Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang

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. 1200 East 151st Street, Olathe, Kansas 66062 Telephone: (913)397-8200 Telephone Toll Free: (888)606-5482 Facsimile: (913)397-8282 Facsimile Toll Free: (800)801-4670 E-mail: orders@garmin.com avionics@garmin.com warranty@garmin.com Garmin (Europe) Ltd. Liberty House, Bulls Copse Road, Southampton, SO40 9RB, UK Telephone: ++44 (0) 870-8501243 Telephone Toll Free: ++44 (0) 0808 238 0000 (option 5) Facsimile: ++44 (0) 238052004 E-mail: avionics.europe@garmin.com 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang i 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 the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the 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 Pilots using any outdated database do so entirely at their own risk.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: Do not use data link 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. WARNING: The Garmin G1000, as installed in the Cessna Citation Mustang 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 system. 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: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories (if installed), ATC guidance, or positive visual acquisition of conflicting traffic. WARNING: For safety reasons, system operational procedures must be learned on the ground. Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-04 Rev. A ii WARNINGS, CAUTIONS, AND NOTES 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 system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000 Pilot’s Guide documentation and the Cessna Citation Mustang Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the system 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 system to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/ aboutGarmin/environment/disposal.jsp. 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. 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 system 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. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang iii WARNINGS, CAUTIONS, AND NOTES NOTE: All visual depictions contained within this document, including screen images of the panel and displays, are subject to change and may not reflect the most current system and 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: 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: 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 : Use of polarized eyewear may cause the flight displays to appear dim or blank. Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-04 Rev. A iv WARNINGS, CAUTIONS, AND NOTES Blank Page 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang v REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190-00494-00 A B October, 2006 November, 2006 i through I-6 4-7, 4-16, 4-34 5-108 through 5-126 7-33 through 7-45 Production release Added ‘SQ’ and ‘RX’ annunciations. Added transponder code entry using the FMS Knob. Added flying an example flight plan to the GPS Navigation section. Udated AFCS examples to be consistent with the example flight plan in GPS Navigation section. 190-00494-01 A B February, 2007 May, 2007 i through I-6 i through I-6 Added GDU 8.00 parameters and made various corrections. Added KHF 1050 HF and KTA 870 TAS Reformatted GPS Navigation Section Corrected various clerical errors 190-00494-02 A B April, 2008 May, 2008 i through I-6 All Production Release Added Synthetic Vision System Added other GDU 9.01 parameters Corrected clerical error. 190-00494-03 A June, 2010 i through I-6 Added GDU 10.01 parameters Added GSD 41 Added GMA -20 Added new page navigation TCAS II Radar Altimeter Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Corrected various clerical errors 190-00494-04 A December, 2011 All Added Profile View Added Standby Navigation Database Added new database update procedures Updated system messages Added other GDU 12.03 parameters Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-04 Rev. A vi REVISION INFORMATION Blank Page 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang vii 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 Controls ................................................................ 7 Controls Associated With the MFD ................................. 9 AFCS Controls ............................................................ 11 Audio Panel Controls .................................................. 13 1.4 Secure Digital Cards.............................................. 15 1.5 System Power-up ................................................... 16 1.6 System Operation .................................................. 17 Normal Operation ....................................................... 17 Reversionary Mode ..................................................... 17 AHRS Operation ......................................................... 19 G1000 System Annunciations ...................................... 20 Softkey Function ......................................................... 21 GPS Receiver Operation .............................................. 29 1.7 Accessing G1000 Functionality............................ 34 Menus ....................................................................... 34 MFD Page Groups ....................................................... 34 MFD System Pages...................................................... 38 1.8 Display Backlighting ............................................. 48 Automatic Adjustment ................................................ 48 Manual Adjustment .................................................... 48 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ................................................. 54 Airspeed Indicator ...................................................... 54 Attitude Indicator ....................................................... 57 Altimeter ................................................................... 59 Vertical Speed Indicator (VSI) ....................................... 63 Vertical Deviation ....................................................... 63 Horizontal Situation Indicator (HSI) .............................. 64 Course Deviation Indicator (CDI) .................................. 69 2.2 Supplemental Flight Data .................................... 77 Temperature Displays .................................................. 77 Wind Data ................................................................. 78 Vertical Navigation (VNV) Indications ........................... 79 2.3 PFD Annunciations and Alerting Functions ........ 80 System Alerting .......................................................... 80 Marker Beacon Annunciations...................................... 81 Traffic Annunciations................................................... 81 TAWS Annunciations ................................................... 82 Minimum Descent Altitude/Decision Height Alerting ...... 82 Altitude Alerting ......................................................... 84 Low Altitude Annunciation .......................................... 84 Radar Altimeter (Optional)........................................... 85 2.4 Abnormal Operations ........................................... 87 Abnormal GPS Conditions ........................................... 87 Unusual Attitudes ....................................................... 88 SECTION 3 ENGINE INDICATION & CREW ALERTING SYSTEM (EICAS) 3.1 Engine Indication System (EIS) ............................ 91 Engine Stage Rotation Speeds (N1 and N2) ................... 92 Oil Pressure and Temperature ...................................... 93 Fuel Display ............................................................... 93 Interstage Turbine Temperature .................................... 94 Electrical Display ........................................................ 94 Pressurization Display ................................................. 95 Trim and Flap Indicators .............................................. 96 3.2 Crew Alerting System (CAS) ................................. 97 CAS Messages and Prioritization .................................. 98 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview .............................................................. 101 Audio Panel Volume Control ...................................... 101 PFD Controls and Frequency Display ........................... 102 Audio Panel Controls ................................................ 104 4.2 COM Operation .................................................... 106 COM Transceiver Selection and Activation ................... 106 COM Transceiver Manual Tuning ................................ 107 Quick-tuning and Activating 121.500 MHz .................. 108 Auto-tuning the COM Frequency ................................ 109 Frequency Spacing .................................................... 114 Automatic Squelch.................................................... 115 Volume .................................................................... 115 4.3 NAV Operation ..................................................... 116 NAV Radio Selection and Activation ........................... 116 NAV Receiver Manual Tuning ..................................... 117 Auto-tuning a NAV Frequency from the MFD ............... 119 Marker Beacon Receiver ............................................ 124 ADF/DME Tuning ...................................................... 125 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-04 Rev. A viii TABLE OF CONTENTS 4.4 Mode S Transponder ........................................... 129 GTX 33/33D Transponder Controls .............................. 130 GTX 33/33D Transponder Mode Selection.................... 131 TCAS II Transponder Controls (optional) ...................... 133 TCAS II Transponder Mode Selection (optional)............ 134 Entering a Transponder Code ..................................... 136 IDENT Function ........................................................ 137 Flight ID Reporting.................................................... 138 4.5 Additional Audio Panel Functions ..................... 139 Power-up ................................................................. 139 Mono/Stereo Headsets .............................................. 139 Speaker ................................................................... 139 Unmuted Inputs ....................................................... 139 Intercom .................................................................. 140 Passenger Address (PA) System .................................. 141 Simultaneous COM Operation.................................... 141 Clearance Recorder and Player................................... 142 4.6 Audio Panels Preflight Procedure...................... 143 4.7 Abnormal Operation ........................................... 145 Stuck Microphone..................................................... 145 COM Tuning Failure................................................... 145 PFD Failure, Dual System ........................................... 145 Audio Panel Fail-safe Operation ................................. 146 Reversionary Mode ................................................... 146 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction ......................................................... 147 Navigation Status Box............................................... 148 5.2 Using Map Displays ............................................. 150 Map Orientation ....................................................... 150 Map Range .............................................................. 152 Map Panning............................................................ 154 Measuring Bearing and Distance ................................ 159 Topography .............................................................. 160 Map Symbols ........................................................... 163 Airways ................................................................... 169 Track Vector ............................................................. 171 Wind Vector ............................................................. 172 Nav Range Ring........................................................ 173 Fuel Range Ring ....................................................... 174 Field of View (SVS) .................................................... 175 Selected Altitude Intercept Arc ................................... 176 5.3 Waypoints............................................................. 177 Airports ................................................................... 178 Intersections ............................................................ 185 NDBs ....................................................................... 187 VORs ....................................................................... 189 User Waypoints ........................................................ 191 5.4 Airspaces .............................................................. 197 5.5 Direct-to-Navigation .......................................... 201 5.6 Flight Planning..................................................... 207 Flight Plan Creation .................................................. 208 Adding Waypoints to an Existing Flight Plan................ 213 Adding Airways to a Flight Plan ................................. 215 Adding Procedures to a Stored Flight Plan .................. 219 Flight Plan Storage ................................................... 226 Flight Plan Editing .................................................... 228 Along Track Offsets ................................................... 231 Parallel Track ............................................................ 233 Activating a Flight Plan Leg ....................................... 236 Inverting a Flight Plan ............................................... 237 Flight Plan Views ...................................................... 238 Closest Point of FPL .................................................. 240 5.7 Vertical Navigation ............................................. 241 Altitude Constraints .................................................. 243 5.8 Procedures ........................................................... 248 Departures ............................................................... 248 Arrivals ................................................................... 251 Approaches ............................................................. 253 5.9 Trip Planning ........................................................ 259 Trip Planning ............................................................ 259 Weight Planning ....................................................... 263 Weight Caution And Warning Conditions .................... 265 5.10 RAIM Prediction................................................... 266 5.11 Navigating a Flight Plan ..................................... 269 5.12 Abnormal Operation ........................................... 297 SECTION 6 HAZARD AVOIDANCE 6.1 XM WX Satellite Weather ................................... 300 Activating Services.................................................... 300 Using XM WX Products ............................................. 301 Weather Softkeys on the Weather Data Link (XM) Page 305 6.2 Airborne Color Weather Radar .......................... 335 System Description ................................................... 335 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang ix TABLE OF CONTENTS Principles of Pulsed Airborne Weather Radar ............... 335 Safe Operating Distance ............................................ 340 Basic Antenna Tilt Setup ............................................ 340 Weather Mapping and Interpretation ......................... 342 Ground Mapping and Interpretation ........................... 355 System Status........................................................... 356 6.3 TAWS-B ................................................................. 357 Displaying TAWS-B Data ............................................ 358 TAWS-B Page ........................................................... 361 TAWS-B Alerts .......................................................... 363 System Status........................................................... 369 6.4 Profile View Terrain ............................................. 371 Profile View Display .................................................. 372 6.5 Traffic Information Service (TIS) ........................ 375 Displaying TRAFFIC Data ........................................... 376 Traffic Map Page....................................................... 378 TIS Alerts ................................................................. 379 System Status........................................................... 381 6.6 Traffic Advisory System (TAS)............................. 384 TAS Symbology......................................................... 384 Operation ................................................................ 385 Altitude Display ........................................................ 388 Traffic Map Page Display Range ................................. 388 TAS Alerts ................................................................ 390 System Status........................................................... 391 6.7 TCAS II Traffic ....................................................... 393 TCAS II Symbology.................................................... 393 TCAS II Alerts ........................................................... 394 System Test .............................................................. 397 Operation ................................................................ 398 System Status........................................................... 404 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Controls ...................................................... 408 7.2 Flight Director Operation ................................... 410 Activating the Flight Director ..................................... 410 AFCS Status Box ....................................................... 411 Flight Director Modes................................................ 412 Switching Flight Directors .......................................... 412 Command Bars ......................................................... 413 7.3 Vertical Modes ..................................................... 414 Pitch Hold Mode (PIT) ............................................... 415 Selected Altitude Capture Mode (ALTS) ....................... 416 Altitude Hold Mode (ALT) .......................................... 417 Vertical Speed Mode (VS) .......................................... 418 Flight Level Change Mode (FLC) ................................. 419 Vertical Navigation Modes (VPTH, ALTV) ..................... 422 Glidepath Mode (GP) ................................................ 427 Glideslope Mode (GS) ............................................... 429 Takeoff (TO) and Go Around (GA) Modes .................... 430 7.4 Lateral Modes ...................................................... 431 Roll Hold Mode (ROL) ............................................... 432 Low Bank Mode ....................................................... 432 Navigation Modes (GPS, VOR, LOC) ............................ 434 Approach Modes (GPS, VAPP, LOC) ............................. 436 Backcourse Mode (BC) .............................................. 437 7.5 Autopilot and Yaw Damper Operation ............. 439 Flight Control ........................................................... 439 Engagement............................................................. 440 Control Wheel Steering ............................................. 440 Disengagement ........................................................ 441 7.6 Example Flight Plan ............................................ 442 Departure ................................................................ 443 Intercepting a VOR Radial .......................................... 445 Flying a Flight Plan/GPS Course ................................. 446 Descent ................................................................... 447 Approach ................................................................. 451 Go Around/Missed Approach ..................................... 454 7.7 AFCS Annunciations and Alerts ......................... 456 AFCS Status Alerts .................................................... 456 Overspeed Protection ................................................ 457 Emergency Descent Mode (EDM) ............................... 457 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision System (SVS) ........................... 460 SVS Operation .......................................................... 461 SVS Features ............................................................ 463 Field of View ............................................................ 472 8.2 SafeTaxi ................................................................ 474 SafeTaxi Cycle Number and Revision .......................... 477 8.3 ChartView ............................................................. 480 ChartView Softkeys ................................................... 480 ChartView Terminal Procedures Charts........................ 481 Chart Options........................................................... 489 Day/Night View ........................................................ 495 ChartView Cycle Number and Expiration Date ............. 497 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-04 Rev. A x TABLE OF CONTENTS 8.4 FliteCharts ............................................................ 500 FliteCharts Softkeys .................................................. 500 FliteCharts Terminal Procedures Charts ....................... 501 Chart Options........................................................... 508 Day/Night View ........................................................ 512 FliteCharts Cycle Number and Expiration Date............. 514 8.5 AOPA Airport Directory....................................... 517 AOPA Database Cycle Number and Revision ............... 518 8.6 SiriusXM Satellite Radio Entertainment........... 520 Activating SiriusXM Satellite Radio Services ................ 520 Using SiriusXM Satellite Radio ................................... 522 8.7 Scheduler.............................................................. 525 8.8 Flight Data Logging ............................................ 527 8.9 Abnormal Operation ........................................... 529 SVS Troubleshooting ................................................. 529 Reversionary Mode ................................................... 529 Unusual Attitudes ..................................................... 530 APPENDICES Annunciations and Alerts ............................................. 533 CAS Messages .......................................................... 533 Comparator Annunciations ........................................ 534 Reversionary Sensor Annunciations ............................ 535 G1000 System Annunciations .................................... 535 G1000 System Message Advisories............................. 538 AFCS Alerts .............................................................. 551 TAWS-B ALERTS ........................................................ 552 TCAS II Alerts and Annunciations ............................... 553 Weather Radar Alerts and Annunciations .................... 554 Other G1000 Aural Alerts .......................................... 555 Flight Plan Import/Export Messages ........................... 555 Database Management ................................................ 557 Jeppesen Databases.................................................. 557 Garmin Databases .................................................... 561 Glossary.......................................................................... 567 Frequently Asked Questions ........................................ 573 General TIS Information ............................................... 577 Introduction ............................................................. 577 TIS vs. TAS/TCAS ....................................................... 577 TIS Limitations.......................................................... 577 Display Symbols ............................................................ 579 INDEX Index ................................................................................ I-1 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna Citation Mustang. 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 1040A Primary Flight Display (PFD) • GDU 1500 Multi Function Display (MFD) • GIA 63W Integrated Avionics Unit • GDC 74B Air Data Computer (ADC) • GEA 71 Engine/Airframe Unit • GRS 77 Attitude and Heading Reference System (AHRS) • GMU 44 Magnetometer • GMA 1347D or GMA 1347D-20 Dual Audio System with Integrated Marker Beacon Receiver • GTX 33/33D Mode S Transponder (not used with optional TCAS II) • GDL 69A Satellite Data Link Receiver • GWX 68 Weather Radar • GCU 475 MFD Control Unit • GMC 710 AFCS Control Unit • GSD 41 Data Concentrator (optional) • GTP 59 Outside Air Temperature (OAT) Probe • GA 36 GPS/SBAS and GA 37 GPS/SBAS/SiriusXM Antennas • GSA 80 and GSA 81 AFCS Servos • GSM 85A Servo Gearboxes A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, or GSM 85A). The following equipment is also connected to the G1000 system and interfaces with the GIA 63Ws: • Becker RA 3502 – A remotely mounted ADF receiver that operates in the 190.0 kHz to 1799.5 kHz frequency band with 0.5 kHz channel spacing. • Honeywell KN 63 – A remotely mounted 200-channel, 100-watt, all-solid-state digital DME transceiver that provides distance information to the G1000 system. • Honeywell KTA 870 – Traffic Advisory System • Honeywell KHF 1050 – HF Transceiver • Honeywell KRA405B – Radar Altimeter • Aviation Communication & Surveillance Systems RCZ 852 – Mode S Transponder • L-3 FA2100 – Cockpit Voice and Flight Data Recorder NOTE: Refer to the AFCS section for details on the GFC 700 AFCS. In the Cessna Citation Mustang, the GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 2 SYSTEM OVERVIEW 1.2 LINE REPLACEABLE UNITS (LRU) • GDU 1040A (2) – Each unit is configured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution. The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection. • GDU 1500 (1) – Features a 15-inch LCD with 1024 x 768 resolution and is configured as an MFD. This unit is linked to both PFDs via HSDB connection. • GIA 63W (2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA 63Ws are not paired together and do not communicate with each other directly. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 3 SYSTEM OVERVIEW • GDC 74B (2) – 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 on-side GIA 63W, on-side GDU 1040A and on-side GRS 77, using an ARINC 429 digital interface (it also interfaces directly with the on-side GTP 59). The GDC 74B is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace. • GEA 71 (2) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63Ws using an RS-485 digital interface. • GRS 77 (2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU 1040A and the on-side GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74B to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document. • GMU 44 (2) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77, using an RS-485 digital interface. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 4 SYSTEM OVERVIEW • GMA 1347D or GMA 1347D-20 (2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with the on-side GIA 63W, using an RS-232 digital interface. • GTX 33 (1) and GTX 33D (1 or 2) – Solid-state transponders that provide Modes A, C and S capability. Transponder #1 (XPDR1) is a GTX 33D, which includes Mode S with diversity. Either the GTX 33 or GTX 33D may be installed as Transponder #2 (XPDR2). Both transponders can be controlled from either PFD, and only one transponder can be active at a time. Each transponder communicates with the on-side GIA 63W through an RS-232 digital interface. • GDL 69A (1) – A satellite radio receiver that provides 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. • GWX 68 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the GDL 69A, via HSDB connection. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 5 SYSTEM OVERVIEW • GCU 475 (1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital interface. • GMC 710 (1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing communication with both PFDs. • GSD 41 (1) – This optional unit is a data concentrator used to expand the input and output capabilities of the system when a Cockpit Voice Data Recorder is installed. Communication is through the High Speed Data Bus. • GTP 59 (2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B. • GSA 80 (2), GSA 81 (2), and GSM 85A (4) – The GSA 80 servos are used for the automatic control of roll and yaw, while the GSA 81 servos are used for the automatic control of pitch and pitch trim. These units interface with each GIA 63W. The GSM 85A servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to the mechanical flight-control surface linkage. • GA 36 (1) and GA 37 (1) – The GA 36 is a through-mount GPS/SBAS antenna. The GA 37 is a through-mount GPS/SBAS antenna with SiriusXM/Data Link. GA 36 GA 37 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 6 SYSTEM OVERVIEW GDU 1040A (PFD #1) GDU 1040A (PFD #2) GDU 1500 (MFD) GIA 63W #2 GSA 80 (Yaw) GSA 80 (Roll) GSA 81 (Pitch) GSA 81 (Pitch Trim) GRS 77 #1 GIA 63W #1 GMC 710 GMU 44 #1 GEA 71 #2 GEA 71 #1 GDC 74B #1 GTP 59 #1 #2 GMA 1347D or GMA 1347D-20 #1 GTX 33D GTX 33 GCU 475 GDL 69A GRS 77 #2 GMU 44 #2 GDC 74B #2 GTP 59 #2 VHF COM VHF NAV/LOC GPS/WAAS G/S AFCS Mode Logic Flight Director Servo Management VHF COM VHF NAV/LOC GPS/WAAS G/S AFCS Mode Logic Flight Director Servo Management GMA 1347D or GMA 1347D-20 GSD 41 GWX 68 Figure 1-1 G1000 System (LRU Configuration) 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 7 SYSTEM OVERVIEW 1.3 G1000 CONTROLS NOTE: The Audio Panel (GMA 1347D) and AFCS controls (GMC 710) are described in the CNS & Audio Panel and AFCS sections respectively. The G1000 system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD CONTROLS Figure 1-2 PFD Controls 2 1 5 4 6 8 7 3 11 12 10 9 15 14 13 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 8 SYSTEM OVERVIEW The following list provides an overview of the controls located on the PFD bezel (see Figure 1-2). 1 NAV VOL/ID Knob – Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON and OFF. Volume level is shown in the NAV frequency field as a percentage. 2 NAV Frequency Transfer Key – Toggles the standby and active NAV frequencies. 3 Dual NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2. 4 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. 5 BARO Knob – Sets the altimeter barometric pressure. Press to enter standard pressure (STD BARO). 6 Dual COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2. 7 COM Frequency Transfer Key – Toggles the standby and active COM frequencies. Press and hold this key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field. 8 COM VOL/SQ Knob – Controls COM audio volume level. Volume level is shown in the COM frequency field as a percentage. Press to turn the COM automatic squelch ON and OFF. 9 Direct-to Key ( ) – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 10 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan. 11 CLR Key – Erases information, cancels entries, or removes page menus. 12 Dual FMS Knob – Flight Management System Knob. Press the FMS Knob to turn the selection cursor ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small and large knobs. The large knob moves the cursor on the page, while the small knob selects individual characters for the highlighted cursor location. 13 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 14 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 15 ENT Key – Validates or confirms a menu selection or data entry. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 9 SYSTEM OVERVIEW CONTROLS ASSOCIATED WITH THE MFD The controls for the MFD (GDU 1500) are located on both the MFD bezel and the MFD Control Unit (GCU 475). The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide documentation. The following list provides an overview of the controls located on the MFD Control Unit (see Figure 1-3): 3 4 5 2 6 7 8 9 13 12 11 10 Figure 1-3 MFD Control Unit (GCU 475) 1 14 1 Dual FMS Knob – Flight Management System Knob. This knob selects the MFD page to be viewed; the large knob selects a page group (MAP, WPT, AUX, NRST), while the small knob selects a specific page within the page group. Pressing the FMS Knob turns the selection cursor ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small and large knobs. 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). In this case, the large knob moves the cursor on the page, while the small knob selects individual characters for the highlighted cursor location. Figure 1-4 Data Insertion Pointer and Quick Select Box Data is Inserted Above the Cursor, Indicated by the Data Insertion Pointer Data Can be Inserted Directly into the Quick Select Box 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 10 SYSTEM OVERVIEW 2 Direct-to Key ( ) – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 3 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. 4 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 5 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. Theses procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 6 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. Also, used to position the Quick Select Box in the desired field as shown in Figure 1-4. Also, see the Flight Planning discussion in the Flight Management section for further explanation of the Quick Select Box. 7 Alphanumeric Keys – Allow the user to enter data quickly, without having to select individual characters with the FMS Knob. 8 Plus (+) Minus (-) Key – Toggles a (+) or (-) character. 9 Decimal Key – Enters a decimal point. 10 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box to the right and left, respectively. 11 ENT Key – Validates or confirms a menu selection or data entry. 12 CLR Key – Erases information, cancels entries, or removes page menus. Pressing and holding this key displays the Navigation Map Page automatically. 13 SPC Key – Adds a space character. 14 BKSP Key – Moves the cursor back one character space. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 11 SYSTEM OVERVIEW AFCS CONTROLS NOTE: With the exception of the FD and SPD Keys, if a key is selected, its respective annunciator is illuminated. 1 2 3 4 5 6 7 8 10 9 17 16 15 14 13 12 11 18 19 Figure 1-5 AFCS Control Unit (GMC 710) The GFC 700 AFCS is mainly controlled through the GMC 710 AFCS Control Unit. The AFCS Control Unit consists of the following controls: 1 HDG Key – Selects/deselects Heading Select Mode. 2 APR Key – Selects/deselects Approach Mode. 3 NAV Key – Selects/deselects Navigation Mode. 4 FD Key – Activates/deactivates the flight director in the default pitch and roll modes. If the autopilot is engaged, the FD Key is disabled. 5 XFR Key – Switches the autopilot between the pilot-side and the copilot-side flight directors. This selection also selects which air data computer is communicating with the active transponder. Upon power-up, the pilot-side FD is selected. 6 ALT Key – Selects/deselects Altitude Hold Mode. 7 VS Key – Selects/deselects Vertical Speed Mode. 8 FLC Key – Selects/deselects Flight Level Change Mode. 9 CRS2 Knob – Sets the copilot-selected course on the HSI of PFD2 when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The copilot-selected course provides course reference to the copilot-side flight director when operating in Navigation and Approach modes. 10 SPD Key – Switches the Flight Level Change mode reference speed between IAS and MACH number. 11 NOSE UP/DN Wheel – Controls the active mode reference for the Pitch, Vertical Speed, and Flight Level Change modes. 12 VNV Key – Selects/deselects Vertical Navigation mode. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 12 SYSTEM OVERVIEW 13 ALT SEL Knob – Sets the selected altitude in the Selected Altitude Box. In addition to providing the standard G1000 altitude alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold mode of the AFCS. 14 YD Key – Engages/disengages the yaw damper. 15 AP Key – Engages/disengages the autopilot. 16 BANK Key – Selects/deselects Low Bank Mode. 17 CRS1 Knob – Sets the pilot-selected course on the HSI of PFD1 when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The pilot-selected course provides course reference to the pilot-side flight director when operating in Navigation and Approach modes. 18 BC Key – Selects/deselects Back Course Mode. 19 HDG Knob – Sets the selected heading on the HSI. When operating in Heading Select mode, this knob provides the heading reference to the flight director. ADDITIONAL AFCS CONTROLS The AP DISC (Autopilot Disconnect) Switch, CWS (Control Wheel Steering) Button, GO AROUND Switch, and MEPT (Manual Electric Pitch Trim) Switch are additional AFCS controls and are located in the cockpit, separately from the AFCS Control Unit. These are discussed in detail in the AFCS section. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 13 SYSTEM OVERVIEW AUDIO PANEL CONTROLS Figure 1-6 Audio Panel Controls 17 18 15 13 11 9 20 7 5 3 1 14 2 16 4 6 8 10 12 22 24 23 21 19 21 25 GMA 1347D GMA 1347D-20 NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 1 COM1 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. 2 COM1 – When selected, audio from the #1 COM receiver can be heard. 3 COM2 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. 4 COM2 – When selected, audio from the #2 COM receiver can be heard. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 14 SYSTEM OVERVIEW 5 COM3 MIC – Selects the KHF 1050 transmitter for transmitting (if installed). COM3 is simultaneously selected when this key is pressed allowing received audio from the HF receiver to be heard. COM3 can be deselected by pressing the COM3 Key, or COM1/COM2 can be added by pressing the COM1/COM2 Key. 6 COM3 – When selected, audio from the HF receiver (if installed) can be heard. 7 PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key is pressed. 8 TEL – Not used on the Cessna Citation Mustang. 9 MUSIC – Press to deliver SiriusXM audio to the cockpit. 10 SPKR – Pressing this key selects and deselects the corresponding cockpit speaker. COM and NAV receiver audio will be heard on the speaker. 11 MKR/MUTE – Mutes the currently received marker beacon receiver audio. Unmutes when new marker beacon audio is received. 12 HI SENS – Press to increase Marker Beacon Receiver sensitivity. Press again to return to normal. 13 DME – Pressing turns the optional DME audio on or off. 14 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 15 ADF – Pressing turns on or off the audio from the ADF receiver. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Not used on the Cessna Citation Mustang. 18 REC – Press to start the recording up to 2.5 minutes of COM receiver audio. When no audio is being received, nothing is recorded. Press again to stop recording. 19 PLAY – Press once to play the last recorded audio. Press again to stop playing. Press twice quickly while audio is playing and the previous block of recorded audio will be played. Each subsequent two presses will skip back to the previously recorded block. 20 INTR COM – Pressing selects the pilot/copilot intercom on both audio panels. Press again to deselect the intercom. 21 MAN SQ – Press to enable manual squelch for the intercom. When active, press the ICS Knob to illuminate ‘SQ’. Turn the ICS Knob to adjust squelch. 22 ICS Knob – Turn to adjust intercom volume or squelch. Press to switch between volume and squelch control as indicated by the ‘VOL’ or ‘SQ’ being illuminated. The MAN SQ Key must be selected to allow squelch adjustment. 23 MSTR Knob – The Master Volume Control adjusts volume for the blended NAV, COM, and intercom audio. 24 Reversionary Mode Button – Pressing manually selects Reversionary Mode. 25 CABIN – Not used on the Cessna Citation Mustang. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 15 SYSTEM OVERVIEW 1.4 SECURE DIGITAL CARDS NOTE: Refer to the Appendices for instructions on updating the aviation database. NOTE: Ensure that the G1000 system is powered off before inserting the SD card. The GDU 1040A and GDU 1500 data card slots use Secure Digital (SD) cards and are located on the top right portion of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database and system software updates as well as terrain database storage. Not all SD cards are compatible with the G1000. Use only SD cards supplied by Garmin or the aircraft manufacturer. Install an SD card 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. Remove an SD card Gently press on the SD card to release the spring latch and eject the card. Figure 1-7 Display Bezel SD Card Slots PFD MFD SD Card Slots 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 16 SYSTEM OVERVIEW 1.5 SYSTEM POWER-UP NOTE: Refer to the Appendices for AHRS initialization bank angle limitations. NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts. NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. The G1000 system is integrated with the aircraft electrical system and receives power directly from electrical busses. The G1000 PFDs, 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 1-8. All system annunciations should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the audio panels, the control units and the display bezels. 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 one minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up (Figure 1-9), the MFD Power-up Page displays the following information: • System version • Copyright • Land database name and version • Safe Taxi database information • Terrain database name and version • Airport Terrain database name and version • Obstacle database name and version • Navigation database name, version, and effective dates • Airport Directory name, version and effective dates • FliteCharts or ChartView database information Current database information includes the valid operating dates, cycle number and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information and displays the Auxiliary (AUX) Weight Planning Page. Figure 1-9 MFD Power-up Page Figure 1-8 PFD Initialization 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 17 SYSTEM OVERVIEW 1.6 SYSTEM OPERATION The displays are connected together via a single Ethernet bus, thus allowing for high-speed communication. As shown in Figure 1-1, each GIA 63W is connected to the on-side PFD. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the G1000 system. NORMAL OPERATION PFD In normal mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude and vertical speed), thereby replacing the traditional flight instrument cluster. The PFD also offers control for COM and NAV frequency selection. MFD In normal mode, the right portion of the MFD displays a full-color moving map with navigation information, while the left portion of the MFD is dedicated to the Engine Indication and Crew Alerting System (EICAS). Figure 1-10 gives an example of the G1000 displays in normal mode. Figure 1-10 Normal Operation MFD PFD1 PFD2 REVERSIONARY MODE NOTE: The G1000 system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for further information regarding system-specific alerts. Reversionary mode is a mode of operation in which all important flight information is presented identically on at least one of the remaining displays (see Figure 1-11). Transition to reversionary mode should be straightforward for the pilot, for flight parameters are presented in the same format as in normal mode. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 18 SYSTEM OVERVIEW In reversionary mode, critical flight instrumentation is combined with engine instrumentation on the remaining display. Minimal navigation capability is available on the reversionary mode display. Figure 1-11 Reversionary Mode (Manual) If the system detects a failure in the MFD, PFD1 will enter reversionary mode automatically. Reversionary mode must be entered manually in the case of PFD1 or PFD2 failure. Reversionary mode is manually activated by pressing the dedicated DISPLAY BACKUP button at the bottom of the audio panel (see Figure 1-12 and refer to the Audio Panel section for further details). Pressing this button again deactivates reversionary mode. Figure 1-12 DISPLAY BACKUP Button Pressing the D I S P L AY BACKUP button activates/ deactivates reversionary mode for both the on-side PFD and the MFD. Each display can be configured to operate in reversionary mode, as follows: • PFD1 – Manual reversion by pressing the DISPLAY BACKUP button on the left audio panel. • MFD – Auto-reversion by the system or manually by pressing the DISPLAY BACKUP button on the left or the right audio panel. • PFD2 – By pressing the DISPLAY BACKUP button on the right audio panel. Should the connection between a PFD and the on-side GIA 63W become inoperative, the on-side GIA 63W can no longer communicate with the remaining PFD (refer to Figure 1-1). As a result, the NAV and COM functions provided to the failed PFD by the on-side GIA 63W are flagged as invalid (red “X”) on the remaining PFD (see Figure 1-13). Figure 1-13 Inoperative Input (NAV1 Shown) 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 19 SYSTEM OVERVIEW AHRS OPERATION NOTE: Refer to the Appendices for specific AHRS alert information. NOTE: Aggressive maneuvering while the AHRS is not operating normally can degrade AHRS accuracy. In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic field data and air data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic field measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air data information for attitude determination. Four AHRS modes of operation are available (see Figure 1-14) and depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor inputs is communicated to the pilot by message advisory alerts. Attitude/Heading Invalid AHRS no-GPS Mode AHRS Normal Operation AHRS no- Mag Mode AHRS no-Mag/ no-Air Mode Heading Invalid available available unavailable unavailable available unavailable unavailable available Air Data Magnetometer Data unavailable available GPS Data Magnetometer Data Air Data Figure 1-14 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. The G1000 system provides two sources of GPS information. If a single GPS receiver fails, or if the information provided from one of the GPS receivers is unreliable, the AHRS seamlessly transitions to using the other GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 20 SYSTEM OVERVIEW GPS inputs fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer inputs are available and valid. AIR DATA INPUT FAILURE A failure of the air data input has no effect on AHRS output while AHRS is operating in normal mode. A failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid attitude and heading information on the PFD (as indicated by red “X” flags). MAGNETOMETER FAILURE If the magnetometer input fails, the AHRS transitions to one of the reversionary No-Magnetometer modes and continues to output valid attitude information. However, if the aircraft is airborne, the heading output on the PFD does become invalid (as indicated by a red “X”). G1000 SYSTEM ANNUNCIATIONS NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Airplane Flight Manual (AFM) 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 1-15 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 Garmin- authorized repair facility. Figure 1-15 G1000 System Failure Annunciations GDC 74B Air Data Computer GTX 33/D Transponder Or GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GEA 71 Engine Airframe Unit Or GIA 63W Integrated Avionics Unit GIA 63W Integrated Avionics Units GRS 77 AHRS Or GMU 44 Magnetometer GIA 63W Integrated Avionics Units GIA 63W Integrated Avionics Units FADEC Fuel Qty. Signal Conditioner KAPSII Pressure Controller GEA 71 Engine Airframe Unit GEA 71 Engine Airframe Unit 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 21 SYSTEM OVERVIEW 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 Names (displayed) Figure 1-16 Softkeys (Second-Level PFD Configuration) Bezel-Mounted Softkeys (press) Softkey On Another means of selecting softkeys on the MFD is by using the MFD Control Unit: Selecting a softkey using the MFD Control Unit 1) Move the softkey selection box to the desired softkey using the arrows of the SEL Key. 2) Press the center of the SEL Key to select the desired softkey. PFD SOFTKEYS The CDI, IDENT, TMR/REF, NRST, and MSG Softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. If messages remain after acknowledgement, the MSG Softkey will be black on white. 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 pressed to return to the previous level. The MSG Softkey is visible in all softkey levels. For the top level softkeys and the transponder (XPDR) levels, the IDENT Softkey remains visible. Level 1 Level 2 Level 3 Level 4 Description INSET or TRFC/MAP Displays Inset Map in PFD lower left corner. The TRFC/MAP Softkey is displayed when the TCAS II option is installed. Pressing the TRFC/ MAP Softkey displays the Inset Map showing Traffic Map Page. 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: TRAFFIC: Traffic not displayed on inset map TRFC-1: Traffic displayed on inset map TRFC-2: Traffic Map Page is displayed in the inset map window 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 22 SYSTEM OVERVIEW Level 1 Level 2 Level 3 Level 4 Description TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map (optional feature) XM LTNG Displays XM WX lightning information on Inset Map (optional feature) METAR Displays METAR flags on airport symbols shown on the Inset Map (optional) SENSOR Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers ADC1 Selects the #1 Air Data Computer ADC2 Selects the #2 Air Data Computer AHRS1 Selects the #1 AHRS AHRS2 Selects the #2 AHRS 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 WIND Displays softkeys to select wind data parameters OPTN 1 Wind direction arrows with headwind/tailwind and crosswind components OPTN 2 Wind direction arrow and speed OPTN 3 Wind direction arrow with headwind/tailwind and crosswind components OFF Information not displayed DME Displays the information window for DME BRG1 Cycles the Bearing 1 Information Window through NAV1, GPS/ waypoint identifier and GPS-derived distance information. BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS-derived distance information. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 23 SYSTEM OVERVIEW Level 1 Level 2 Level 3 Level 4 Description ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled, displays altimeter in meters 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 units are selected) OBS Selects OBS mode on the CDI when navigating by GPS (only available with active leg) CDI Cycles through GPS, VOR1 (LOC1), and VOR2 (LOC2) navigation source on the CDI ADF/DME (when ADF is installed) or DME Displays the ADF/DME Tuning Window, providing ADF (when installed) tuning tuning, ADF Mode selection, ADF volume control, and selection of the NAV source for tuning each DME Transponder Softkeys without TCAS II Option XPDR Displays transponder mode selection softkeys XPDR1 Selects the #1 transponder as active XPDR2 Selects the #2 transponder as active STBY Selects standby mode (transponder does not reply to any interrogations) ON Selects Mode A (transponder replies to identification interrogations) ALT Selects Mode C – altitude reporting mode (transponder replies to identification and altitude interrogations) GND Manually selects Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations (not available with TCAS II) VFR Automatically enters the VFR code (1200 in the U.S.A. only)(not avialable with TCAS II) CODE Displays transponder code selection softkeys 0-7 0 — 7 Use numbers to enter code 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 NRST Displays Nearest Airports Window MSG Displays Messages Window 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 24 SYSTEM OVERVIEW Level 1 Level 2 Level 3 Level 4 Description Transponder/Traffic Softkeys with TCAS II Option XPDR/TFC Displays the transponder and TCAS II system selection softkeys MODE Displays transponder mode selection softkeys STBY Selects transponder Standby Mode (transponder does not reply to any interrogations). When the transponder is set to standby, the TCAS II system is also set to standby. ON Activates transponder (transponder replies to identification interrogations). When the transponder is set to ON, the TCAS II system is set to standby. ALT Altitude Reporting Mode (transponder replies to identification and altitude interrogations). When the transponder is set to ALT, the TCAS II system is set to standby. TA ONLY Activates the TCAS II system in TA Only Mode and sets the transponder to ALT TA/RA Activates the TCAS II system in TA/RA Mode and sets the transponder to ALT BACK Returns to the previous softkey level TCAS Displays the TCAS control softkeys REL Displays intruder altitude as altitude relative to own aircraft altitude ABS Displays intruder MSL altitude ALT RNG Displays the altitude display range softkeys ABOVE Displays non-threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. NORMAL Displays non-threat traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. BELOW Displays non-threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight. UNREST All traffic is displayed TEST Activates Test Mode and displays test intruder symbols BACK Returns to the previous softkey level 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, 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 NRST Displays Nearest Airports Window MSG Displays Messages Window 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 25 SYSTEM OVERVIEW Figure 1-17 Top Level PFD Softkeys Figure 1-18 INSET Softkeys Select the BACK or OFF Softkey to return to the top-level softkeys. TRFC-1 TRFC-2 WX LGND METAR Figure 1-19 SENSOR Softkeys Press the BACK Softkey to return to the top level softkeys. BACK MSG ADC2 ADC1 AHRS1 AHRS2 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 26 SYSTEM OVERVIEW Figure 1-20 PFD Configuration Softkeys Select the BACK Softkey to return to the top-level softkeys ALT UNIT METERS IN HPA SYN VIS SYN TERR HRZN HDG PATHWAY APTSIGNS (optional) Figure 1-21 XPDR Softkeys (without TCAS II) Press the BACK Softkey to return to the top-level softkeys. Press the BACK Softkey to return to the top-level softkeys. MSG MSG 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 27 SYSTEM OVERVIEW MSG MSG ADF/DME TRFC/MAP XPDR/TFC Press the BACK Softkey to return to the top-level softkeys. MSG MODE TCAS CODE IDENT Selecting BACK returns to the previous softkey level. Selecting BACK returns to the previous softkey level. Selecting BACK returns to the previous softkey level. MSG REL ABS ALT RNG TEST TA ONLY TA/RA SENSOR PFD OBS CDI IDENT TMR/REF NRST MSG BACK STBY ON ALT BACK BACK IDENT BKSP BACK 0 5 4 3 2 1 6 7 MSG Selecting BACK returns to the previous softkey level. UNREST ABOVE BELOW NORMAL BACK Figure 1-22 XPDR Softkeys (with TCAS II) MFD SOFTKEYS Level 1 Level 2 Level 3 Description CAS ↑ Scroll up (enabled only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling) CAS ↓ Scroll down (enabled only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling) 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 (not available with TAWS-A) AIRWAYS Displays airways on the map; cycles through the following: AIRWAYS: No airways are displayed AIRWY ON: All airways are displayed AIRWY LO: Only low altitude airways are displayed AIRWY HI: Only high altitude airways are displayed (Default label is dependant on map setup option selected) 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 28 SYSTEM OVERVIEW Level 1 Level 2 Level 3 Description NEXRAD Displays NEXRAD weather and coverage information on Navigation Map (optional feature) XM LTNG Displays XM WX lightning information on Navigation Map (optional feature) 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 the active flight plan SHW CHRT When available, displays optional airport and terminal procedure charts Figure 1-23 MFD Softkeys MAP DCLTR DCLTR-2 DCLTR-3 DCLTR-1 SHW CHRT (optional) (Default softkey is dependant on the selection made in the map setup options) AIRWY ON AIRWY LO AIRWAYS AIRWY HI Press the BACK softkey to return to the top-level softkeys. BACK METAR XM LTNG NEXRAD AIRWAYS TERRAIN PROFILE TOPO TRAFFIC LEGEND CAS ↓ CAS ↑ 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 29 SYSTEM OVERVIEW GPS RECEIVER OPERATION Each GIA 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. GPS1 provides information to the pilot-side PFD and GPS2 provides data to the copilot-side PFD. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFDs. In some circumstances, both GPS receivers may be providing accurate data, but one receiver may be providing a better GPS solution than the other receiver. In this case the GPS receiver producing the better solution is automatically coupled to both PFDs. “BOTH ON GPS 1” or “BOTH ON GPS 2” are then displayed in the Reversionary Sensor Window (see Appendix A) indicating which GPS receiver is being used. Both GPS receivers are still functioning properly, but one receiver is performing better than the other at that particular time. These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other, or one of the GPS receivers has not yet acquired an SBAS (Satellite Based Augmentation System) 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 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) Select 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. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 30 SYSTEM OVERVIEW Figure 1-24 GPS Status Page (RAIM or SBAS Selected) Satellite Signal Strength Bars Satellite Constellation Diagram Satellite Signal Information Status RAIM Availability Prediction GPS Receiver Status Enabled SBAS Options RAIM Softkey Selected SBAS Softkey Selected GPS Selection Softkeys 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. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 31 SYSTEM OVERVIEW 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 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 differential 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 be 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, select 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: 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 32 SYSTEM OVERVIEW 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. 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. 8) 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 Predicting RAIM availability at present position 1) Select the GPS Status Page. 2) If necessary, select the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Press the MENU Key. 5) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. 6) Press the ENT Key to accept the waypoint entry. 7) Use the FMS Knob to enter an arrival time and press the ENT Key. 8) Use the FMS Knob to enter an arrival date and press the ENT Key. 9) 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. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 33 SYSTEM OVERVIEW Disabling WAAS, EGNOS or MSAS 1) Select the GPS Status Page. 2) If necessary, select 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). 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 34 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. Figure 1-25 Page Menu Examples No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed MFD PAGE GROUPS NOTE: Refer to other supporting sections in this Pilot’s Guide 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 box are displayed in the upper right of the screen. In the bottom right corner of the screen, a page group window is displayed by turning either FMS Knob. The page group tabs are displayed along the bottom of the window. The page titles are displayed in a list above the page group tabs. The current page group and current page within the group are shown in light blue. For some of these pages (Airport/Procedures/ Weather Information, SiriusXM, Procedure Loading), the active title of the page changes while the page name in the list remains the same. 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 35 SYSTEM OVERVIEW Figure 1-26 Page Title and Page Groups Page Group Active Page Title MFD Page Groups Pages in Current Group The main page groups are navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the FMS Knob: 1) Turn the large FMS Knob to display the list of page groups; continue turning the large FMS Knob until the desired page group is selected 2) Turn the small FMS Knob to display the desired page within a specific page group. 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 selected. Figure 1-27 Map Pages Map Pages (MAP) Navigation Map Traffic Map Weather Radar Weather Data Link (service optional) TAWS 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 36 SYSTEM OVERVIEW 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 1-28 Waypoint Pages Airport Information Pages Figure 1-29 Auxiliary Pages Auxiliary Pages (AUX) Weight Planning Trip Planning Utility GPS Status System Setup SiriusXM Satellite pages - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) System Status SiriusXM Satellite Pages 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 37 SYSTEM OVERVIEW Figure 1-30 Nearest Pages Nearest Pages (NRST) Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies Nearest Airspaces 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. Figure 1-31 Flight Plan Pages Flight Plan Pages (FPL) Active Flight Plan - Wide View, Narrow View (VIEW Softkey) Flight Plan Catalog or Stored Flight Plan (NEW Softkey) Narrow and Wide View 190-00494-04 Rev. A Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 38 SYSTEM OVERVIEW 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). Figure 1-32 Procedure Pages Procedure Pages (PROC) Departure Loading Arrival Loading Approach Loading 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. 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: • Date/time • Display Units (see Flight Instruments Section)