street, Olathe, Kansas 66062, USA

Тел.: 913/397.8200	Факс: 913/397.8282
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Тел.: 503/391.3411	Факс: 503/364.2138
Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Houndsdown Business Park, Southampton, SO40 9 RB,
U.K.
Тел.: 44/0870.8501241	Факс: 44/0870.8501251
Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan
Тел.: 886/02.2642.9199	Факс: 886/02.2642.9099

Адрес в интернете: www.garmin.com

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Garmin® и G1000® – зарегистрированные торговые маргки компании Garmin Ltd. или ее филиалов. FliteChartsTM и SafeTaxiTM – торговые марки компании Garmin Ltd. Или ее филиалов. Эти торговые марки не могут быть использованы без предварительного разрешения компании Garmin.

NavData® – это зарегистрированная торговая марка компании Jeppesen, Inc.; Stormscope® – это зарегис-

трированная торговая марка компании XM Satellite Radio, Inc.; Honeywell® и Bendix/King® – это зарегист-

рированные торговые марки компании Honeywell International, Inc.; CO Guardian – это зарегистрированная торговая марка компании CO Guardian, Inc.

Garmin G1000: Справочное руководство для Cessna Nav III		3
Данный перевод не является официальным и может использоваться только для справки	IDEPENDENT

	REPRESENTATIVE

ПРЕДУПРЕЖДЕНИЯ, ПРЕДОСТЕРЕЖЕНИЯ И ПРИМЕЧАНИЯ

ПРЕДУПРЕЖДЕНИЕ: Навигация и огибание рельефа местности НЕ должны осуществляться на основе функции земного ландшафта (terrain function). Функция Terrain Proximity, которая предупреждает о близости земли G1000 НЕ рассчитана на то, чтобы ее использовали как основной инструмент предотвращения столкновения с землей и не освобождает пилота от ответственности и необходимости следить за окрестностями и ландшафтом во время полета. Функция Terrain Proximity используется только как вспомогательное средство для предупреждения столкновения с землей и не сертифицирована для использования в системах, где требуется сертифицированная система предотвращения столкновения с землей. Данные по земному ландшафту предоставляются сторонним источником.Garmin не может независимо проверять точность данных по земному ландшафту.

ПРЕДУПРЕЖДЕНИЕ: Отображаемые минимальные безопасные высоты (MSA) носят рекомендательный характер и не могут служить единственным источником информации о препятствиях для предотвращения столкновения с землей. Необходимо всегда обращаться к аэронавигационным картам для получения информации по минимальным безопасным высотам.

ПРЕДУПРЕЖДЕНИЕ: Высота, рассчитываемая приемниками G1000 GPS, является геометрической высотой над средним уровнем моря и может значительно отличаться от высоты, которую показывают барометрические высотомеры, такие как GDC 74A Air Data Computer, или другие высотомеры на борту самолета. Запрещено использовать высоту по GPS для вертикальной навигации. Всегда используйте барометрическую высоту, которая отображается на G1000 PFD или других барометрических высотомерах на борту самолета.

ПРЕДУПРЕЖДЕНИЕ: Не используйте информацию из устаревшей базы данных. Базы данных, которые используются в системе G1000, должны регулярно обновляться, чтобы гарантировать достоверность информации. Пилоты, которые пользуются устаревшими базами данных, делают это исключительно на свой страх и риск..

ПРЕДУПРЕЖДЕНИЕ: Не используйте базовую карту (ландшафта и водных объектов) для основной навигации. Базовая карта является дополнением к другим одобренным источникам навигационных данных и должна рассматриваться только как вспомогательное средство для информирования о положении воздушного судна.

ПРЕДУПРЕЖДЕНИЕ: Информация по воздушному движению, которая отображается на многофункциональном дисплее MFD G1000, является дополнительной к визуальному наблюдению воздушного движения. Пилоты должны маневрировать воздушным судном, основываясь только на информации от авиадиспетчерской службы или на визуальном наблюдении встречного воздушного движения.

ПРЕДУПРЕЖДЕНИЕ: Назначение прибора Stormscope не предполагает его использование в опасных погодных условиях (например, для входа в грозу). Информацию прибора Stormscope, которая отображена на многофункциональном дисплее MFD G1000, можно использовать только для того, чтобы избегать опасных погодных условий, но не для полетов в опасных погодных условиях.

ПРЕДУПРЕЖДЕНИЕ: Прибор GDL 69 Weather запрещено использовать для входа в зону с опасными погодными условиями. Метеорологическая информация, которая отображается на приборе GDL 69 Weather, должна использоваться только для того, чтобы избегать опасных погодных условий, но не для полетов в опасных погодных условиях.

ПРЕДУПРЕЖДЕНИЕ: Метеорологические данные NEXRAD должны использоваться только для долгосрочного планирования. Из-за свойственного системе отставания в передаче данных и относительного устаревания информации метеорологические данные NEXRAD не могут быть использованы для краткосрочного планирования с целью избежать плохих метеоусловий.

4			Garmin G1000: Справочное руководство для Cessna Nav III
IDEPENDENT		Данный перевод не является официальным и может использоваться только для справки

	REPRESENTATIVE

ПРЕДУПРЕЖДЕНИЯ, ПРЕДОСТЕРЕЖЕНИЯ И ПРИМЕЧАНИЯ

ПРЕДУПРЕЖДЕНИЕ: Garmin G1000, установленный на воздушное судно Cessna Nav III, обладает очень высокой степенью функциональной целостности. Однако пилот должен понимать, что невозможно обеспечить мониторинг и/или внутренний тест на отсутствие всех возможных отказов системы. Существуют очень небольшая вероятность некорректной работы прибора G1000, при которой будет отсутствовать индикация неисправной работы прибора. Поэтому пилот обязан выявить подобную ситуацию путем перекрестной проверки всей возможной взаимосвязанной информации в кабине.

ПРЕДУПРЕЖДЕНИЕ: Для обеспечения безопасности правила эксплуатации прибора G1000 должны быть изучены на земле.

ПРЕДУПРЕЖДЕНИЕ: Эксплуатация Глобальной системы навигации (GPS) осуществляется правительством Соединенных Штатов Америки, которое несет ответственность за ее точность и проводит техническое обслуживание системы. В систему GPS могут быть внесены изменения, которые могут повлиять на точность и работу оборудования GPS. Отдельные узлы системы Garmin G1000 используют GPS как точное электронное устройство (NAVAID), поэтому (как и в других устройствах NAVAID) информация, предоставляемая прибором G1000, может быть неправильно использована или неправильно истолкована и из-за этого стать небезопасной.

ПРЕДУПРЕЖДЕНИЕ: Для того чтобы снизить возможные риски небезопасной работы, внимательно прочитайте Руководство по эксплуатации и поймите все аспекты работы G1000. Основательно потренируйтесь работать с прибором перед его фактической эксплуатацией. Во время полета сравнивайте показания G1000 со всеми возможными источниками навигационной информации, включая информацию от других приборов NAVAID, визуальное наблюдение, аэронавигационные карты и т.д. Для безопасности всегда определяйте причину любого расхождения в данных, перед тем как продолжить навигацию.

ПРЕДУПРЕЖДЕНИЕ: Приведенные в данном Руководстве иллюстрации являются просто примерами. Запрещено использовать G1000, чтобы войти в зону грозы. Информационный циркуляр Федерального авиационного агентства США (Тема: Грозы), а также Руководство по авиационной информации (AIM) рекомендуют облетать «по крайней мере за 20 миль любую грозу, которая определена как сильная или которая посылает сильное радиолокационное эхо».

ПРЕДУПРЕЖДЕНИЕ: Лампы, находящиеся внутри данного прибора, могут содержать ртуть (HG) и должны перерабатываться или утилизироваться в соответствии с местными, государственными или федеральными законами. Для получения более подробной информации посетите наш сайт www.garmin.com/aboutGarmin/ environment/disposal.jsp

ПРЕДУПРЕЖДЕНИЕ: Из-за аномалий магнитного поля земли эксплуатация G1000 в следующих зонах может привести к потере показаний надежного угла тангажа и курса. К северу от 70° северной широты и к югу от 70° южной широты. Зона к северу от 65° северной широты между 75° и 120° западной долготы. Зона к югу от 55° южной широты между 120° и 165° восточной долготы.

ПРЕДОСТЕРЕЖЕНИЕ: Дисплеи PFD и MFD используют линзу, покрытую специальным противоотражающим слоем, который очень чувствителен к кожным маслам, воску и абразивным чистящим средствам. ЧИСТЯЩИЕ СРЕДСТВА, КОТОРЫЕ СОДЕРЖАТ АММИАК, ПРИВЕДУТ К ПОВРЕЖДЕНИЮ ПРОТИВООТРАЖАЮЩЕГО СЛОЯ. Очень важно чистить линзу чистой, без бумажной пыли и пуха тряпочкой и чистящим средством для офтальмологических линз, которое безопасно для противоотражающих покрытий.

Garmin G1000: Справочное руководство для Cessna Nav III		5
Данный перевод не является официальным и может использоваться только для справки	IDEPENDENT

	REPRESENTATIVE

ПРЕДУПРЕЖДЕНИЯ, ПРЕДОСТЕРЕЖЕНИЯ И ПРИМЕЧАНИЯ

ПРЕДОСТЕРЕЖЕНИЕ: Garmin G1000 не содержит деталей, техническое обслуживание которых может быть проведено пользователем. Ремонт может проводиться только авторизованным сервисным центром Garmin. Несанкционированный ремонт или модификации могут аннулировать как гарантию производителя, так и право пилота эксплуатировать прибор в соответствии с положениями FAA/FCC (Федерального авиационного агентства США, Федеральной комиссии связи США).

ПРИМЕЧАНИЕ: При использовании прибора Stormscope существуют несколько атмосферных явлений в дополнение к отображению ближайшей грозовой активности, которые могут привести к отображению отдельных точечных разрядов в режиме отображения разрядов молнии. Однако именно концентрация двух или более точечных разрядов в режиме отображения разрядов молнии означает грозовую активность, если после очистки экрана эти точечные разряды появляются снова.

ПРИМЕЧАНИЕ: Все иллюстрации в данном документе, включая рисунки дисплеев и экранов на панели G1000, могут быть изменены и не обязательно отражают самую последнюю версию G1000 системы и новейшие авиационные базы данных. Рисунки оборудования могут немного отличаться от фактического оборудования.

ПРИМЕЧАНИЕ: Данный прибор соответствует требованиям части 15 Положений FCC (Федеральной комиссии связи США). Эксплуатация данного прибора осуществляется на основе следующих положений: (1) прибор не может вызвать критические помехи и (2) прибор подвержен любому взаимному влиянию, включая помехи, которые могут привести к некорректной работе.

ПРИМЕЧАНИЕ: GDU 1040 и GDU 1044B PFD/MFD могут потребовать предварительного прогрева в течение 30 минут, если они продолжительное время находились при температуре -40°С. Может потребоваться предварительный прогрев в течение 15 минут, если приборы продолжительное время находились при температуре -30°С.

ПРИМЕЧАНИЕ: Данный продукт, его упаковка и компоненты включают в себя химические вещества, которые известны в штате Калифорния как канцерогены, а также способны привести к врожденных дефектам и повредить репродуктивное здоровье. Это примечание дано в соответствии с Положением 65 штата Калифорния. Если у вас возникнут вопросы или вам потребуется дополнительная информация, обращайтесь, пожалуйста, на наш сайт в интернете www.garmin.com/prop65.

ПРИМЕЧАНИЕ: Помехи от ретрансляторов GPS, работающих в ближайших ангарах, могут привести к периодической потере отображения окон углового пространственного положения и курса, когда самолет находится на земле. Перемещение самолета на 100 и более ярдов (примерно 100 метров – прим. переводчика) от источника помех устранит проблему.

ПРИМЕЧАНИЕ: При ношении поляризационных очков экраны приборов могут казаться бледными и нечеткими.

6			Garmin G1000: Справочное руководство для Cessna Nav III
IDEPENDENT		Данный перевод не является официальным и может использоваться только для справки

	REPRESENTATIVE

ПРЕДУПРЕЖДЕНИЯ, ПРЕДОСТЕРЕЖЕНИЯ И ПРИМЕЧАНИЯ

	Номер по каталогу запасных	Внесенное изменение
	частей и сборочных единиц

		Добавлены приборы XM Radio и XM Weather
		Добавлена функция ADF
		Добавлена функция DME
		Добавлены указатели BRG1/BRG2
	190-00384-03 (Изменение А)	Добавлена функция двойной работы аудиопанели
	Добавлены параметры С172

		Изменен вектор воздушной скорости
		Изменен вектор высоты
		Добавлена функция Checklist (карта проверки)
		Добавлена функция Flight ID

	190-00384-03 (Изменение В)	Обновлены номера программного обеспечения системы

	190-00384-04 (Изменение А)	Изменен формат Руководства
	Добавлена функция TAS


	190-00384-04 (Изменение В)	Добавлены клавиша DONE, страница XM-INFORMATION и
	страница XM-RADIO


		Добавлено объяснение работы EIS окна в случае
		превышения параметров
		Добавлено новое объяснение работы системы внутренней
	190-00384-05 (Изменение А)	связи
	Добавлено объяснение работы Stormscope при потере

		данных по курсу полета
		Добавлена функция TAWS-B
		Добавлен новый сумматор объема топлива
		Обновлены сообщения системы G1000

		Добавлены новые параметры программного обеспечения
		GDU 7.00 (WAAS, VNAV&Charts)
		Добавлена функция AFCS для 182 и 206
	190-00384-06 (Изменение А)	Добавлены инструкции по загрузке базы данных
		Обновлены сообщения системы G1000
		Номера программного обеспечения предыдущей системы
		объединены с 0563.00

	190-00384-07	Добавлены параметры GDU 8.02, Airways и ADS-B

	190-00384-08	Добавлены параметры GDU 8.20, включая градиентный
	задний фон на PFD и GFC 700 для С172

Garmin G1000: Справочное руководство для Cessna Nav III		7
Данный перевод не является официальным и может использоваться только для справки	IDEPENDENT

	REPRESENTATIVE

ПРЕДУПРЕЖДЕНИЯ, ПРЕДОСТЕРЕЖЕНИЯ И ПРИМЕЧАНИЯ

8			Garmin G1000: Справочное руководство для Cessna Nav III
IDEPENDENT		Данный перевод не является официальным и может использоваться только для справки

	REPRESENTATIVE

СОДЕРЖАНИЕ

ГЛАВА 1: ОБЗОР СИСТЕМЫ . . . . . . . . . . . . . . .	. 13. . . .	2. .9. .	СКОРОСТЬ И НАПРАВЛЕНИЕ ВЕТРА . . . . . . . .	. .	.38. . . . .
1.1	ПАНЕЛЬ PFD/MFD . . . . . . . . . . . . . . . . . . . . .	14. . . .	.2.10. .	УНИВЕРСАЛЬНЫЙ. . ТАЙМЕР . . . . . . . . . . . . .	. .	.39. . . . . . .
1.2	КЛАВИШИ PFD . . . . . . . . . . . . . . . . . . . . . . .	17. . . . .	. . .	. . .
1.3	КЛАВИШИ MFD . . . . . . . . . . . . . . . . . . . . . .	20. . . . .	ГЛАВА. . . . . 3:. СИСТЕМА ИНДИКАЦИИ РАБОТЫ
1.4	ГРУППЫ СТРАНИЦ MFD . . . . . . . . . . . . . . . . . .	21. . . . .	ДВИГАТЕЛЯ. . . . (EIS) . . . . . . . . . . . . . . . . . . . .	. .	41. . . . . . . . . . .
1.5	ВЕРТИКАЛЬНАЯ НАВИГАЦИЯ . . . . . . . . . . . . . .	22. . . . .	3.1.	ОКНО ДВИГАТЕЛЯ (ENGINE DISPLAY) . . . . . . .	. .	. 41. . . . .
1.6	ПОДСВЕТКА . . . . . . . . . . . . . . . . . . . . . . . . .	24. . . .	3..2. . .	ОКНО. . . БЕДНОЙ СМЕСИ . . . . . . . . . . . . . . . .	. .	44. . . . . . . . .
1.7	XM RADIO – АВТОМАТИЧЕСКОЕ СНИЖЕНИЕ			БЕЗНАДДУВНОЕ ВОЗДУШНОЕ СУДНО . . . . . . .	. .	. 47. . . . .
	ГРОМКОСТИ . . . . . . . . . . . . . . . . . . . . . . . . .	24. . . .	. . . .	ВОЗДУШНОЕ. . . СУДНО С ТУРБОНАДДУВОМ . . . . .	. .	. 47. . . .
1.8	ОБНОВЛЕНИЕ БАЗЫ ДАННЫХ . . . . . . . . . . . . . . .	24. . . .	3.3.	СИСТЕМНЫЙ ДИСПЛЕЙ (SYSTEM DISPLAY) . . . .	. .	.47. . .
	База данных JEPPESEN AVIATION . . . . . . . . . . . . .	24. . . .	. .
	Базы данных GARMIN . . . . . . . . . . . . . . . . . . .	25. . . . .	ГЛАВА. . . . 4: NAV/COM
			И БОРТОВОЙ ОТВЕТЧИК . . . . . . . . . . . . . . . . . .	. .	. 51. . . . . . . . . .
ГЛАВА 2: ПИЛОТАЖНЫЕ ПРИБОРЫ . . . . . . . . .	27. . . .	4.1	СООБЩЕНИЯ СИСТЕМЫ РАДИОСВЯЗИ . . . . . .	. .	.53. . . .
2.1	ИНДИКАТОР ВОЗДУШНОЙ СКОРОСТИ . . . . . . . . . .	29. . . .	4.2	ГРОМКОСТЬ . . . . . . . . . . . . . . . . . . . . . .	. .	53. . . . . . . . . . . .
	ПОКАЗАНИЯ СКОРОСТИ . . . . . . . . . . . . . . . . . .	29. . . .	4. .3. . .	АВТОМАТИЧЕСКАЯ РЕГУЛИРОВКА ГРОМКОСТИ	. .	. 53. .
	ДИАПАЗОН СКОРОСТИ . . . . . . . . . . . . . . . . . . .	29. . . .	4..4. .	БЫСТРАЯ.	АКТИВАЦИЯ 121500 MHZ . . . . . . . .	. .	.53. . . . .
	ВЕКТОР ТРЕНДА ВОЗДУШНОЙ СКОРОСТИ . . . . . . . . .	29. . .	4.5	РАДИО NAV (ОПЦИИ) . . . . . . . . . . . . . . . .	. .	. 53. . . . . . . . .
	СПРАВОЧНАЯ ИНФОРМАЦИЯ			Радио DME (опция) . . . . . . . . . . . . . . . . . .	. .	53. . . . . . . . . .
	ПО ВЕРТИКАЛЬНОЙ СКОРОСТИ . . . . . . . . . . . . . .	29. . . .	. .	Радио ADF (опция) . . . . . . . . . . . . . . . . . .	. .	. 54. . . . . . . . . .
2.2	АВИАГОРИЗОНТ . . . . . . . . . . . . . . . . . . . . . . .	29. . . .	4..6. . .	АВТО. . -НАСТРОЙКА ЧАСТОТЫ . . . . . . . . . . . .	. .	.54. . . . . . .
2.3	ВЫСОТОМЕР . . . . . . . . . . . . . . . . . . . . . . . .	30. . . .	. . . .	Авто. . .-настрока на дисплее PDF . . . . . . . . . . .	. .	. 54. . . . . . .
	УКАЗАТЕЛЬ ВЫБРАННОЙ ВЫСОТЫ . . . . . . . . . . . . .	30. . . .	.	Авто-настройка в MFD . . . . . . . . . . . . . . . .	. .	. 54. . . . . . . . .
	ВЕКТОР ТРЕНДА ВЫСОТЫ . . . . . . . . . . . . . . . . .	30. . . . .	4.7 . .	БОРТОВОЙ ОТВЕТЧИК . . . . . . . . . . . . . . . .	. .	54. . . . . . . . .
	УСТАНОВКА БАРОМЕТРА . . . . . . . . . . . . . . . . . .	30. . . .	. . . .	Выбор режима . . . . . . . . . . . . . . . . . . . .	. .	. 54. . . . . . . . . . .
	ПРЕДУПРЕЖДЕНИЕ О НАБОРЕ ВЫСОТЫ . . . . . . . . .	30. . . .		Статус ответов . . . . . . . . . . . . . . . . . . . .	. .	. 55. . . . . . . . . . .
	МЕТРИЧЕСКИЙ ДИСПЛЕЙ . . . . . . . . . . . . . . . . .	31. . . . .	. . .	Выбор кода . . . . . . . . . . . . . . . . . . . . . .	. .	. 55. . . . . . . . . . . .
	ПРЕДУПРЕЖДЕНИЕ О НИЗКОЙ ВЫСОТЕ . . . . . . . . .	31. . . .		Идентификационный номер воздушного судна .	. .	.56. .

2.4ИНДИКАТОР ВЕРТИКАЛЬНОГО

	ОТКЛОНЕНИЯ/ГЛИССАДЫ/КРИВИЗНЫ ГЛИССАДЫ . .32	ГЛАВА 5: АУДИОПАНЕЛЬ . . . . . . . . . . . . . . . . .	57. . . . . . . .
2.5	ОПОВЕЩЕНИЯ МАРКЕРНОГО МАЯКА . . . . . . . . .	33. . . . .	5.1	ВЫБОР РАДИО СОМ . . . . . . . . . . . . . . . . . . .	.58. . . . . . . . .
2.6	ИНДИКАТОР ВЕРТИКАЛЬНОЙ СКОРОСТИ . . . . . . .	33. . . .	5.2	ГРОМКОГОВОРИТЕЛЬ В КАБИНЕ . . . . . . . . . . . .	58. . . . . .
2.7	МИНИМУМЫ БАРОМЕТРИЧЕСКОЙ ВЫСОТЫ .. .. .. .. .. .. ..	..33	5.3	СИСТЕМА ОПОВЕЩЕНИЯ ПАССАЖИРОВ (РА),
2.8	НАВИГАЦИОННЫЙ ПЛАНОВЫЙ ПРИБОР (НПП) . . .	.34. .		ТОЛЬКО ДЛЯ (Т)182Т И (Т)206Н . . . . . . . . . . . . .	58. . . . . .
	ИНДИКАТОР СКОРОСТИ РАЗВОРОТА И ВЕКТОР		5.4	ПРИЕМНИК МАРКЁРНОГО МАЯКА . . . . . . . . . . .	58. . . . . .
	ТРЕНДА ВЫДЕРЖИВАНИЯ КУРСА . . . . . . . . . . . . .	35. . . .	. .	Чувствительность к сигналу маркёрного маяка . . . .	.58. .
	УКАЗАТЕЛЬ КУРСА . . . . . . . . . . . . . . . . . . . . .	35. . . .	5.5. . .	ВЫБОР. . АУДИО NAV RADIO . . . . . . . . . . . . . . . .	59. . . . . . . .
	ИНДИКАТОР ОТКЛОНЕНИЯ ОТ КУРСА (CDI) . . . . . . .	35. . . .	5.6	СИСТЕМА ВНУТРЕННЕЙ СВЯЗИ (ICS)
	УКАЗАТЕЛИ ПЕЛЕНГА И ИНФОРМАЦИОННЫЕ ОКНА . .	37. .		И ЕЕ ИЗОЛЯЦИЯ . . . . . . . . . . . . . . . . . . . . . .	59. . . . . . . . . .
	DME – ДАЛЬНОМЕРНОЕ ОБОРУДОВАНИЕ (ОПЦИЯ) . .	37. .	5.7	РЕГУЛИРОВКА ГРОМКОСТИ СИСТЕМЫ
	ИСТОЧНИК ИНФОРМАЦИИ ПО НАВИГАЦИИ . . . . . . .	37. . .		ВНУТРЕННЕЙ СВЯЗИ . . . . . . . . . . . . . . . . . . . .	60. . . . . . . . .
Garmin G1000: Справочное руководство для Cessna Nav III					9

Данный перевод не является официальным и может использоваться только для справки				IDEPENDENT

					REPRESENTATIVE

ГЛАВА 1 – ОБЗОР СИСТЕМЫ

5.8	ПРОИГРЫВАТЕЛЬ И РЕГИСТРАТОР ЦИФРОВОГО		7.8	ИНФОРМАЦИОННАЯ СТРАНИЦА
	КЛИРЕНСА . . . . . . . . . . . . . . . . . . . . . . . .	. 60. . .	. . . .	. ПОЛЬЗОВАТЕЛЬСКИХ. . . . ТОЧЕК МАРШРУТА . . . . .	.	. 121. . . .
				7.9	БЛИЖАЙШИЕ АЭРОПОРТЫ . . . . . . . . . . . . .	.	. .121. . . . . . .
ГЛАВА 6: АТОМАТИЧЕСКАЯ БОРТОВАЯ			Информация о ближайших аэропортах
СИСТЕМА УПРАВЛЕНИЯ (AFCS) . . . . . . . . . . .	. 61. . .	. . .	на экране MFD	. .	. . . . . . . . . . . . . . . . . . .	.	. 121. . . . . . . . . . .
6.1	ИНСТРУМЕНТЫ УПРАВЛЕНИЯ АБСУ . . . . . . . . .	. .61. . .	. .	Информация о ближайших аэропортах
6.2	РАБОТА ПИЛОТАЖНОГО КОМАНДНОГО ПРИБОРА	. .62.		на экране PFD	. . .	. . . . . . . . . . . . . . . . . . .	.	.122. . . . . . . . . . .
	Запуск пилотажного командного прибора . . . . . .	. 62. . .	7.10.	БЛИЖАЙШИЕ ПЕРЕСЕЧЕНИЯ . . . . . . . . . . . . .	.	.122. . . . . . .
	Командные стрелки . . . . . . . . . . . . . . . . . . .	. 62. . .	7.11. . . .	.БЛИЖАЙШАЯ.	ОПРС (NDB) . . . . . . . . . . . . . .	.	. 123. . . . . . . .
	Окно состояния AFCS (АБСУ) . . . . . . . . . . . . .	. .63. . .	7 12. . .. .	БЛИЖАЙШИЙ ВОР (VOR) . . . . . . . . . . . . . . .	.	. 123. . . . . . . .
6.3	РЕЖИМЫ ПИЛОТАЖНОГО		7.13	БЛИЖАЙШАЯ ПОЛЬЗОВАТЕЛЬСКАЯ ТОЧКА
	КОМАНДНОГО ПРИБОРА . . . . . . . . . . . . . . . .	. 63. . .	. . . .	. МАРШРУТА .	.	. .	. . . . . . . . . . . . . . . . . . .	.	. 124. . . . . . . . . . . .
	Режимы тангажа . . . . . . . . . . . . . . . . . . . .	. .63. . .	7 14. .. . .	.БЛИЖАЙШИЕ. . ЧАСТОТЫ . . . . . . . . . . . . . . . .	.	.124. . . . . . . .
	Режимы вращения вокруг продольной оси . . . . .	. .77. . .	7.15	БЛИЖАЙШЕЕ ВОЗДУШНОЕ ПРОСТРАНСТВО . . . .	.	. 125. . .
6.4	РАБОТА АВТОПИЛОТА . . . . . . . . . . . . . . . . . .	. 82. . .	. . . .	. .
	Управление полетом . . . . . . . . . . . . . . . . . . .	.82. . .	. ГЛАВА. . . 8:. ПЛАНИРОВАНИЕ ПОЛЕТА. . . . . . . . . . . . . .	.	.127. . . . . . .
	Включение автопилота .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. ..	..82	8.1	ОПРЕДЕЛЯЕМЫЕ ПОЛЬЗОВАТЕЛЕМ ТОЧКИ
	Совмещенной управление (CWS) . . . . . . . . . . .	. 83. . .	. . .	МАРШРУТА .	.	. .	. . . . . . . . . . . . . . . . . . .	.	. 127. . . . . . . . . . . .
	Отключение автопилота . . . . . . . . . . . . . . . . .	.83. . .	. . . .	.Выбор информационной страницы пользователь
6.5	ПРИМЕРЫ ПОСЛЕДОВАТЕЛЬНОСТИ ДЕЙСТВИЙ . . .	.84. .		ских точек маршрута . . . . . . . . . . . . . . . . . .	.	.127. . . . . . . . .
	ВЫЛЕТ .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. ..	..85		СОЗДАНИЕ ТОЧКИ МАРШРУТА НА СТРАНИЦЕ
	Перехват радиала VOR . . . . . . . . . . . . . . . . .	. 86. . .	. . . . .	НАВИГАЦИОННОЙ.	КАРТЫ . . . . . . . . . . . . . .	.	. 128. . . . . . . .
	Полет в соответствии с курсом плана полета/GPS . .	87. .	8.2	ВИЗУАЛЬНОЕ ОТОБРАЖЕНИЕ АКТИВНОГО
	Снижение . . . . . . . . . . . . . . . . . . . . . . . . .	.88. . .	. . . .	. ПЛАНА. . . . ПОЛЕТА .	. . . . . . . . . . . . . . . . . . .	.	. 128. . . . . . . . . . .
	Заход на посадку . . . . . . . . . . . . . . . . . . . . .	.91. . .	8 3. . .. .	.АКТИВАЦИЯ. . СОХРАНЕННОГО ПЛАНА ПОЛЕТА . .	.	. .128. .
	Уход на второй круг . . . . . . . . . . . . . . . . . . .	. 93. . .	8 4. . .. . .	.АКТИВАЦИЯ.	УЧАСТКА ПОЛЕТА . . . . . . . . . . .	.	. 129. . . . . . .
6.6	ИНФОРМАЦИОННЫЕ СООБЩЕНИЯ		8.5	ПРЕКРАЩЕНИЕ НАВИГАЦИИ ПО ПЛАНУ ПОЛЕТА . .	.	.129. .
	И УВЕДОМЛЕНИЯ AFCS (АБСУ) . . . . . . . . . . . . .	94. . .	8 6.. . . .	ПРЕОБРАЗОВАНИЕ АКТИВНОГО ПЛАНА ПОЛЕТА .	.	. 129. .
	Сообщения о состоянии AFCS . . . . . . . . . . . . .	. 94. . .	8 7.. . ..	СОЗДАНИЕ НОВОГО ПЛАНА ПОЛЕТА . . . . . . . .	.	. 130. . . . .
	Защита от превышения скорости . . . . . . . . . . .	. 95. . .	. . .	Создание нового плана полета
					с помощью MFD .. .. ..	.. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. ..	.. ..	..130
ГЛАВА 7: НАВИГАЦИЯ . . . . . . . . . . . . . . . . . . .	.97. . .	. . . .	.Создание.	нового плана полета
7.1	СТРАНИЦА НАВИГАЦИОННОЙ КАРТЫ . . . . . . . .	. 97. . .	. .	с помощью PFD .	. . . . . . . . . . . . . . . . . . .	.	. 130. . . . . . . . . . .
7.2	НАВИГАЦИЯ DIRECT-TO (направление) . . . . . . . .	.97. . .	8.8.	ВНЕСЕНИЕ ВОЗДУШНОЙ ТРАССЫ
	Навигация Direct-to с дисплея MFD . . . . . . . . . .	. 97. . .	. . .	В ПЛАН ПОЛЕТА .	. . . . . . . . . . . . . . . . . . .	.	. 131. . . . . . . . . . .
	Навигация Direct-to c дисплея PFD . . . . . . . . . .	. 99. . .	8 9. . ..	ЗАГРУЗКА ВЫЛЕТА . . . . . . . . . . . . . . . . . .	.	. 132. . . . . . . . . .
7.3	ПРИМЕР НАВИГАЦИИ ПО ПЛАНУ ПОЛЕТА . . . . . .	. 101. . .	8.10.	ЗАГРУЗКА ПРИЛЕТА . . . . . . . . . . . . . . . . . .	.	.132. . . . . . . . .
7.4	ИНФОРМАЦИЯ ПО АЭРОПОРТУ . . . . . . . . . . . .	.117. . .	8 11. . ..	ЗАГРУЗКА ЗАХОДА НА ПОСАДКУ . . . . . . . . . .	.	. 132. . . . . .
7.5	ИНФОРМАЦИЯ ПО ПЕРЕСЕЧЕНИЯМ . . . . . . . . . .	.119. . .	8 12. . .	УДАЛЕНИЕ ВЫЛЕТА, ПРИЛЕТА, ЗАХОДА
7.6	ИНФОРМАЦИЯ ПО ОПРС (NDB) . . . . . . . . . . . . .	120. . .	. . . .	НА ПОСАДКУ ИЛИ ВОЗДУШНОЙ ТРАССЫ
7.7	ИНФОРМАЦИЯ ПО ВОР (VOR) . . . . . . . . . . . . .	. 120. . .	. . . .	ИЗ ПЛАНА ПОЛЕТА	. . . . . . . . . . . . . . . . . .	.	. 132. . . . . . . . . .
10					Garmin G1000: Справочное руководство для Cessna Nav III

IDEPENDENT				Данный перевод не является официальным и может использоваться только для справки

	REPRESENTATIVE

ГЛАВА 1 – ОБЗОР СИСТЕМЫ

8.13	СОХРАНИЕНИЕ ПЛАНА ПОЛЕТА . . . . . . . . . . . . .	132. . . . .	. .	Консультативная информация о воздушном
8.14	РЕДАКТИРОВАНИЕ СОХРАНЕННОГО			движении (TAS) (Опция) . . . . . . . . . . . . . . . . .	.148. . . . . . . .
	ПЛАНА ПОЛЕТА . . . . . . . . . . . . . . . . . . . . . .	133. . . . .	. . .	.Воздушное. . движение ADS-B (опция) . . . . . . . . .	. 149. . . . .
8.15	УДАЛЕНИЕ ТОЧКИ МАРШРУТА ИЗ ПЛАНА ПОЛЕТА . .	133. .	10.5	СБЛИЖЕНИЕ С ЗЕМЛЕЙ И ПРЕПЯТСТВИЯМИ . . . .	. 150. . .
8.16	ПРЕОБРАЗОВАНИЕ И АКТИВАЦИЯ			Отображение земли и препятствий на странице
	СОХРАНЕННОГО ПЛАНА ПОЛЕТА . . . . . . . . . . . . .	133. . . .	. .	сближения с землей . . . . . . . . . . . . . . . . . . .	.150. . . . . . . . .
8.17	КОПИРОВАНИЕ ПЛАНА ПОЛЕТА . . . . . . . . . . . . .	133. . . .	. .	Отображение земной поверхности
8.18	УДАЛЕНИЕ ПЛАНА ПОЛЕТА . . . . . . . . . . . . . . .	.134. . . .	. . .	и препятствий на навигационной карте . . . . . . . .	.150. . . .
8.19	СОЗДАНИЕ ГРАФИЧЕСКОГО ПЛАНА ПОЛЕТА . . . . . .	134. . .	10.6	СИСТЕМА РАННЕГО ПРЕДУПРЕЖДЕНИЯ
8.20	ПЛАНИРОВАНИЕ ПОЛЕТА . . . . . . . . . . . . . . . . .	134. . . .	. . . .	ПРИБЛИЖЕНИЯ К ЗЕМЛЕ (TAWS) – ОПЦИЯ . . . . .	. 151. . .
				Отображение Земли на странице TAWS . . . . . . . .	.151. . . .
ГЛАВА 9: ПРОЦЕДУРЫ . . . . . . . . . . . . . . . . . .	137. . . . .	. . .	Показать.	/Скрыть авиационную информацию . . . .	. 151. . .
9.1	ПРОЦЕДУРЫ ПО ВЫЛЕТУ И ПРИЛЕТУ . . . . . . . . .	137. . . . .		Запрет TAWS	. . . . . . .		. . . . . . . . . . . . . . . . .	151. . . . . . . . . . . .
	Загрузка и активация процедур по вылету . . . . . . .	137. . .		Ручная проверка системы . . . . . . . . . . . . . . .	. 153. . . . . . . .
	Загрузка и активация процедур по прилету . . . . . .	137. . .		Система предупреждения столкновения
9.2	ПРОЦЕДУРЫ ЗАХОДА НА ПОСАДКУ . . . . . . . . . . .	138. . . .	.	с наземными препятствиями
				переднего обзора (FLTA) . . . . . . . . . . . . . . . . .	.153. . . . . . . .
ГЛАВА 10: ПРЕДУПРЕЖДЕНИЕ			Оповещение о преждевременном
ОПАСНЫХ СИТУАЦИЙ . . . . . . . . . . . . . . . . . . .	141. . . .	. . . .	снижении.	(PDA) . . . . . . . . . . . . . . . . . . . . . .	153. . . . . . . . . . .
10.1	ПОЛЬЗОВАТЕЛЬСКАЯ НАСТРОЙКА ЭКРАНОВ,			Система оповещения
	Отображающих опасные ситуации,			о превышении скорости снижения (EDR) . . . . . . .	. 154. . . .
	на навигационной карте . . . . . . . . . . . . . . . . . .	141. . . .	. . . .	Система оповещения об отрицательной
10.2	STORMSCOPE® (ОПЦИЯ) . . . . . . . . . . . . . . . . .	141. . . .	. . . .	скорости набора высоты (NCR) . . . . . . . . . . . . .	154. . . . . . .
	Отображение информации по грозовой			Звуковое предупреждение ‘Five-Hundred’
	активности stormscope на странице			(пятьсот)		. . .	. . . . . .		. . . . . . . . . . . . . . . . .	.154. . . . . . . . . . . .
	навигационной карты . . . . . . . . . . . . . . . . . . .	141. . . .	. . . .	Отображение.	земной поверхности
	Страница Stormscope . . . . . . . . . . . . . . . . . . .	142. . . .	. . . .	и. препятствий на навигационной карте . . . . . . . .	.154. . . .
10.3	XM WEATHER – ОПЦИЯ (ПОГОДА XM) . . . . . . . . . .	143. . . .	.	Всплывающие окна предупреждающих
	Отображение информации METAR и TAF			сообщений .	. . . . . .	.	. . . . . . . . . . . . . . . .	. 155. . . . . . . . . . . .
	на странице информации по аэропортам . . . . . . .	143. . . .		Резюме предупреждающих сообщений
	Отображение метеорологической			системы TAWS . . . . . . . . . . . . . . . . . . . . . . .	.156. . . . . . . . . . .
	информации на странице weather data link . . . . . . .	144. . .		Предупреждающие сообщения . . . . . . . . . . . . .	158. . . . . . .
	Панорамирование карты –
	Страница Weather Data Link . . . . . . . . . . . . . . . .	145. . . .	ГЛАВА. . . 11: НЕИСПРАВНАЯ РАБОТА . . . . . . . . . .	.159. . . . .
	Опции и символы метеорологической информации . .	145	11.1	РЕВЕРСИВНЫЙ РЕЖИМ . . . . . . . . . . . . . . . . .	.159. . . . . . . .
	Время, в течение которого информация		11.2	НЕИСПРАВНАЯ РАБОТА COM . . . . . . . . . . . . . .	.160. . . . . . .
	остается актуальной . . . . . . . . . . . . . . . . . . . .	146. . . .	11 3. . . .	НЕОБЫЧНЫЕ.	ЗАХОДЫ НА ПОСАДКУ . . . . . . . . .	. 160. . . . .
10.4	СИСТЕМЫ ИНФОРМИРОВАНИЯ		11.4	РАБОТА ПРИБОРА STORMSCOPE ПРИ ПОТЕРЕ КУРСА . 160
	О ВОЗДУШНОМ ДВИЖЕНИИ . . . . . . . . . . . . . . .	146. . . .	11 5.. ..	ПРЕДУПРЕЖДЕНИЯ ОБ ОПАСНОСТИ
	Сервис информирования			ПРИ ПОТЕРЕ ПОЛОЖЕНИЯ GPS . . . . . . . . . . . .	.160. . . . . .
	о воздушном движении (TIS) . . . . . . . . . . . . . . .	146. . . .	11 6.. ..	СЧИСЛЕНИЕ ПУТИ (DR) . . . . . . . . . . . . . . . . . .	161. . . . . . . . .
Garmin G1000: Справочное руководство для Cessna Nav III									11

Данный перевод не является официальным и может использоваться только для справки								IDEPENDENT

									REPRESENTATIVE

Соседние файлы в папке G1000

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18.04.201510.82 Mб74G1000_CessnaNavIII_PilotsGuide_SystemSoftwareVersion0563.00orlater_.pdf
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Источник

инструкцияGarmin G1000

G1000

Integrated Flight Deck

Pilot’s Guide

Daher TBM 850/900

System Software Version 0719.16 or later

Руководство пользователя

768 страниц(ы)

Инструкция по установке

99 страниц(ы)

Посмотреть инструкция для Garmin G1000 бесплатно. Руководство относится к категории без категории, 6 человек(а) дали ему среднюю оценку 9.3. Руководство доступно на следующих языках: английский. У вас есть вопрос о Garmin G1000 или вам нужна помощь? Задайте свой вопрос здесь

Section 1 System Overview
Section 2 Flight Instruments
Section 3 Engine and Airframe Systems
Section 4 Audio Panel and CNS
Section 5 Flight Management
Section 6 Hazard Avoidance
Section 7 Automatic Flight Control System
Section 8 Additional Features
Appendices
Index

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Источник

G1000® Integrated Flight Deck

Pilot’s Guide

Cessna Nav III

SYSTEM OVERVIEW

FLIGHT INSTRUMENTS

EIS

AUDIO PANEL & CNS

FLIGHT MANAGEMENT

HAZARD AVOIDANCE

AFCS

ADDITIONAL FEATURES

APPENDICES

INDEX

This manual reflects the operation of System Software version 0563.25 or later for Cessna 172R, 172S, 182T, T182T, 206H, and T206H aircraft. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.

NOTE: Cessna Nav III aircraft include the Cessna 172R, the Cessna 172S, the normally aspirated Cessna 182 (182), the turbocharged Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206 (T206). Unless otherwise indicated, information in the G1000 Cockpit Reference Guide pertains to all Cessna Nav III aircraft.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200	Fax: 913/397.8282
Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.
Tel: 503/391.3411	Fax 503/364.2138
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Tel: 44/0870.8501241	Fax: 44/0870.8501251
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Tel: 886/02.2642.9199	Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836.

Web Site Address: www.garmin.com

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.

Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

NavData® is a registered trademark of Jeppesen, Inc.; Stormscope® is a registered trademark of L-3 Communications; and XM® is a registered trademark of XM Satellite Radio, Inc.; Honeywell® and Bendix/King® are registered trademarks of Honeywell International, Inc.; CO Guardian is a trademark of CO Guardian, Inc.

October, 2011

190-00498-07 Rev. A

Printed in the U.S.A.

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

LIMITED WARRANTY

Within the warranty period, Garmin will, at its sole discretion, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and/or labor incidental to the direct repair of said product. Garmin may, at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any country.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply in every case.

Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating the nearest Service Center, call Garmin Customer Service at one of the numbers listed below.

Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction confirmations are not accepted for warranty verification.To obtain warranty service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace missing components from any package purchased through an online auction.

Garmin International Inc.		Garmin (Europe) Ltd.
1200 East 151st Street, Olathe, Kansas 66062	Liberty House, Bulls Copse Road, Southampton, SO40
Telephone:	(913)397-8200	9RB, UK
Telephone Toll Free:	(888)606-5482	Telephone:	++44 (0)	870-8501243
Facsimile:	(913)397-8282	Telephone Toll Free:	++44 (0)	0808 238 0000
Facsimile Toll Free:	(800)801-4670	(option 5)
E-mail: orders@garmin.com	Facsimile:	++44 (0)	238052004
avionics@garmin.com	E-mail: avionics.europe@garmin.com
warranty@garmin.com

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

WARNINGS, CAUTIONS, AND NOTES

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness.

WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic.

WARNING: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000 MFD, is to be used only for weather avoidance, not penetration.

WARNING: Do not use datalink weather products (e.g., XM WX Satellite Weather, GFDS World Wide Weather, or FIS-B) for hazardous weather penetration. Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear.

WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance.

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

WARNINGS, CAUTIONS, AND NOTES

WARNING: For safety reasons, G1000 operational procedures must be learned on the ground.

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. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.

WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic 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. 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.”

WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand).

WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed.

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Garmin G1000 Pilot’s Guide for Cessna Nav III

iii

WARNINGS, CAUTIONS, AND NOTES

CAUTION: The 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.

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: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition.

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 and aviation databases. 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: The GDU 1040 PFD/MFD may require a warm-up time of up to 30 minutes when exposed to -40˚C for an extended period. A warm-up time of up to 15 minutes may be required when exposed to -30˚C for an extended period.

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.

NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank.

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

REVISION INFORMATION

Record of Revisions

Part Number	Revision	Date	Page Range	Description
190-00498-00	A	10/27/05	i — I-4	Reformatted for single part number (all previous part numbers
				incorporated into this part number)
				Added TAWS-B
				Added CO Guardian
				Added new fuel totalizer
190-00498-01	A	9/11/06	i — I-6	Added GFC 700 AFCS
				Added WAAS and VNAV
				Added Chartview, Flitecharts, and SafeTaxi
				Added GDU 7.00 parameters
				Change manual to larger format

190-00498-02	A	3/8/07	i — I-6	Added Airways
				Added ADS-B
				Added GDU 8.02 parameters
				Various clerical changes
190-00498-03	A	11/6/07	i — I-6	Added GDU 8.20 parameters, including gradient background on
				the PFD and GFC 700 for the C172.
190-00498-04	A	9/26/08	All	Added GDU 9.03 parameters
				Removed gradient background.
				Added Synthetic Vision System
190-00498-05	A	8/14/09	All	Added GDU 9.14
				Added new page navigation
				Added flight plan import/export
				Added new EIS displays
				Added CDI use in Dead Reckoning Mode
				Various clerical changes
190-00498-06	A	1/10	All	Added GDU 10.01
				Added Auxiliary Video
				Added AOPA Airport Directory
				Added Flight Data Logging
	B	4/10	484	Removed statement regarding certain SD cards voiding the
				G1000 warranty.
190-00498-07	A	10/11	All	Added Profile View
				Added FIS-B Weather
				Added Arrival Alert
				Added GTS 800 Traffic System
				Updated database synchronization
				Added GDU 12.02 parameters

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

REVISION INFORMATION

Blank Page

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

TABLE OF CONTENTS

	SECTION 1 SYSTEM OVERVIEW
1.1	System Description…………………………………………..	1
1.2	Line Replaceable Units (LRU)…………………………….	2
1.3	G1000 Controls………………………………………………..	7
	PFD/MFD Controls…………………………………………………	7
	Audio Panel Controls……………………………………………	10
1.4	Secure Digital (SD) Cards………………………………..	12
1.5	System Power-up……………………………………………	13
1.6	System Operation…………………………………………..	14
	Normal Display Operation……………………………………..	14
	Reversionary Display Operation………………………………	14
	AHRS Operation………………………………………………….	15
	G1000 System Annunciations…………………………………	17
	Softkey Function…………………………………………………	17
	GPS Receiver Operation………………………………………..	25
1.7	Accessing G1000 Functionality……………………….	29
	Menus………………………………………………………………	29
	MFD Page Groups……………………………………………….	30
	MFD System Pages………………………………………………	34
1.8	Display Backlighting……………………………………….	44
	Automatic Adjustment………………………………………….	44
	Manual Adjustment……………………………………………..	44
	SECTION 2 FLIGHT INSTRUMENTS
2.1	Flight Instruments…………………………………………..	50
	Airspeed Indicator……………………………………………….	50
	Attitude Indicator………………………………………………..	52
	Altimeter…………………………………………………………..	53
	Vertical Speed Indicator (VSI)…………………………………	55
	Horizontal Situation Indicator (HSI)………………………….	57
	Course Deviation Indicator (CDI)……………………………..	62
2.2	Supplemental Flight Data……………………………….	69
	Outside Air Temperature………………………………………..	69
	Wind Data…………………………………………………………	71
	Vertical Navigation (VNV) Indications……………………….	72
2.3	PFD Annunciations and Alerting Functions………	73
	System Alerting…………………………………………………..	73
	Marker Beacon Annunciations………………………………..	74
	Traffic Annunciation……………………………………………..	74
	TAWS Annunciations……………………………………………	75
	Altitude Alerting………………………………………………….	76
	Low Altitude Annunciation…………………………………….	76
	Minimum Descent Altitude/Decision Height Alerting…….	77

2.4	Abnormal Operations……………………………………..	78
	Abnormal GPS Conditions……………………………………..	78
	Unusual Attitudes………………………………………………..	79
	SECTION 3 ENGINE INDICATION SYSTEM (EIS)
3.1	Engine Display………………………………………………..	83
	Normally-Aspirated and Turbocharged Aircraft……………	83
3.2	Lean Display…………………………………………………..	86
	Normally-Aspirated Aircraft……………………………………	88
	Turbocharged Aircraft…………………………………………..	89
3.3	System Display……………………………………………….	90
	Normally-Aspirated and Turbocharged Aircraft……………	90
	SECTION 4 AUDIO PANEL AND CNS
4.1	Overview………………………………………………………..	95
	MFD/PFD Controls and Frequency Display………………….	96
	Audio Panel Controls……………………………………………	98
4.2	COM Operation…………………………………………….	100
	COM Transceiver Selection and Activation………………..	100
	COM Transceiver Manual Tuning……………………………	101
	Quick-tuning and Activating 121.500 MHz……………….	102
	Auto-tuning the COM Frequency……………………………	103
	Frequency Spacing……………………………………………..	107
	Automatic Squelch…………………………………………….	108
	Volume…………………………………………………………..	108
4.3	NAV Operation……………………………………………..	109
	NAV Radio Selection and Activation……………………….	109
	NAV Receiver Manual Tuning………………………………..	110
	Auto-tuning a NAV Frequency from the MFD……………	112
	Marker Beacon Receiver……………………………………..	117
	DME Tuning……………………………………………………..	118
4.4	GTX 33 Mode S Transponder…………………………	119
	Transponder Controls………………………………………….	119
	Transponder Mode Selection………………………………..	120
	Entering a Transponder Code………………………………..	123
	IDENT Function…………………………………………………	124
4.5	Additional Audio Panel Functions………………….	125
	Power-up…………………………………………………………	125
	Mono/Stereo Headsets………………………………………..	125
	Speaker…………………………………………………………..	125
	Intercom………………………………………………………….	126
	Passenger Address (PA) System……………………………..	128
	Clearance Recorder and Player……………………………..	128
	Entertainment Inputs………………………………………….	129

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TABLE OF CONTENTS

4.6 Audio Panel Preflight Procedure……………………	130
4.7	Abnormal Operation……………………………………..	131
	Stuck Microphone……………………………………………..	131
	COM Tuning Failure……………………………………………	131
	Audio Panel Fail-safe Operation…………………………….	131
	Reversionary Mode…………………………………………….	131
	SECTION 5 FLIGHT MANAGEMENT
5.1	Introduction………………………………………………….	133
	Navigation Status Box………………………………………..	134
5.2	Using Map Displays………………………………………	136
	Map Orientation……………………………………………….	136
	Map Range………………………………………………………	138
	Map Panning……………………………………………………	140
	Measuring Bearing and Distance…………………………..	144
	Topography……………………………………………………..	145
	Map Symbols……………………………………………………	148
	Airways…………………………………………………………..	154
	Track Vector……………………………………………………..	156
	Wind Vector……………………………………………………..	157
	Nav Range Ring………………………………………………..	158
	Fuel Range Ring………………………………………………..	159
	Field of View (SVS)…………………………………………….	160
	Selected Altitude Intercept Arc………………………………	161
5.3	Waypoints…………………………………………………….	162
	Airports…………………………………………………………..	163
	Intersections…………………………………………………….	170
	NDBs……………………………………………………………..	172
	VORs……………………………………………………………..	174
	User Waypoints…………………………………………………	176
5.4	Airspaces………………………………………………………	182
5.5 Direct-to-Navigation ……………………………………	185
5.6	Flight Planning……………………………………………..	190
	Flight Plan Creation……………………………………………	191
	Adding Waypoints to an Existing Flight Plan…………….	196
	Adding Airways to a Flight Plan…………………………….	198
	Adding Procedures to a Stored Flight Plan……………….	201
	Flight Plan Storage…………………………………………….	207
	Flight Plan Editing……………………………………………..	210
	Along Track Offsets…………………………………………….	214
	Parallel Track…………………………………………………….	215
	Activating a Flight Plan Leg………………………………….	218

	Inverting a Flight Plan…………………………………………	219
	Flight Plan Views……………………………………………….	220
	Closest Point of FPL……………………………………………	222
5.7	Vertical Navigation……………………………………….	223
	Altitude Constraints…………………………………………..	225
5.8	Procedures……………………………………………………	229
	Departures……………………………………………………….	229
	Arrivals …………………………………………………………..	232
	Approaches …………………………………………………….	234
5.9	Trip Planning…………………………………………………	240
	Trip Planning…………………………………………………….	240
5.10	RAIM Prediction……………………………………………	244
5.11	Navigating a Flight Plan……………………………….	247
5.12	Abnormal Operation……………………………………..	275
	SECTION 6 HAZARD AVOIDANCE
6.1	XM WX Satellite Weather………………………………	278
	Activating Services…………………………………………….	278
	Using XM WX Satellite Weather Products………………..	279
6.2	GFDS Worldwide Weather……………………………..	312
	Registering the Iridium Satellite System…………………..	312
	Registering the system for Garmin Flight Data Services.313
	GFDS Weather Data Requests……………………………….	322
	Worldwide Weather Products……………………………….	326
	Abnormal Operations…………………………………………	342
6.3	FIS-B Weather……………………………………………….	344
	Using FIS-B Weather Products………………………………	344
6.4	WX-500 Stormscope……………………………………..	359
	Setting Up Stormscope on the Navigation Map…………	359
6.5	Terrain Proximity…………………………………………..	364
	Displaying Terrain Proximity Data…………………………..	364
6.6	Profile View Terrain……………………………………….	369
	Profile View Display……………………………………………	369
6.7	Terrain-SVS……………………………………………………	372
	Displaying Terrain-SVS Data…………………………………	373
	Terrain-SVS Page……………………………………………….	375
	Terrain-SVS Alerts………………………………………………	377
6.8	TAWS-B…………………………………………………………	381
	Displaying TAWS-B Data……………………………………..	382
	TAWS-B Page……………………………………………………	385
	TAWS-B Alerts…………………………………………………..	387
	System Status…………………………………………………..	392

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Garmin G1000 Pilot’s Guide for Cessna Nav III

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TABLE OF CONTENTS

6.9	Traffic Information Service (TIS)……………………	394
	Displaying TRAFFIC Data……………………………………..	395
	Traffic Map Page……………………………………………….	397
	TIS Alerts…………………………………………………………	398
	System Status…………………………………………………..	399
6.10	Garmin GTS 800 Traffic………………………………….	402
	Theory of operation……………………………………………	402
	TAS Alerts………………………………………………………..	405
	System Test………………………………………………………	406
	Operation………………………………………………………..	407
6.11	Honeywell KTA870 Traffic……………………………..	415
	TAS Symbology…………………………………………………	415
	Operation………………………………………………………..	416
	Altitude Display………………………………………………..	419
	Traffic Map Page Display Range…………………………….	419
	TAS Alerts………………………………………………………..	421
	System Status…………………………………………………..	422
6.12	ADS-B Traffic…………………………………………………	423
SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
7.1	AFCS Controls……………………………………………….	430
7.2	Flight Director Operation………………………………	432
	Activating the Flight Director………………………………..	432
	AFCS Status Box………………………………………………..	433
	Command Bars…………………………………………………	434
	Flight Director Modes…………………………………………	434
7.3	Vertical Modes……………………………………………..	435
	Pitch Hold Mode (PIT)…………………………………………	436
	Selected Altitude Capture Mode (ALTS)…………………..	437
	Altitude Hold Mode (ALT)…………………………………….	438
	Vertical Speed Mode (VS)…………………………………….	439
	Flight Level Change Mode (FLC)……………………………	440
	Vertical Navigation Modes (VPTH, ALTV)………………….	442
	Glidepath Mode (GP) (SBAS Only)………………………….	447
	Glideslope Mode (GS)…………………………………………	449
	Go Around Mode (GA)………………………………………..	450
7.4	Lateral Modes……………………………………………….	451
	Roll Hold Mode (ROL)…………………………………………	452
	Heading Select Mode (HDG)…………………………………	453
	Navigation Modes (GPS, VOR, LOC)………………………..	454
	Approach Modes (GPS, VAPP, LOC)…………………………	456
	Backcourse Mode (BC)………………………………………..	458

7.5	Autopilot Operation……………………………………..	459
	Engaging the Autopilot……………………………………….	459
	Control Wheel Steering……………………………………….	460
	Disengaging the Autopilot……………………………………	460
7.6	Example Procedures……………………………………..	461
	Departure………………………………………………………..	462
	Intercepting a VOR Radial……………………………………	464
	Flying a Flight Plan/GPS Course…………………………….	465
	Descent…………………………………………………………..	466
	Approach………………………………………………………..	470
	Go Around/Missed Approach………………………………..	474
7.7	AFCS Annunciations and Alerts……………………..	476
	AFCS Status Alerts……………………………………………..	476
	Overspeed Protection…………………………………………	477
	SECTION 8 ADDITIONAL FEATURES
8.1	Synthetic Vision System (SVS) (Optional)………	480
	SVS Operation…………………………………………………..	481
	SVS Features…………………………………………………….	483
	Field of View…………………………………………………….	491
8.2	SafeTaxi………………………………………………………..	493
	SafeTaxi Cycle Number and Revision………………………	496
8.3	ChartView (Optional)…………………………………….	499
	ChartView Softkeys……………………………………………	499
	Terminal Procedures Charts………………………………….	500
	Chart Options…………………………………………………..	508
	Day/Night View…………………………………………………	514
	ChartView Cycle Number and Expiration Date…………..	516
8.4	FliteCharts…………………………………………………….	519
	FliteCharts Softkeys……………………………………………	519
	Terminal Procedures Charts………………………………….	520
	Chart Options…………………………………………………..	527
	Day/Night View…………………………………………………	531
	FliteCharts Cycle Number and Expiration Date………….	533
8.5	AOPA Airport Directory…………………………………	536
	AOPA Database Cycle Number and Revision…………….	537
8.6	SiriusXM Satellite Radio (Service Optional)…..	539
	Activating SiriusXM Satellite Radio Services……………..	539
	Using SiriusXM Radio…………………………………………	540
	Automatic Audio Muting……………………………………..	544
8.7	Scheduler……………………………………………………..	545
8.8	Electronic Checklists……………………………………..	547

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TABLE OF CONTENTS

8.9	Flight Data Logging………………………………………	550
8.10	Auxiliary Video (Optional)……………………………..	552
	Video Setup……………………………………………………..	553
	Display Selection……………………………………………….	553
	Input Selection………………………………………………….	554
	Zoom/Range…………………………………………………….	554
8.11	Abnormal Operation……………………………………..	556
	SVS Troubleshooting…………………………………………..	556
	Reversionary Mode…………………………………………….	556
	Unusual Attitudes………………………………………………	557
	APPENDICES
Annunciations and Alerts……………………………………….	561
	Alert Level Definitions…………………………………………	562
	Nav III Aircraft Alerts………………………………………….	562
	CO Guardian Messages……………………………………….	563
	G1000 System Annunciations……………………………….	563
	Other G1000 Aural Alerts…………………………………….	566
	G1000 System Message Advisories………………………..	566
	Flight Plan Import/Export Messages……………………….	577
	AFCS Alerts………………………………………………………	578
	Terrain-SVS Alerts………………………………………………	579
	TAWS-B ALERTS………………………………………………..	580
	TAWS-B System Status Annunciations…………………….	581
Database Management………………………………………….	583
	Jeppesen Databases…………………………………………..	583
	Garmin Databases……………………………………………..	587
Glossary………………………………………………………………..	593
Frequently Asked Questions…………………………………..	599
General TIS Information…………………………………………	603
	Introduction……………………………………………………..	603
	TIS vs. TAS/TCAS………………………………………………..	603
	TIS Limitations………………………………………………….	603
Map Symbols…………………………………………………………	605
	INDEX
Index	……………………………………………………………………..	I-1

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section is designed to provide an overview of the G1000 Integrated Flight Deck as installed in Cessna Nav III aircraft, which include the Cessna 172R, 172S, the normally aspirated Cessna 182 (182), the turbocharged Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206 (T206).

The G1000 system is an integrated flight control system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The system consists of the following Line Replaceable Units (LRUs):

•GDU 1040/1044B Primary Flight Display (PFD)

•GDU 1040/1044B Multi Function Display (MFD)

•GIA 63/63W Integrated Avionics Unit (IAU)

•GDC 74A Air Data Computer (ADC)

•GEA 71 Engine/Airframe Unit

•GRS 77 Attitude and Heading Reference System (AHRS)

•GMU 44 Magnetometer

•GMA 1347 Audio System with Integrated Marker Beacon Receiver

•GTX 33 Mode S Transponder

•GDL 69A Satellite Data Link Receiver

•GTS 800 Traffic Avoidance System (optional)

•GDL 90 ADS-B/FIS-B Data Link Transceiver (optional)

•GSA 81 AFCS Servos

•GSM 85 Servo Gearboxs

A top-level G1000 system block diagram is shown in Figure 1-1. See Figure 1-2 for optional/additional equipment.

NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.

The GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD) and autopilot (AP) functions of the G1000 system.

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

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SYSTEM OVERVIEW

1.2 LINE REPLACEABLE UNITS (LRU)

•GDU 1040/1044B – The GDU 1044B features a 10.4-inch LCD display with 1024 x 768 resolution. The left display is configured as a PFD and the right display is configured as an MFD. Both GDU 1044Bs link and display all functions of the G1000 system during flight. The displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each display is also paired via an Ethernet connection with a GIA 63 or 63W Integrated Avionics Unit. Systems that do not use the GFC 700 Automatic Flight Control System use the GDU 1040, which employs the same features as the GDU 1044B without the controls for the Garmin GFC 700 Automatic Flight Control System (AFCS).

•GIA 63/63W (2) – Functions as the main communication hub, linking all LRUs with the PFD. Each GIA 63/63W contains a GPS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. The GIA 63W contains a GPS SBAS receiver. Each GIA is paired with a respective GDU 1040/1044B display through Ethernet. The GIAs are not paired together and do not communicate with each other directly.

•GDC 74A (1) – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates with the GIA 63/63W, GDU 1040/1044B, and GRS 77, using an ARINC 429 digital interface. The GDC 74A also interfaces directly with the GTP 59.

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	• GEA 71 (1) – Receives and processes signals from the engine and airframe sensors. This unit communicates	SYSTEM OVERVIEW

	with both GIA 63/63Ws using an RS-485 digital interface.

		FLIGHT INSTRUMENTS
	• GRS 77 (1) – Provides aircraft attitude and heading information via ARINC 429 to both the GDU 1040/1044B
	and the GIA 63/63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and	EIS
	interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data,

	and with both GIAs to obtain GPS information. AHRS modes of operation are discussed later in this document.
		PANEL AUDIO CNS &
	• GMU 44 (1) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft	FLIGHT MANAGEMENT

	magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77
	using an RS-485 digital interface.
	• GMA 1347 – The GMA 1347 Audio Panel integrates NAV/COM digital audio, intercom system and marker	HAZARD AVOIDANCE
	beacon controls. The GMA 1347 also controls manual display reversionary mode (red DISPLAY BACKUP
	button) and is installed between the MFD and the PFD. The GMA 1347 communicates with both GIA 63/
	63Ws using an RS-232 digital interface.	AFCS

		ADDITIONAL FEATURES
	• GTX 33 (1) – The GTX 33 is a solid-state, Mode-S transponder that provides Modes A, C and S operation. The	APPENDICES

	GTX 33 is controlled through the PFD and communicates with both GIA 63/63Ws through an RS-232 digital
	interface.
		INDEX

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•GDL 69A (1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates with the MFD via HSDB connection. A subscription to the SiriusXM Satellite Radio service is required to enable the GDL 69A capability.

•GTS 800 – The GTS 800 Traffic Advisory System (TAS) uses active interrogations of Mode S and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system.

•GDL 90 (1) – A digital data link transceiver designed to transmit, receive and decode ADS-B traffic information, as well as FIS-B weather information. It broadcasts aircraft position, velocity, projected track, altitude, and flight identification to other equipped aircraft in the vicinity, as well as to FAA ground stations. The GDL 90 receives FIS-B weather information which is displayed on the MFD as NEXRAD radar and METARs.

•GSA 81 (3), and GSM 85 (3) – The GSA 81 servos are used for the automatic control of roll, pitch, and pitch trim. These units interface with each GIA 63/63W.

The GSM 85 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the mechanical flight-control surface linkage.

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PFD			MFD
GDU 1040 or	GMA 1347	GDU 1040 or
GDU 1044B*	Audio Panel	GDU 1044B*
	Reversionary	Reversionary
	Control		Control

GDC 74A

Air Data

Computer

No. 1 GIA 63/63W	OAT	No. 2 GIA 63/63W
Integrated Avionics Unit	Airspeed	Integrated Avionics Unit
Altitude

System Inegration Processors	Vertical Speed	System Integration Processors
I/O Processors		I/O Processors
VHF COM		VHF COM
VHF NAV/LOC	GRS 77	VHF NAV/LOC
GPS/WAAS	GPS/WAAS
Glideslope	AHRS	Glideslope
GFC 700 Flight Director

(172S, 182, & 206)	Attitude
GPS Output	GPS Output
Rate of Turn

	Slip/Skid

GMU 44

Magnetometer

Heading

GTX 33

Transponder

GEA 71

Engine/Airframe

Unit

GSA 81	GSA 81	GSA 81
Pitch Servo	Pitch Trim	Roll Servo
Autopilot Calculations	Autopilot Calculations	Autopilot Calculations
(172S/TD,182 & 206)	(172S/TD,182 & 206)	(172S/TD,182 & 206)

Honeywell

KAP 140

Autopilot

GTS 800

TAS

GDL 90

Data Link

ADS-B Traffic Data

*The GDU 1040 is available in systems not using the GFC 700 Automatic Flight Control System.

The GDU 1044B is available in systems using the Garmin GFC 700 Automatic Flight Control System.

Figure 1-1 Basic G1000 System

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No. 1 GIA 63/63W	No. 2 GIA 63/63W
Integrated Avionics Unit	Integrated Avionics Unit	GDL 69/69A
System Integration Processors	System Integration Processors	Data Link
I/O Processors	I/O Processors
Weather Data
VHF COM	VHF COM
Digital Audio Entertainment
VHF NAV/LOC	VHF NAV/LOC

GPS	GPS
Glideslope	Glideslope
GFC 700 Flight Director

ELT	L3	Honeywell	Honeywell	CO Guardian	Honeywell
Stormscope
Emergency Locator	KR 87	KN 63	Carbon Monoxide	KTA 870
Lightning Strike and	Traffic Avoidance
Transmitter	ADF Receiver	DME	Detection
Thunderstorm Detection	System

Figure 1-2 Additional Equipment Options

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1.3 G1000 CONTROLS

NOTE: The Audio Panel (GMA 1347) and AFCS controls are described in the CNS & Audio Panel and AFCS sections respectively.

The G1000 system controls are located on the PFD and MFD bezels and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section.

FLIGHT SYSTEM INSTRUMENTS OVERVIEW

PFD/MFD CONTROLS

17
18	24		14
19	25	10
11	15

20	26	12	16

21	27
22	28	13
23	29
GFC 700 AFCS Only	Figure 1-3	PFD/MFD Controls

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PFD and MFD control functions are the same.

1NAV 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.

2NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies.

3Dual 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.

4Heading 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.

5Joystick – Changes the map range (distance top to bottom of map display) when rotated. Activates the map pointer when pressed.

6CRS/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.

7Dual 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.

8COM Frequency Transfer Key – Transfers 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.

9COM VOL/SQ Knob – Controls COM audio level. Audio volume level is shown in the field as a percentage. Pressing this knob turns the COM automatic squelch ON and OFF.

10Direct-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 pointer position).

11FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans.

12CLR 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).

13Dual FMS Knob – Press to turn the selection cursor ON/OFF.

Data Entry: With the cursor ON, turn to enter data in the highlighted field (large knob moves cursor location; small knob selects character for highlighted cursor location). When the cursor is turned ON while viewing the Active Flight Plan Page, the cursor is placed on the line below the Data Insertion Pointer see Figure 1-4. The pointer indicates data entered at the cursor will be inserted above the line selected.

Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view. With cursor ON, turn large knob to scroll through the list.

Page Selection: Turn knob on MFD to select the page to view (large knob selects a page group; small knob selects a specific page from the group)

14MENU 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.

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Data is Inserted Above the Cursor, Indicated by the Data Insertion Pointer

Figure 1-4 Data Insertion Pointer

15PROC 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.

16ENT 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.

17Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands (500m for metric), while the small knob selects the hundreds (50m for metric). Altitude Select is used by the Automatic Flight Control System in certain modes, in addition to the standard G1000 Altitude Alerter function.

The following are only available with the GFC 700 AFCS.

18AP Key – Engages/disengages the autopilot and flight director. Pressing the AP Key activates the flight director and engages the autopilot in the default pitch axis and roll axis modes. Pressing the AP Key again disengages the autopilot and deactivates the flight director.

19HDG Key – Selects/deselects Heading Select Mode.

20NAV Key – Selects/deselects Navigation Mode.

21APR Key – Selects/deselects Approach Mode.

22VS Key – Selects/deselects Vertical Speed Mode.

23 FLC Key – Selects/deselects Flight Level Change Mode.

24FD 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.

25ALT Key – Selects/deselects Altitude Hold Mode.

26VNV Key – Selects/deselects Vertical Navigation Mode.

27BC Key – Selects/deselects Back Course Mode.

2829 NOSE UP/NOSE DN Keys – Controls the active pitch reference for the Pitch Hold, Vertical Speed, and Flight Level Change modes.

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SYSTEM OVERVIEW

AUDIO PANEL CONTROLS

1	2
3	4
5	6
7	8
9	10
11	12
13	14
15	16
17
18	19
20	21
22	23
	24

Figure 1-5 Audio Panel Controls (GMA 1347)

NOTE: When a key is selected, a triangular annunciator above the key is illuminated.

1COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receiver audio can be added by pressing the COM2 Key.

2COM1 – When selected, audio from the #1 COM receiver can be heard.

3COM2 MIC – Selects the #2 transmitter for transmitting. COM2 is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM2 can be deselected by pressing the COM2 Key, or COM1 can be added by pressing the COM1 Key.

4COM2 – When selected, audio from the #2 COM receiver can be heard.

5COM3 MIC – Not used on Cessna Nav III aircraft.

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6	COM3 – Not used on Cessna Nav III aircraft.	SYSTEM OVERVIEW

7	COM 1/2 – Split COM is disabled on Cessna Nav III aircraft.
8	TEL – Not used on Cessna Nav III aircraft.
FLIGHT INSTRUMENTS
9	PA – Selects the Passenger Address system. The selected COM transmitter is deselected when the PA Key

is pressed. The Passenger Address system is disabled on the Cessna 172R/S.

10SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker.

11MKR/MUTE – Mutes the currently received marker beacon receiver audio. Unmutes when new marker beacon audio is received. Also, stops play of the clearance recorder.

12HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to normal.

13DME – Pressing turns DME audio on or off.

14NAV1 – When selected, audio from the #1 NAV receiver can be heard.

15ADF – Pressing turns on or off the audio from the ADF receiver.

16NAV2 – When selected, audio from the #2 NAV receiver can be heard.

17AUX – Not used on Cessna Nav III aircraft.

18MAN SQ – Press to enable manual squelch for the intercom. When active, press the PILOT Knob to illuminate ‘SQ’. Turn the PILOT/PASS Knobs to adjust squelch.

19PLAY – Press once to play the last recorded audio. Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. Press the MKR/MUTE Key to stop play.

20PILOT – Pressing selects the pilot intercom isolation. Press again to deselect pilot isolation.

21COPLT – Pressing selects the copilot intercom isolation. Press again to deselect copilot isolation.

22PILOT Knob – Press to switch between volume and squelch control as indicated by the ‘VOL’ or ‘SQ’ being illuminated. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment.

23PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment.

24Reversionary Mode Button – Pressing manually selects Reversionary Mode.

INDEX APPENDICES ADDITIONAL AFCS HAZARD FLIGHT PANEL AUDIO EIS FEATURES AVOIDANCE MANAGEMENT CNS &

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SYSTEM OVERVIEW

1.4 SECURE DIGITAL (SD) CARDS

NOTE: Ensure the G1000 System is powered off before inserting an SD card.

NOTE: Refer to Appendix B for instructions on loading database updates.

The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. SD cards are used for storing the various databases and system software updates. Each display bezel is equipped with two SD card slots. The top slot is used for importing and exporting flight plans, Flight Data Logging, and loading navigation database updates. The bottom slot of each display contains a Garmin Supplemental Data Card which is used for storing the various databases.

Not all SD cards are compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft manufacturer.

Installing an SD card:

1)Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel.

2)To eject the card, gently press on the SD card to release the spring latch.

SD Card Slots

INDEX APPENDICES

Figure 1-6 Display Bezel SD Card Slots

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1.5 SYSTEM POWER-UP

NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation.

NOTE: Refer to Appendix A for system-specific annunciations and alerts.

The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFD, MFD, and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation.

During system initialization, test annunciations are displayed, as shown in Figure 1-7. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel.

On the PFD, the AHRS begins to initialize and displays “AHRS ALIGN: Keep Wings Level”. The AHRS should display valid attitude and heading fields typically within the first minute of power-up. The AHRS can align itself both while taxiing and during level flight.

When the MFD powers up, the power-up screen (Figure 1-8) displays the following information:

• System version	• Obstacle database name and version
• Copyright	• Navigation database name, version, and effective dates
• Land database name and version	• Airport Directory name, version and effective dates
• Safe Taxi database information	• FliteCharts/ChartView database information
• Terrain database name and version

Current database information includes database type, cycle number, or valid operating dates. Review the listed information for currency (to ensure that no databases have expired).

Pressing the ENT Key (or right-most softkey) acknowledges this information, and the Navigation Map Page is displayed upon pressing the key a second time. When the system has acquired a sufficient number of satellites to determine a position, the aircraft’s current position is shown on the Navigation Map Page.

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Figure 1-7 PFD Initialization

Figure 1-8 MFD Power-Up Screen (172R shown)

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1.6 SYSTEM OPERATION

NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In reversionary mode, it can be adjusted from the remaining display.

The displays are connected together via a single Ethernet bus for high-speed communication. Each IAU is connected to a single display, as shown in Figure 1-1. This allows the units to share information, enabling true system integration.. This section discusses normal and reversionary G1000 display operation, as well as the various AHRS modes and G1000 System Annunciations.

NORMAL DISPLAY OPERATION

In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information).

The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section).

Both displays offer control for COM and NAV frequency selection.

Figure 1-9 Normal Mode

REVERSIONARY DISPLAY OPERATION

NOTE: The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Refer to Appendix A for further information regarding system-specific alerts.

In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In reversionary mode, all important flight information is presented on the remaining display in the same format as in normal operating mode.

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If a display fails, the appropriate IAU Ethernet interface to the display is cut off. Thus, the IAU can no longer communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is completely automated for all LRUs and no pilot action is required.

Figure 1-10 Reversionary Mode (Failed PFD)

If the system fails to detect a display problem, reversionary mode may be manually activated by pressing the Audio Panel’s red DISPLAY BACKUP button (refer to the Audio Panel and CNS Section for further details). Pressing this button again deactivates reversionary mode.

Pressing the DISPLAY BACKUP button activates/deactivates reversionary mode

Figure 1-11 DISPLAY BACKUP Button

AHRS OPERATION

NOTE: Refer to Appendix A for specific AHRS alert information.

NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy.

The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs.

Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts. Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments).

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GPS Data

	availab			unavailab
Magnetometer Data	Magnetometer Data
availab		unavailab	availab	unavailab
	Air Data	Air Data
	availab	unavailab	availab	una
	v
	ailab
	le
AHRS Normal	AHRS no-	AHRS no-Mag/	AHRS
Mag Mode	no-Air Mode	no-GPS
Operation	Attitude/Heading Invalid
Heading Invalid	Mode

Figure 1-12 AHRS Operation

GPS INPUT FAILURE

NOTE: In-flight initialization of AHRS, when operating without any valid source of GPS data and at true air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an extended period of time where valid AHRS outputs are unavailable.

Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed data are available and valid.

MAGNETOMETER FAILURE

If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the heading output on the PFD is flagged as invalid with a red ‘X’.

AIR DATA INPUT FAILURE

Failure of the air data input has no affect on the AHRS output while AHRS is receiving valid GPS information. Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information.

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G1000 SYSTEM ANNUNCIATIONS

NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Pilot’s Operating Handbook (POH) for additional information regarding pilot responses to these annunciations.

When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with the failed data (Figure 1-13 displays all possible flags and responsible LRUs). Upon G1000 power-up, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of power-up. If any window remains flagged, the G1000 system should be serviced by a Garminauthorized repair facility.

EIS FLIGHT SYSTEM INSTRUMENTS OVERVIEW

GIA 63/W

Integrated

Avionics Units

GDC 74A Air

Data Computer

Database

GEA 71 Engine

Mismatch in PFD

and MFD

Airframe Unit

GIA 63/W

GRS 77 AHRS

Integrated

Avionics Unit

GMU 44

Magnetometer

GIA 63/W Integrated

Avionics Units

GDC 74A Air

GTX 33 Transponder

Data Computer

GIA 63/W Integrated

Figure 1-13

G1000 System Failure Annunciations

Avionics Units

SOFTKEY FUNCTION

The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background.

Softkey

Softkey Names

Bezel-Mounted (Displayed)

Softkeys (Press)

Figure 1-14 Softkeys (Second-Level PFD Configuration)

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO&

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ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

SYSTEM OVERVIEW

PFD SOFTKEYS

The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected.

The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning (optional). Each softkey sublevel has a BACK Softkey which can be selected to return to the previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued).

INSET			Displays Inset Map in PFD lower left corner

	OFF		Removes Inset Map

	DCLTR (3)		Selects desired amount of map detail; cycles through declutter levels:
			DCLTR (No Declutter): All map features visible
			DCLTR-1: Declutters land data
			DCLTR-2: Declutters land and SUA data
			DCLTR-3: Removes everything except for the active flight plan
	WX LGND		Displays icon and age on the Inset Map for the selected weather products
			(optional)

	TRAFFIC		Cycles through traffic display options:
			TRFC-1: Traffic displayed on inset map
			TRFC-2: Traffic Map Page is displayed in the inset map window
	TOPO		Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation
			scale on Inset Map

	TERRAIN		Displays terrain information on Inset Map

	STRMSCP		Displays Stormscope® information on Inset Map
	NEXRAD		Displays NEXRAD weather and coverage information on Inset Map (optional)
	or
	PRECIP		Displays GFDS or FIS-B precipitation on Inset Map (optional)

	XM LTNG		Displays XM WX lightning information on Inset Map (optional)
	or		Displays GFDS Worldwide Weather lightning information on Inset Map

	DL LTNG		(optional)
	METAR		Displays METAR flags on airport symbols shown on the Inset Map
			(optional)
PFD			Displays second-level softkeys for additional PFD configurations

	SYN VIS		Displays the softkeys for enabling or disabling Synthetic Vision
			features
		PATHWAY	Displays rectangular boxes representing the horizontal and vertical
			flight path of the active flight plan
		SYN TERR	Enables synthetic terrain depiction

		HRZN HDG	Displays compass heading along the Zero-Pitch line

		APTSIGNS	Displays position markers for airports within approximately 15 nm of
			the current aircraft position. Airport identifiers are displayed when
			the airport is within approximately 9 nm.

	DFLTS		Resets PFD to default settings, including changing units to standard

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

			SYSTEM OVERVIEW

					SYSTEM OVERVIEW
	WIND	Displays softkeys to select wind data parameters


		OPTN 1	Wind direction arrows with headwind and crosswind components

		OPTN 2	Wind direction arrow and speed


		OPTN 3	Wind direction arrow with direction and speed		FLIGHT INSTRUMENTS

		OFF	Information not displayed


	DME	Displays the DME Information Window

	BRG1	Cycles the Bearing 1 Information Window through NAV1, GPS/ waypoint
			identifier and GPS-derived distance information, and ADF/frequency

	HSI FRMT	Provides access to the HSI formatting softkeys		EIS

		360 HSI	Displays the HSI in a 360 degree view


		ARC HSI	Displays the HSI as an arc
					PANELAUDIO CNS&
	BRG2	Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint

			identifier and GPS-derived distance information, and ADF/frequency.

	ALT UNIT	Displays softkeys for setting the altimeter and BARO settings to metric
			units
		METERS	When enabled, displays altimeter in meters		FLIGHT MANAGEMENT

		IN	Press to display the BARO setting as inches of mercury


		HPA	Press to display the BARO setting as hectopacals

	STD BARO	Sets barometric pressure to 29.92 in Hg (1013 hPa if METRIC Softkey is selected)

OBS			Selects OBS mode on the CDI when navigating by GPS (only available with		HAZARD AVOIDANCE
			active leg)


CDI			Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI

DME			Displays the DME Tuning Window, allowing selection of the DME

XPDR			Displays transponder mode selection softkeys

	STBY	Selects standby mode (transponder does not reply to any interrogations)		AFCS

	ON	Selects Mode A (transponder replies to interrogations)


	ALT	Selects Mode C – altitude reporting mode (transponder replies to identification
			and altitude interrogations)

	GND	Allows manual selection of ground mode in certain conditions		ADDITIONAL FEATURES

	VFR	Automatically enters the VFR code (1200 in the U.S.A. only)


	CODE	Displays transponder code selection softkeys 0-7

		0 — 7	Use numbers to enter code

	IDENT	Activates the Special Position Identification (SPI) pulse for 18 seconds,		APPENDICES
			identifying the transponder return on the ATC screen

	BKSP	Removes numbers entered, one at a time

IDENT			Activates the Special Position Identification (SPI) pulse for 18 seconds,
			identifying the transponder return on the ATC screen

TMR/REF			Displays Timer/References Window		INDEX

NRST			Displays Nearest Airports Window


ALERTS			Displays Alerts Window

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

SYSTEM OVERVIEW

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

Figure 1-15 Top Level PFD Softkeys

(optional)

DME

ALERTS

(optional)

PRECIP

DL LTNG

(optional)

WX LGND

STRMSCP

METAR

ALERTS

TRFC-1

Press the BACK or OFF Softkey

to return to the top-level softkeys.

TRFC-2

Figure 1-16 INSET Softkeys

SYN VIS

DME

HSI FRMT

ALT UNIT

ALERTS

BRG1(NAV1)

BRG2(NAV2)

Press the BACK Softkey

to return to the top-level softkeys

BRG1(GPS)

BRG2(GPS)

BRG1(ADF)	BRG2(ADF)
BRG1(OFF)	BRG2(OFF)
360 HSI	ARC HSI		ALERTS
			ALERTS
METERS	IN	HPA	ALERTS

PATHWAY SYN TERR HRZN HDG APTSIGNS ALERTS

Figure 1-17 PFD Configuration Softkeys

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

SYSTEM OVERVIEW

DME											ALERTS

ALERTS

Press the BACK Softkey to return to the top-level softkeys.

ALERTS

Press the BACK Softkey to return to the previous softkey level.

EIS FLIGHT SYSTEM INSTRUMENTS OVERVIEW

		Figure 1-18 XPDR (Transponder) Softkeys
MFD SOFTKEYS

ENGINE				Pressing this softkey makes available the LEAN
				and SYSTEM Softkeys

	LEAN			Pressing makes available the CYL SLCT and
				ASSIST Softkeys to facilitate engine leaning

		CYL SLCT		The Cylinder Select Softkey cycles through
				selection of each cylinder indicated by changing
				the cylinder display to light blue

		ASSIST		Pressing the ASSIST Softkey causes the first
				cylinder that peaks to become highlighted and
				information for that cylinder to be displayed

		BACK		Returns to the previous level softkeys

	SYSTEM			Press this softkey to make available the RST
				FUEL and GAL REM Softkeys

		RST FUEL		Pressing the Rest Fuel Softkey resets fuel used and
				gallons remaining to zero

		GAL REM		Press this softkey (Gallons Remaining) to display
				the quantity adjustment softkeys

			-10 GAL	Pressing decreases the fuel remaining quantity in
				10 gallon increments
			-1 GAL	Pressing decreases the fuel remaining quantity in
				1 gallon increments
			+1GAL	Pressing increases the fuel remaining quantity in
				1 gallon increments
			+10 GAL	Pressing decreases the fuel remaining quantity in
				10 gallon increments

			XX GAL	Pressing this softkey sets the fuel remaining to the
				quantity at the filler neck tab where XX is an
				airframe specific quantity
			XX GAL	Pressing this softkey sets the fuel remaining to
				the full tank quantity where XX as an airframe
				specific quantity

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO&

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Garmin G1000 Pilot’s Guide for Cessna Nav III

SYSTEM OVERVIEW

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

MAP		Enables second-level Navigation Map softkeys

	TRAFFIC	Displays traffic information on Navigation Map

	PROFILE	Displays/removes Profile View on Navigation
		Map Page

	TOPO	Displays topographical data (e.g., coastlines,
		terrain, rivers, lakes) and elevation scale on
		Navigation Map
	TERRAIN	Displays terrain information on Navigation Map

	AIRWAYS	Displays airways on the map; cycles
	(Default label	through the following:
	is dependant	AIRWAYS: No airways are displayed
	on map setup	AIRWY ON: All airways are displayed
	option selected)	AIRWY LO: Only low altitude airways
		are displayed
		AIRWY HI: Only high altitude airways
		are displayed

	STRMSCP	Pressing this softkey displays/removes Stormscope
		lightning data on the Navigation Map.
	NEXRAD	Displays NEXRAD weather and coverage
	or	information on the Navigation Map (optional)

	PRECIP	Displays GFDS or FIS-B precipitation on
		Navigation Map (optional)
	XM LTNG	Displays XM WX lightning information on
	or	the Navigation Map (optional)

	DL LTNG	Displays GFDS Worldwide Weather
		lightning information on the Navigation
		Map (optional)

	METAR	Displays METAR flags on airport symbols
		shown on the Navigation Map
	LEGEND	Displays the legend for the selected weather
		products. Available only when NEXRAD,
		XM LTNG, METAR and/or PROFILE
		softkeys are selected.
	BACK	Returns to top-level softkeys

DCLTR (3)		Selects desired amount of map detail; cycles
		through declutter levels:
		DCLTR (No Declutter): All map features visible
		DCLTR-1: Declutters land data
		DCLTR-2: Declutters land and SUA data
		DCLTR-3: Removes everything except for the
		active flight plan
SHW CHRT		Displays the appropriate chart

CHKLIST		Displays the Checklist Page

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

ENGINE

CHECK

EXIT

EMERGCY

SYSTEM OVERVIEW

Displays the engine checklist		SYSTEM OVERVIEW


Pressing this softkey checks off a checklist item.
If an item is already checked, an UNCHECK
Softkey is displayed.		FLIGHT INSTRUMENTS
Press to exit the checklist

Displays the emergency checklist
		EIS
		PANEL AUDIO CNS &
		FLIGHT MANAGEMENT
		HAZARD AVOIDANCE
		AFCS
		ADDITIONAL FEATURES
		APPENDICES
		INDEX

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

SYSTEM OVERVIEW

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

(All except Diesel)

ENGINE

MAP

DCLTR

SHW CHRT

CHKLIST

(optional)

DCLTR-1

DCLTR-2

DCLTR-3

(Default softkey

is dependant on

(optional)

the selection made

in the map setup

(optional)

PRECIP

DL LTNG

(optional) (optional)

options)

TRAFFIC

PROFILE

TOPO

TERRAIN

AIRWAYS STRMSCP

NEXRAD

XM LTNG

METAR

LEGEND

BACK

AIRWAYS

ENGINE

LEAN

SYSTEM

BACK

AIRWY ON

AIRWY LO

ENGINE

LEAN

SYSTEM

RST FUEL

GAL REM

BACK

AIRWY HI

Press the ENGINE or BACK Softkey to return to the default Engine Page level.

ENGINE		LEAN								BACK
		SYSTEM	CYL SLCT	ASSIST

Press the BACK Softkey to return Press the ENGINE Softkey to to the previous softkey level.

the default Engine Page level.

Press the BACK softkey to return to the top-level softkeys.

The CHECK Softkey changes to UNCHECK when the checklist item is already checked.

		CHECK		EXIT		EMERGCY
ENGINE

ENGINE

LEAN

SYSTEM

-10 GAL

-1 GAL

+1 GAL

+10 GAL

XX GAL

BACK

X = airframe specific values

(Diesel only)

ENGINE

Press the ENGINE or BACK Softkey to

return to the default Engine Page level.

ENGINE

SYSTEM

FUEL

BACK

Press the ENGINE or BACK Softkey to

return to the default Engine Page level.

ENGINE

SYSTEM

RST FUEL

BACK

FUEL

GAL REM

Press the ENGINE Softkey to return

Press the BACK Softkey to return

to the default Engine Page level.

to the previous softkey level.

ENGINE

SYSTEM

FUEL

-10 GAL

-1 GAL

+1 GAL

+10 GAL

44 GAL

BACK

Figure 1-19 MFD Softkeys

INDEX

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

SYSTEM OVERVIEW

GPS RECEIVER OPERATION

Each GIA 63/63W Integrated Avionics Unit (IAU) contains a GPS receiver. Information collected by the specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX — GPS Status Page.

These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other, or in SBAS (Satellite Based Augmentation System) capable systems, one of the GPS receivers has not yet acquired an SBAS signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal.

If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem.

Viewing GPS receiver status information

1)Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD page groups).

2)Use the small FMS Knob to select GPS Status Page.

Selecting the GPS receiver for which data may be reviewed

1)Use the FMS Knob to select the AUX — GPS Status Page.

2)To change the selected GPS receiver:

a)Press the desired GPS Softkey.

Or:

a)Press the MENU Key.

b)Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key.

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

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Garmin G1000 Pilot’s Guide for Cessna Nav III

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

SYSTEM OVERVIEW

Satellite Constellation	Satellite Signal	GPS Receiver
Diagram	Information Status	Status	RAIM

				Availability
				Prediction

Enabled

SBAS

Options

Satellite Signal

Strength Bars

RAIM Softkey
Selected	SBAS Softkey
	Selected

Figure 1-20 GPS Status Page (RAIM or SBAS Selected)

The GPS Status Page provides the following information:

• Satellite constellation diagram

Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead.

Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals.

• Satellite signal information status

The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement.

DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver.

The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements.

• GPS receiver status

Garmin G1000 Pilot’s Guide for Cessna Nav III

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SYSTEM OVERVIEW

The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution.

When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS indicates ACTIVE.

• RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is selected)

In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach.

Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time.

The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time.

Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The G1000 automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown.

Predicting RAIM availability

1)Select the GPS Status Page.

2)If necessary, press the RAIM Softkey.

3)Press the FMS Knob. The ‘WAYPOINT’ field is highlighted.

4)Turn the small FMS Knob to display the Waypoint Information Window.

5)Enter the desired waypoint:

a)Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer to Section 1.7 for instructions on entering alphanumeric data into the G1000.

Or:

a)Use the large FMS Knob to scroll to the Most Recent Waypoints List.

b)Use the small FMS Knob to highlight the desired waypoint in the list and press the ENT Key. The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint.

c)Press the ENT Key to accept the waypoint entry.

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

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Garmin G1000 Pilot’s Guide for Cessna Nav III

SYSTEM OVERVIEW

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

Or:

a)To use the present position, press the MENU Key.

b)With ‘Set WPT to Present Position’ highlighted, press the ENT Key.

c)Press the ENT Key to accept the waypoint entry.

6)Use the FMS Knob to enter an arrival time and press the ENT Key.

7)Use the FMS Knob to enter an arrival date and press the ENT Key.

With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed:

•‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination

•‘COMPUTING AVAILABILITY’—RAIM calculation in progress

•‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date

•‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date

• SBAS Selection (SBAS Softkey is pressed)(WAAS, EGNOS, or MSAS capable systems only)

In certain situations, such as when the aircraft is outside or on the fringe of the WAAS, EGNOS, or MSAS coverage area, it may be desirable to disable the reception of the applicable SBAS signal (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for the GPS Status box to be updated upon WAAS, EGNOS, and MSAS enabling/disabling.

Disabling WAAS, EGNOS or MSAS

1)Select the GPS Status Page.

2)If necessary, press the SBAS Softkey.

3)Press the FMS Knob, and turn the large FMS Knob to hightlight the desired SBAS system.

4)Press the ENT Key to uncheck the box.

5)Press the FMS Knob to remove the cursor.

•GPS Satellite Signal Strengths

The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for WAAS) below each bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance:

—No bar—Receiver is looking for the indicated satellite

—Hollow bar—Receiver has found the satellite and is collecting data

—Light blue bar—Receiver has collected the necessary data and the satellite signal can be used

—Green bar—Satellite is being used for the GPS solution

—Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion)

—“D” indication—Denotes the satellite is being used as part of the differential computations

Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid).

Garmin G1000 Pilot’s Guide for Cessna Nav III

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SYSTEM OVERVIEW

1.7 ACCESSING G1000 FUNCTIONALITY

MENUS

The G1000 has a MENU Key that, when pressed, displays a context-sensitive list of options. This options list allows the user to access additional features or make settings changes which specifically relate to the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to additional submenus that are used to view, edit, select, and review options. Menus display ‘NO OPTIONS’ when there are no options for the window/page selected. The main controls used in association with all window/page group operations are described in section 1.3. Softkey selection does not display menus or submenus.

Navigating the Page Menu Window:

1)Press the MENU Key to display the Page Menu Window.

2)Turn the FMS Knob to scroll through a list of available options (a scroll bar appears to the right of the window when the option list is longer than the window).

3)Press the ENT Key to select the desired option.

4)The CLR Key may be pressed to remove the menu and cancel the operation. Pressing the FMS Knob also removes the displayed menu.

No Options with

NRST Window

Displayed on the

PFD

Options with FPL Window Displayed

Figure 1-21 Page Menu Examples

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

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Garmin G1000 Pilot’s Guide for Cessna Nav III

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

SYSTEM OVERVIEW

MFD PAGE GROUPS

NOTE: Refer to the Flight Management, Hazard Avoidance, and Additional Features sections for details on specific pages.

Information on the MFD is presented on pages which are grouped according to function. The page group and active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom right corner of the screen, the page group tabs are displayed along the bottom Available pages in the group are displayed in a list above the page groups. The current page group and current page within the group are shown in cyan. For some of these pages (Airport/Procedures/Weather Information, XM WX Satellite Weather, Procedure Loading), the active title of the page changes while the page name in the list remains the same.

Page Group

Active Page Title

Pages in

Current

Group


MFD
Page	Groups

Figure 1-22 Page Title and Page Groups

Selecting a page using the FMS Knob:

1)Turn either FMS Knob one click to display the pop-up page selection window.

2)Turn the large FMS Knob until the desired page group is selected. For example, the MAP page group is selected in Figure 1-22.

3)Turn the small FMS Knob until the desired page is selected.

There are also several pages (Airport Information and XM Information pages) which are selected first from within a main page group with the FMS Knobs, then with the appropriate softkey at the bottom of the page. In this case, the page remains set to the selected screen until a different screen softkey is pressed.

Garmin G1000 Pilot’s Guide for Cessna Nav III

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SYSTEM OVERVIEW

Map Pages (MAP)

Navigation Map

Traffic Map

Stormscope®

Weather Data Link (service optional)

—XM WX Satellite Weather

—FIS-B Weather

—GFDS Worldwide Weather

Terrain Proximity/Terrain-SVS/

TAWS-B

Figure 1-23 Map Pages

Waypoint Pages (WPT)

Airport Information pages

—Airport Information (INFO-1 Softkey)

—Airport Directory (INFO-2 Softkey)

—Departure Information (DP Softkey)

—Arrival Information (STAR Softkey)

—Approach Information (APR Softkey)

—Weather Information (WX Softkey)

Intersection Information

NDB Information

VOR Information

User Waypoint Information

Figure 1-24 Waypoint Pages

Airport

Information

Pages

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

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Garmin G1000 Pilot’s Guide for Cessna Nav III

SYSTEM OVERVIEW

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

Auxiliary Pages (AUX)
Trip Planning
Utility
GPS Status
System Setup
SiriusXM Satellite pages
— XM Information
(INFO Softkey)			SiriusXM
— XM Radio			Satellite

		Pages

(RADIO Softkey)
System Status
Video (Optional)	Figure 1-25 Auxiliary Pages

Flight Plan Pages (FPL)

Active Flight Plan

—Wide View, Narrow View (VIEW Softkey)

Flight Plan Catalog or

Stored Flight Plan (NEW Softkey)

Figure 1-26 Flight Plan Pages

The Flight Plan Pages may also be accessed using the FPL Key. Main pages within this group are selected by turning the small FMS Knob.

The Checklist Page may be accessed from the page group tab or the CHKLIST Softkey. See the Additional Features section for a discussion on checklists.

Garmin G1000 Pilot’s Guide for Cessna Nav III

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SYSTEM OVERVIEW

Nearest Pages (NRST)

Nearest Airports

Nearest Intersections

Nearest NDB

Nearest VOR

Nearest User Waypoints

Nearest Frequencies

Nearest Airspaces

Figure 1-27 Nearest Pages

In addition to the main page groups accessed exclusively using the FMS Knobs, there are pages for flight planning (FPL) and loading procedures (PROC) which are accessed by bezel key. In some instances, softkeys may be used to access the Procedure Pages.

The Flight Plan Pages are accessed using the FPL Key on the MFD. Main pages within this group are selected by turning the small FMS Knob.

The Procedure pages may be accessed at any time on the MFD by pressing the PROC Key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading Page is opened. Turning the FMS Knob does not scroll through the Procedure pages (note the single page icon in the lower right corner).

Procedure Pages

(PROC)

Departure Loading

Arrival Loading

Approach Loading

Figure 1-28 Procedure Pages

For some of these pages (Airport Information pages, SiriusXM Satellite pages, Procedure pages), the title of the page may change while the page icon remains the same.

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

SYSTEM OVERVIEW

MFD SYSTEM PAGES

In the Auxiliary (AUX) Page Group, there are two system pages: System Setup and System Status. The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000 system LRUs.

SYSTEM SETUP PAGE

The System Setup Page allows management of the following system parameters:

•Time display format (local or UTC )

•Displayed measurement units

•Baro transition alert (see Flight Instruments

Section)

•Arrival Alerts

•Airspace alerts

•Audio alert voice

•Flightdirectorformat(onlythesinglequeoption is available in the Cessna Nav III)

•Page Navigation

•MFD Data Bar (Navigation Status Box) fields

•GPS Course Deviation Indicator (CDI) range

•COM transceiver channel spacing

•Displayed nearest airports

Selecting the System Setup Page:

1)Turn the large FMS Knob to select the AUX Page group.

2)Turn the small FMS Knob to display the System Setup Page.

Figure 1-29 System Setup Page

INDEX

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

SYSTEM OVERVIEW

Date/Time

The Date/Time Box on the System Setup Page displays the current date and time and allows the pilot to set the time format (local 12-hr, local 24-hr, or UTC) and offset. The time offset is used to define current local time. UTC (also called GMT or Zulu) date and time are calculated directly from the GPS satellites signals and cannot be changed. When using a local time format, designate the offset by adding or subtracting the desired number of hours.

Set the system time format:

1)While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.

2)Turn the large FMS Knob to highlight the time format field in the Date/Time Box.

3)Turn the small FMS Knob to select the desired system time format (local 12hr, local 24hr, UTC) and press the ENT Key.

Set the current time offset:

1)While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.

2)Turn the large FMS Knob to highlight the time offset field in the Date/Time Box.

3)Turn the FMS Knobs to enter the time offset and press the ENT Key.

Display Units

The Display Units Box on the System Setup Page allows configuration of the measurement units used for the following displayed data:

• Nav angle (magnetic, true)

When set to ‘MAGNETIC’, magnetic variation is figured into the displayed value. When ‘TRUE’ is selected, no magnetic variation is calculated and a ‘T’ is displayed next to the value.

Affects the BRG field in the PFD Navigation Status Box.

Affects Current Heading, Selected Heading, and Selected Course boxes on the PFD. Affects the BRG, DTK, TKE, TRK, and XTK fields in the MFD Navigation Status Box.

• Distance and speed (metric, nautical)

Affects the DIS field in the PFD Navigation Status Box and the range setting of the Inset Map.

Affects all distance and speed displays on the MFD with the exception of the displayed wind speed displayed on the Navigation Map Page. Wind speed is affected on the Trip Planning Page.

• Altitude and vertical speed (feet, meters)

Affects all altitude and elevation displays on the MFD, with the exception of VNAV altitudes on the Active Flight Plan Page.

• Temperature (Celsius, Fahrenheit)

Affects all temperature displays on the PFD.

Affects the temperature display on the Trip Planning Page. Does not affect the Engine Indicating System display.

INDEX APPENDICES ADDITIONALFEATURES AFCS AVOIDANCEHAZARD MANAGEMENTFLIGHT PANELCNSAUDIO& EIS INSTRUMENTSFLIGHT OVERVIEWSYSTEM

190-00498-07 Rev. A

Garmin G1000 Pilot’s Guide for Cessna Nav III

ADDITIONAL HAZARD FLIGHT AUDIO PANEL FLIGHT SYSTEM INDEX APPENDICES FEATURES AFCS AVOIDANCE MANAGEMENT & CNS EIS INSTRUMENTS OVERVIEW

SYSTEM OVERVIEW

• Fuel and fuel flow (gallons, gallons/hour)

Indicates fuel quantities are measured in gallons and fuel flow is measured in gallons per hour.

• Weight (pounds, kilograms)

The weight setting is not applicable to the Nav III.

• Position (HDDD°MM.MM’, HDDD°MM’SS.S”, MGRS)

Affects all position displays.

Change a Display Units setting:

1)While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.

2)Turn the large FMS Knob to highlight the desired field in the Display Units Box.

3)Turn the small FMS Knob to select from a list of measurement units and press the ENT Key when the desired unit is highlighted. Press the CLR Key to cancel the action without changing the units.

BARO Transition Alert

See the Flight Instruments section for a discussion on setting the Baro Transition Alert.

Airspace Alerts

The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the MFD Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace.

Alerts for the following airspaces can be turned on/off in the Airspace Alerts Box:

• Class B/TMA	• Restricted
• Class C/TCA	• MOA (Military)
• Class D	• Other airspaces

An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example, if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message is not generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot is notified with an alert message. The default setting for the altitude buffer is 200 feet.

Change the altitude buffer distance setting:

1)While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor.

2)Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box.

3)Turn the FMS Knobs to enter an altitude buffer value and press the ENT Key.

Garmin G1000 Pilot’s Guide for Cessna Nav III

190-00498-07 Rev. A

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Источник

Руководство полностью переведено на русский язык. Имеет оригинальные иллюстрации. Тем не менее, не является официальным переводом. Документ не может быть использован для летной эксплуатации.

Для получения последней версии документа отправьте запрос на E-mail sales@cessna-aircraft.ru.

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Здравствуйте! Подскажите пожалуйста есть ли видео уроки по G1000 на русском языке? если есть то скиньте плиз ссылку

− bogdan737,
8 лет назад,
#

Спасибо. Хоть и два года назат выложен здесь материал по данному прибору, а понадобился мне только сейчас. И это здорово!

− ivans71,
8 лет назад,
#

Хорошая штука G 1000.

А ктивно использую все ей качества во время полета.

Но вот в симе она не реализована а жаль.

− oops,
10 лет назад,
#

Наконец-то разберемся сэтим чудом техники! Огромное мерси!

− flyalex,
11 лет назад,
#

Большое спасибо!

− Karadag,
11 лет назад,
#

Источник

Quick Links

Related Manuals for Garmin G1000

Summary of Contents for Garmin G1000

Page 3: Copyright

Page 4: Table Of Contents

Page 5: Table Of Contents

Page 7: Introduction

Page 9: Ground Lesson 1

Page 10: Exercise 1.2: Component Review

Page 11: Ground Lesson 2

Page 12: Ground Lesson 3

Page 13: Ground Lesson 4

Page 14: Ground Lesson 5

Page 15: Exercise 5.2: Practice (Optional)

Page 16: Ground Lesson 6

Page 17: Exercise 6.3: Gps Navigation

Page 18: Exercise 6.5: Instrument Approaches

Page 19: Exercise 6.6: Practice (Optional)

Page 20: Ground Lesson 7

Page 22: Ground Lesson 8

Page 24: Ground Lesson 9

Page 25: Ground Lesson 10

Page 27: Ground Lesson 11

Page 29: Ground Lesson 12

Page 31: Procedure 1

Page 33: Procedure 2

Page 34: Procedure 3

Page 36: Procedure 4

Page 37: Flying The Dme Arc

Page 38: Procedure 5

Page 39: Procedure 6

Page 41: Procedure 7

Page 43: Procedure 8

Page 44: Procedure 9

Page 45: Flying A Course From Fix To Manual Sequence

Page 46: Procedure 10

Page 47: Flying The Ils Approach

Page 48: Procedure 11

Page 49: Flying The Vectors Approach

Page 50: Appendix

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G1000

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FLIGHT INSTRUMENTS

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

1.2 LINE REPLACEABLE UNITS (LRU)

1.3 G1000 CONTROLS

PFD/MFD CONTROLS

AUDIO PANEL CONTROLS

1.4 SECURE DIGITAL (SD) CARDS

1.5 SYSTEM POWER-UP

1.6 SYSTEM OPERATION

NORMAL DISPLAY OPERATION

REVERSIONARY DISPLAY OPERATION

AHRS OPERATION

G1000 SYSTEM ANNUNCIATIONS

SOFTKEY FUNCTION

GPS RECEIVER OPERATION

1.7 ACCESSING G1000 FUNCTIONALITY

MENUS

MFD PAGE GROUPS

MFD SYSTEM PAGES