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1 | INSTALLATION MANUAL | Users Manual | 1.53 MiB |
SPECIFICATION CONTROL DRAWING DATE REV. 1 5/12/05 Preliminary Release ECO NO.
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REVISIONS DESCRIPTION 11"
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GWX 68 Installation Manual 3-Hole Punch DER REVIEW REQUIRED GWX 68 Installation Manual Letter: Width = 8.5 inches, Height = 11 inches Tabloid: Width = 11.0 inches, Height = 17.0 inches NOTES:
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30 5 single-sided tabloid sheets. 190-00286-01.pdf The following les have been archived under the aboce ARCHIVE FILENAME. Filename 190-00286-01.pdf release.indd Manual Elements
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File Contents Portable Document Format, contains Installation Manual and Release Speci cation Adobe InDesign Format, Release Speci cation Word 97 for PC, Formatted Files and Figures Various supporting illustrations, drawings, and artwork. CONFIDENTIAL This drawing and the speci cations contained herein are the property of Garmin Ltd. or its subsidiaries and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products without written permission . Drafter:
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GWX 68 Installation Manual Garmin Ltd. or its subsidiaries c/o Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 U.S.A. PART NO:
SIZE A Scale: N/A 190-00286-01 REV. 1 Page of 1 36 Preliminary GWX 68 Installation Manual Garmin P/N 190-00286-01 May, 2005 Preliminary Revision 1 Copyright 2005 Garmin Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin International, Inc. 1200 E. 151st Street Olathe, KS 66062 USA Telephone: 913-397-8200 www.garmin.com Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL U.K. 44/0870.851241 RECORD OF REVISIONS Revision 1 Revision Date 5/12/05 Initial Release Description ECO #
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DOCUMENT PAGINATION Section Table of Contents Section 1 Section 2 Section 3 Section 4 Appendix A Appendix B Page Range i - vi 1-1 1-6 2-1 2-2 3-1 3-10 4-1 4-4 A-1 A-2 B-1 B-8 Page A Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 This manual reflects the operation of software version TBD. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. INFORMATION SUBJECT TO EXPORT CONTROL LAWS This document may contain information which is subject to the Export Administration Regulations
("EAR") issued by the United States Department of Commerce (15 CFR, Chapter VII, Subchapter C) and which may not be exported, released, or disclosed to foreign nationals inside or outside of the United States without first obtaining an export license. A violation of the EAR may be subject to a penalty of up to 10 years imprisonment and a fine of up to $1,000,000 under Section 2410 of the Export Administration Act of 1979. Include this notice with any reproduced portion of this document. WARNING 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 additional would at www.garmin.com/prop65. information, our web please refer like site to WARNING This radar device produces microwave radiation. DO NOT OPERATE THIS DEVICE UNTIL ALL SAFETY PRECAUTIONS AND INSTRUCTIONS IN THE OPERATING AND INSTALL MANUALS HAVE BEEN READ. IMPROPER USE OR EXPOSURE MAY RESULT IN BODILY INJURY. All personnel should remain the prescribed safe distance Never expose any part of the body to an unterminated CAUTION from this radar. waveguide. GWX 68 Installation Manual 190-00286-01 Page i Preliminary Revision 1 SAFE DISTANCE DETERMINATION The following information establishes a minimum safe distance from the antenna for personnel near an operating airborne weather radar. The minimum safe distance is based upon the FCCs exposure limit at 9.3 to 9.5 GHz for general population/uncontrolled environments which is 1 mW/cm2. See AC 20-68B for more information on safe distance determination. Antenna Size 10 12 Safe Distance 9.16 ft 10.8 ft MAXIMUM PERMISSIBLE EXPOSURE LEVEL (MPEL) The zone in which the radiation level exceeds the US Government standard of 1 mW/cm2, is the semi-
circular area of at least 9.16 ft from the 10 antenna and 10.83 ft from the 12 antenna as indicated in the illustration below. All personnel must remain outside of this zone. The distance to the MPEL boundary is calculated upon the basis of each antenna available with the GWX 68 system, rated output power of the transmitter, and in the non-rotating or boresight position of the antenna (see example calculations above). With a scanning or rotating beam, the averaged power density at the MPEL boundary is significantly reduced. MPEL Boundary 10.83 ft for 12 ant 9.16 ft for 10 ant Center Line of Aircraft Radome Antenna Page ii Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 GENERAL PRECAUTIONS Airborne weather radar should be operated on the ground only by qualified personnel. Installed airborne radar should not be operated while the aircraft is in a hanger or other enclosure unless the radar transmitter is not operating, or the energy is directed toward an absorption shield which dissipates the radio frequency energy. Otherwise, radiation within the enclosure can be reflected throughout the area. BODY DAMAGE To prevent possible human body damage, the following precautions should be taken:
1. Personnel should never stand nearby and in front of a radar antenna which is transmitting. When the antenna is not scanning, the danger increases. 2. The recommended safe distance which is established above should be followed. The distance from any person to the radar should be greater than that distance. 3. Personnel should be advised to avoid the end of an open waveguide unless the radar is turned off. 4. Personnel should be advised to avoid looking into a waveguide, or into the open end of a coaxial connector or line connector to a radar transmitter output, as severe eye damage may result. 5. Personnel should be advised that when high power radar transmitters are operated out of their protective cases, X-rays may be emitted. Stray X-rays may emanate from the glass envelope type pulser, oscillator, clipper, or rectifier tubes, as well as magnetrons. COMBUSTIBLE MATERIALS To prevent possible fuel ignition, an installed airborne weather radar should not be operated while an aircraft is being refueled or defueled. GWX 68 Installation Manual 190-00286-01 Page iii Preliminary Revision 1 TABLE OF CONTENTS PARAGRAPH PAGE 1 GENERAL DESCRIPTION..............................................................................................................1-1 1.1 Introduction........................................................................................................................................1-1 1.2 Equipment Description ......................................................................................................................1-1 1.3 Interface Summary.............................................................................................................................1-1 1.4 Technical Specifications....................................................................................................................1-1 1.5 License Requirements........................................................................................................................1-3 1.6 Certification .......................................................................................................................................1-4 1.7 Reference Documents........................................................................................................................1-4 1.8 Limited Warranty...............................................................................................................................1-5 2 INSTALLATION OVERVIEW ........................................................................................................2-1 2.1 Introduction........................................................................................................................................2-1 2.2 Installation Materials .........................................................................................................................2-1 2.3 Installation Considerations ................................................................................................................2-1 2.4 Cabling and Wiring............................................................................................................................2-2 2.5 Cooling Requirements .......................................................................................................................2-2 2.6 Mounting Requirements ....................................................................................................................2-2 3 INSTALLATION PROCEDURE......................................................................................................3-1 3.1 Unpacking Unit..................................................................................................................................3-1 3.2 Wiring Harness Installation ...............................................................................................................3-1 3.3 Backshell Assemblies and D-Subminiature Connectors....................................................................3-2 3.4 Unit Installation ...............................................................................................................................3-10 3.5 Post Installation Configuration & Checkout....................................................................................3-10 3.6 Continued Airworthiness .................................................................................................................3-10 4 SYSTEM INTERCONNECTS..........................................................................................................4-1 4.1 Pin Function List................................................................................................................................4-1 4.2 Power .................................................................................................................................................4-2 4.3 Serial Data .........................................................................................................................................4-3 4.4 Configuration.....................................................................................................................................4-3 4.5 Auto Pilot...........................................................................................................................................4-3 APPENDIX A: OUTLINE & INSTALLATION DRAWINGS..............................................................A-1 APPENDIX B: INTERCONNECT EXAMPLE....................................................................................... B-1 Page iv Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 LIST OF ILLUSTRATIONS FIGURE PAGE 3-1 Shield Block Install onto Backshell Connector Assembly ................................................................3-3 3-2 Shielded Cable Preparation................................................................................................................3-4 3-3 Daisy Chain Method for Shield Termination.....................................................................................3-7 3-4 Parallel Shield Termination ...............................................................................................................3-8 3-5 Configuration Module Installation.....................................................................................................3-9 A-1 GWX 68 Outline Drawing................................................................................................................A-1 B-1 GWX 68 Typical G1000 Interconnect Wiring Diagram................................................................... B-1 B-2 GWX 68 Typical MX20 Interconnect Wiring Diagram ................................................................... B-3 B-3 GWX 68 Analog Stabilization Interconnect Wiring Diagram.......................................................... B-5 B-4 GWX 68 AHRS Stabilization Interconnect Wiring Digram............................................................. B-7 LIST OF TABLES TABLE PAGE 3-1 Pin Contact Part Numbers..................................................................................................................3-1 3-2 Recommended Crimp Tools ..............................................................................................................3-1 3-3 Backshell Assembly...........................................................................................................................3-2 3-4 Shield Block Components .................................................................................................................3-3 3-5 Shielded Cable Preparation................................................................................................................3-4 3-6 Configuration Module Kit 011-00979-00.......................................................................................3-8 3-7 Configuration Module Wire Color Reference Chart..........................................................................3-9 GWX 68 Installation Manual 190-00286-01 Page v Preliminary Revision 1 GWX 68 HARDWARE MOD LEVEL HISTORY The following table identifies hardware modification (Mod) Levels for the GWX 68. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using their Garmin-provided user name and password. MOD LEVEL SERVICE BULLETIN NUMBER SERVICE BULLETIN DATE PURPOSE OF MODIFICATION Page vi Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 1 GENERAL DESCRIPTION Introduction 1.1 This manual presents mechanical and electrical installation requirements for installing the GWX 68 Airborne Weather Radar. NOTE The ability of a weather radar system to accurately display weather returns is highly dependent upon the quality of the radome and its Transmission Efficiency. The specified performance of the GWX 68 Airborne Weather Radar can be achieved when installed behind a DO-213 Class A Radome within the RF window defined as +-45 degrees from dead ahead in azimuth and +-15 degrees from dead ahead in elevation. Refer to RTCA document DO-213 Class A for minimum operational performance standards for nose mounted radomes. Equipment Description 1.2 The GWX 68 Airborne Weather Radar is a microprocessor-based Line Replaceable Unit (LRU) that outputs weather radar data to an external MFD. The GWX 68 communicates with other LRUs via ARINC 429/453 and/or Ethernet high speed data bus (HSDB). CAUTION The operation of ground-based cellular telephones or other ground-based cellular devices aboard aircraft while airborne is prohibited by FCC rules. Due to the potential for interference with onboard systems, the operation of ground-based cellular communication devices while onboard an aircraft that is on the ground is subject to FAA regulations 14 CFR 91.21. FCC regulation 47 CFR 22.925 prohibits airborne operation of ground-based cellular telephones installed in or carried aboard aircraft. Ground-based cellular telephones must not be operated aboard any aircraft while the aircraft is off the ground. When any aircraft leaves the ground, all ground-based cellular telephones on board that aircraft must be turned off. Ground-based cellular telephones that are on, even in a monitoring state, can disrupt GPS performance. Interface Summary 1.3 The GWX 68 is designed as an open architecture system that uses typical ARINC 429, ARINC 453, and Ethernet communications interfaces. 1.4 Technical Specifications 1.4.1 Environmental Qualification Form It is the responsibility of the installing agency to obtain the latest revision of the GWX 68 Environmental Qualification Form. This form is available directly from Garmin under the following part number:
GWX 68 Environmental Qualification Form, Garmin part number 005-00171-00 To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site (www.garmin.com). GWX 68 Installation Manual 190-00286-01 Page 1-1 Preliminary Revision 1 1.4.2 Physical Characteristics Characteristics Specifications Unit Size Unit weight See Figure A-1. GWX 68 Outline Drawing 10" 9.0 lbs (4.08 kg) 12" 9.1 lbs (4.13 kg) 1.4.3 General Specifications The table below contains general environmental specifications. For detailed specifications, see the Environmental Qualification Form (005-00171-00). Characteristics Operating Temperature Range Humidity Altitude Range Specifications
-55C to +70C. For more details see Environmental Qualification Form. 95% non-condensing
-1,500 ft to 50,000 ft 1.4.4 Performance Specifications Characteristics Display Colors Selectable Ranges Weather Avoidance Range Performance Index Rx Sensitivity Manual Gain Antenna Beamwidth Magnetron Power Pulse Width Scan Angle Scan Centerline Scan Rate Manual Tilt Stabilization Altitude STC Extended STC Interface 2.5, 5, 10, 20, 40, 80, 160, 320nm Specifications 4 Colors 305nm w/ 12 Ant. 270nm w/ 10 Ant. 213dB w/ 12 Ant. 210dB w/ 10 Ant.
-110 dBm MDS
+12 to 64dB 7.8 w/ 12 Ant. 9.0 w/ 10 Ant. 6.5kW nominal 5kW minimum 1 or 4 S Pilot adjustable 12 looks/minute 15 Pilot adjustable 20, 40, 60 or 90 30 combined pitch and roll 50k Ft unpressurized Effective to 80nm 80nm to 320nm Garmin HSDB/ARINC 429/ARINC 453 Page 1-2 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 1.4.5 Power Requirements Characteristics Input Voltage Range Input Current Specifications 14/28 Vdc See the Environmental Qualification Form for details on surge ratings and minimum/maximum operating voltages. 2A @ 28V, maximum 1.5 License Requirements The Telecommunications Act of 1996, effective February 8, 1996, provides the FCC discretion to eliminate radio station license requirements for aircraft and ships. The GWX 68 installation must comply with current transmitter licensing requirements. To find out the specific details on whether a particular installation is exempt from licensing, please visit the FCC web site http://wireless.fcc.gov/aviation. If an aircraft license is required, make application for a license on FCC form 404, Application for Aircraft Radio Station License. The FCC also has a fax-on-demand service to provide forms by fax. The GWX 68 owner accepts all responsibility for obtaining the proper licensing before using the transponder. CAUTION The transmitter in this equipment is guaranteed to meet Federal Communications Commission acceptance over the specified operating temperature range. Modifications to Garmin equipment not expressly approved by Garmin could invalidate the license and make it unlawful to operate the equipment. GWX 68 Installation Manual 190-00286-01 Page 1-3 Preliminary Revision 1 1.6 Certification The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. At the time of publication, installations of this TSO approved article are only approved when installed in an aircraft as part of a Garmin G1000 system. 1.6.1 TSO/ETSO Compliance TSO-C63c Class 7 1.7 Reference Documents The following publications are sources of additional information for installing the GWX 68. Before installing the GWX 68, the technician should read all referenced materials along with this manual. Part Number 190-00303-00 560-1025-09 Document G1000 System Installation Manual MX20 Multi-Function Display Installaltion Manual Page 1-4 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 1.8 Limited Warranty This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident or unauthorized alteration or repairs. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you. Garmin retains the exclusive right to repair or replace the unit or software or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, call Garmin Customer Service at one of the numbers shown below. Products sold through online auctions are not eligible for 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, U.S.A. Phone: 913/397.8200 FAX:
913/397.8282 Garmin (Europe) Ltd. Unit 5, The Quadrangle, Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. Phone: 44/0870.851241 FAX:
44/0870.851251 GWX 68 Installation Manual 190-00286-01 Page 1-5 Preliminary Revision 1 This page intentionally left blank Page 1-6 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 2 INSTALLATION OVERVIEW Introduction 2.1 This section provides hardware equipment information for installing the GWX 68, related hardware, and antennas. Installation of the GWX 68 should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The final installation must meet the requirements of FAA AC 43.13-1B and AC 43.13-2A. 2.2 The GWX 68 is available under the following part number:
Installation Materials Item GWX 68 Unit Only, (011-00883-00) GWX 68 Standard, (011-00883-00) *
*Includes installation kit (011-01114-00). Catalog P/N 010-00299-00 010-00300-00 Antenna Considerations Installation Considerations 2.3 Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are required for installation of the GWX 68. 2.3.1 Antenna installations on pressurized cabin aircraft require FAA approved installation design and engineering substantiation data whenever such antenna installations incorporate alteration (penetration) of the cabin pressure vessel by connector holes and/or mounting arrangements. For needed engineering support pertaining to the design and approval of such pressurized aircraft antenna installations, it is recommended that the installer proceed according to any of the following listed alternatives:
1. Obtain approved antenna installation design data from the aircraft manufacturer. 2. Obtain an FAA approved STC, pertaining to, and valid for the antenna installation. 3. Contact the FAA Aircraft Certification Office in the appropriate Region and request identification of FAA Designated Engineering Representatives (DERs) who are authorized to prepare and approve the required antenna installation engineering data. 4. Obtain FAA Advisory Circular AC-183C and identify a DER from the roster of individuals in it. 5. Contact an aviation industry organization such as the Aircraft Electronics Association for assistance. GWX 68 Installation Manual 190-00286-01 Page 2-1 Preliminary Revision 1 Cabling & Wiring 2.4 Use AWG #24 or larger wire for all connections unless otherwise specified by the aircraft manufacturer or Garmin. The standard pin contacts supplied in the connector kit are compatible with up to AWG #22 wire. In cases where some installations have more than one unit sharing a common circuit breaker, sizing and wire gauge is based on aircraft circuit breaker layout, length of wiring, current draw of units, and internal unit protection characteristics. Do not attempt to combine more than one unit on the same circuit breaker unless it is specified on aircraft manufacturer approved drawings. In these cases, a larger gauge wire such as AWG #18 or #16 may be needed for power connections. The provided connector kit supplies extended barrel contacts for AWG #16 and #18 wire, if required. Special thin-wall heat shrink tubing is also provided to insulate the extended barrels inside the backshell. If using AWG #16 or #18 barrel contacts, ensure that no two contacts are mounted directly adjacent to each other. This minimizes the risk of contacts touching and shorting to adjacent pins and to ground. Ensure that routing of the wiring does not come in contact with sources of heat, RF or EMI interference. Check that there is ample space for the cabling and mating connectors. Avoid sharp bends in cabling and routing near aircraft control cables. 2.5 The GWX 68 does not have provisions for attaching cooling air and does not generate an excessive amount of heat during typical operations, however thermal characteristics of the installation should always be assessed. An undesirable thermal condition could be created due to the units own internal power dissipation combined with restricted ventilation, or due to heat generated by adjacent equipment. Limiting thermal build up, by means of fan or natural convection is always good practice and recommended to increase the product life. 2.6 Mounting Requirements The GWX 68 mounting surface must be capable of providing structural support and electrical bond to the aircraft to minimize radiated EMI and provide protection from High-Intensity Radiation Fields (HIRF). Cooling Requirements Page 2-2 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 3 INSTALLATION PROCEDURE 3.1 Unpacking Unit Carefully unpack the equipment and make a visual inspection of the unit for evidence of damage incurred during shipment. If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has authorized the claim. Retain the original shipping containers for storage. If the original containers are not available, a separate cardboard container should be prepared that is large enough to accommodate sufficient packing material to prevent movement of the item within the container. 3.2 Wiring Harness Installation Allow adequate space for installation of cables, connectors, and strain relief as necessary. The installer shall supply and fabricate all of the cables. All wiring must be in accordance with FAA AC 43.13-1B. All electrical connections are made through a 44-pin D subminiature connector. Section 4 defines the electrical characteristics of all input and output signals. Required connectors and associated hardware are supplied with the connector kit. See Appendix C for examples of interconnect wiring diagrams. Construct the actual harnesses in accordance with aircraft manufacturer authorized interconnect standards. Table 3-1. Pin Contact Part Numbers Manufacturer Garmin P/N Military P/N AMP Positronic ITT Cannon 16 AWG
(Power Only) 336-00044-01 N/A N/A N/A N/A 44 pin D-Subminiature connector (P400) 18 AWG
(Power Only) 336-00044-00 N/A N/A N/A N/A 20 AWG 336-00044-02 N/A N/A N/A N/A 22-28 AWG 336-00021-00 M39029/58-360 204370-2 MC8522D 030-2042-000 Table 3-2. Recommended Crimp Tools 16, 18 & 20 AWG Positioner Manufacturer Hand Crimping Tool Military P/N Positronic ITT Cannon AMP Daniels Astro M22520/2-01 9507 995-0001-584 601966-1 AFM8 615717 N/A 9502-11 N/A N/A K774 N/A Insertion/
Extraction Tool
(note 2) M81969/1-04 M81969/1-04 N/A 91067-1 M81969/1-04 M81969/1-04 22-28 AWG Positioner Insertion/
Extraction Tool M22520/2-09 9502-3 995-0001-739 601966-6 K42 615725 M81969/1-04 M81969/1-04 N/A 91067-1 M81969/1-04 M81969/1-04 GWX 68 Installation Manual 190-00286-01 Page 3-1 Preliminary Revision 1 NOTES 1. Non-Garmin part numbers shown are not maintained by Garmin and consequently are subject to change without notice. 2. Extracting the #16, #18 and #20 contact requires that the expanded wire barrel be cut off from the contact. It may also be necessary to push the pin out from the face of the connector when using an extractor due to the absence of the wire. A new contact must be used when reassembling the connector. 3.3 Backshell Assembly and D-Subminiature Connectors The GWX 68 connector kit (011-01114-00) includes one Garmin backshell assembly. Garmins backshell connectors give the installer the ability to quickly and easily terminate shield grounds at the backshell housing using the Shield Block ground kit. The term D-Sub (D-Subminiature) connectors have a letter D physical shape. D-Sub refers only to the polarized shell that holds the contacts (pins or sockets) in place. Table 3-3 lists Garmin part numbers for the GWX 68 D-Sub Connectors and the Backshell Assembly. Table 3-3. Backshell Assembly Figure Ref Description 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Cast Housing (From Garmin Backshell kit.) Shield block Screw, 4-40 x.250, FLHP100, SS/P, Nylon. Multiple Conductor Shielded Cable
(See Interconnect Diagrams, Appendix C) Shield Termination Braid, Flat (19 20 AWG equivalent, tinned plated copper strands 36 AWG, Circular Mil Area 1000 1300) Shrink Tubing Pins Ring terminal, #8, insulated, 18-22 AWG, 14-16 AWG, 10-12 AWG Screw, PHP, 8-32x.312", Stainless or Cad Plated Steel Split Washer, #8, (.045" compressed thickness) Stainless or Cad-plated steel Flat Washer, #8, .032" thick, .174"ID, .375"
OD, Stainless or Cad Plated Steel Silicon Fusion Tape Strain Relief Screw,4-40x.375,PHP,SS/P,w/Nylon Lid Screw,4-40x.187,FLHP100,SS/P,w/Nylon Garmin P/N 125-00085-00 117-00147-xx 211-63234-08 As Required As Required As Required As Required 336-00021-00 MS25036-149, MS25036-153, MS25036-156 MS51957-42, MS35206-242 MS35338-137, MS35338-42 NAS1149CN832R, NAS1149FN832P 249-00114-00 115-00499-xx 211-60234-10 115-00500-xx 211-63234-06 Page 3-2 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 3.3.1 Shield Block Assembly Procedure The parts for the connector and backshell assembly, GWX68 installations, are listed in Table 3-3 and shown in Figure 3-1. Figure 3-1. Shield Block Install onto Backshell Connector Assembly Table 3-4. Shield Block Components Backshell Assembly Garmin P/N 011-00950-12
(25/44 Pin High Density) Shield Block Garmin P/N 011-01169-01 GWX 68 Installation Manual 190-00286-01 Page 3-3 Preliminary Revision 1 1. Attach the Shield Block(s) (2) to the backshell (1) by inserting the flathead screws (3) through the holes on the Shield Block and threading into the tapped holes on the backshell (1). (See Figure 3-1). The appropriate number of Shield Block kits is included in the GWX 68 connector kit. Table 3-5. Shielded Cable Preparation Float Max 2.5 Ideal Float 2.0 Max 5.5 Window Window Min 3.0 Ideal Window 4.5 Float Min 1.5 Figure 3-2. Shielded Cable Preparation 2. At one end of a shielded cable (4) measure back a distance between Window Min to Window Max (Table 3-5) and cut a window (max size 0.35) in the jacket to expose the shield. (See Figure 3-2). Use caution when cutting the jacket to avoid damaging the individual braids of the shield. When dealing with a densely populated connector with many cables it may prove beneficial to stagger the windows throughout the Window Min to Window Max range. If staggering is not needed the Ideal Window length is recommended. Tools needed to Accomplish the Window Cut:
Coaxial Cable Stripper Thermal Stripper Sharp Razor Blade 3. Connect a Flat Braid (6) to the shield exposed through the window of the prepared cable assembly
(4). The Flat Braid goes out the front of the termination towards the connector. Do not allow wires to exit the rear of the termination and loop back towards the connector. (See Figure 3-2). Make this connection using an approved shield termination technique. Refer to FAA Advisory Circular AC 43.13 as a reference for termination techniques. Page 3-4 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 Preferred Method, Solder Sleeves:
Slide a solder sleeve (5) onto the prepared cable assembly (4) and connect the Flat Braid (6) to the shield using a heat gun approved for use with solder sleeves. It may be easier to use a solder sleeve with a pre-
installed Flat Braid versus having to cut a length of Flat Braid to be used. The chosen size of solder sleeve must accommodate both the number of conductors present in the cable and the Flat Braid (6) to be attached. NOTE Solder Sleeves with pre-installed Flat Braid: A preferred solder sleeve is the Raychem S03 Series with the thermochromic temperature indicator. These solder sleeves come with a pre-installed braid and effectively take the place of items 5 and 6. For detailed instructions on product use, refer to Raychem installation procedure RCPS 100-70. Raychem Recommended Heating Tools:
HL1802E AA-400 Super Heater CV-1981 MiniRay IR-1759 Individual Solder Sleeves and Flat Braid Solder Sleeves:
Reference the following MIL-Specs for general solder sleeves:
(M83519/1-1, M83519/1-2, M83519/1-3, M83519/1-4, M83519/1-5). Flat Braid:
If the preferred Raychem sleeves are not being used, the individual flat braid selected should conform to ASTMB33 for tinned copper and be made up of 36 AWG strands to form an approximately 19-20 AWG equivalent flat braid. A circular mil area range of 1000 to 1300 is required. The number of individual strands in each braid bundle is not specified. NOTE Flat Braid as opposed to insulated wire is specified in order to insure continuing airworthiness by allowing for visual inspection of the conductor. GWX 68 Installation Manual 190-00286-01 Page 3-5 Preliminary Revision 1 Secondary Method, Heat Shrink instead of Solder Sleeves:
Solder a Flat Braid (6) to the shield exposed through the window of the prepared cable assembly (4). Ensure a solid electrical connection through the use of acceptable soldering practices. Use care to avoid applying excessive heat that burns through the insulation of the center conductors and shorts the shield to the signal wire. Slide a minimum 0.75 of Teflon heat shrinkable tubing (5) onto the prepared wire assembly and shrink using a heat gun. The chosen size of heat shrinkage tubing must accommodate both the number of conductors present in the cable and the Flat Braid (6) to be attached. 4. At the same end of the shielded cable (4) and ahead of the previous shield termination, strip back Float Min to Float Max (Table 3-5) length of jacket and shield to expose the insulated center conductors. (See Figure 3-2). It may be best to build the Ideal Float length optimally. Preferred Method:
The jacket and shield should be cut off at the same point so no shield is exposed. Slide 0.75 minimum of Teflon heat shrinkable tubing (7) onto the cable and use a heat gun to shrink the tubing. The chosen size of heat shrinkage tubing must accommodate the number of conductors present in the cable Secondary Method:
Leave a max 0.35 of shield extending past the jacket. Fold this 0.35 of shield back over the jacket. Slide a solder sleeve (7) over the end of the cable and use a heat gun approved for solder sleeves to secure the connection. The chosen size of solder sleeve must accommodate the number of conductors present in the cable. 5. Strip back 1/8 of insulation and crimp a pin (8) to each of the conductors in the shielded cable. 6. Insert newly crimped pins and wires into the appropriate connector housing location as specified by the installation wiring diagrams. 7. Cut the Flat Braid (6) to a length with the addition of a ring terminal that will reach one of the tapped holes of the Shield Block (2). (See Figure 3-1). An appropriate amount of excess length without looping should be given to the Flat Braid (6) to allow it to move freely with the wire bundle. Note that the maximum distance from the backshell allowed for the window splice should keep the Flat Braid (6) to a worst case length of approximately 4. Page 3-6 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 8. Guidelines for terminating the newly cutoff Flat Braid(s) (item 6) with insulated ring terminals (9):
Each tapped hole on the Shield Block (2) may accommodate only two ring terminals (9). It is preferred that only two Flat Braids (6) be terminated per ring terminal. Two Flat Braids per ring terminal will necessitate the use of a Ring terminal, #8, insulated, 14-16 AWG
(MS25036-153). If only a single Flat Braid is left or if only a single Flat Braid is need for this connector, a Ring terminal, #8, insulated, 18-22 AWG (MS25036-149) can accommodate this single Flat Braid. If more braids exist for this connector than two per ring terminal, it is permissible to terminate three braids per ring terminal. This will necessitate the use of a Ring terminal, #8, insulated, 10-12 AWG (MS25036-156). In rare situations where more braids need to be terminated for this connector than three per ring terminal it is allowable to daisy chain a maximum of two shields together before coming to the ring terminal. (See Figure 3-3). Figure 3-3: Daisy Chain Method for Shield Termination GWX 68 Installation Manual 190-00286-01 Page 3-7 Preliminary Revision 1 9. Repeat steps 2 through 8 as needed for the remaining shielded cables. 10. Terminate the ring terminals to the Shield Block (2) by placing items on the Pan Head Screw (10) in the following order: Split Washer (11), Flat Washer (12), first Ring Terminal, second Ring Terminal if needed, before finally inserting the screw into the tapped holes on the Shield Block. Do not violate the guidelines presented in Step 8 regarding ring terminals. 11. It is recommended to wrap the cable bundle with Silicone Fusion Tape (13) (GPN: 249-00114-00 or a similar version) at the point where the backshell strain relief and cast housing will contact the cable bundle. Note: Choosing to use this tape is at the discretion of the installer. 12. Place the smooth side of the backshell strain relief (14) across the cable bundle and secure using the three screws (15). Warning: Placing the grooved side of the strain relief across the cable bundle may risk damage to wires. 13. Attach the cover (16) to the backshell (1) using two screws (17). 9 7 5 6 Figure 3-4: Parallel Shield Termination 3.3.2 Configuration Module Installaltion (MX20 only) Table 3-6 lists part numbers for the Configuration Module Kit. Table 3-6. Configuration Module Kit 011-00979-00 Item Description Configuration Module Cable Crimp Pins Spacer PCB Board Assembly w/EEPROM 4-Conductor Harness
#22 AWG (HD) Spacer, Config Module Garmin P/N 012-00605-00 325-00122-00 336-00021-00 213-00043-00 Page 3-8 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 3.3.3 Configuration Module Assembly Procedure (MX20 only) Table 3-7. Configuration Module Wire Color Reference Chart Color Black Red Yellow White Function Ground Vcc Data Clock J400 Pin 1 17 16 31 1. Crimp pins (4) onto each wire of the four-conductor wire harness (3). Strip 1/8 of insulation from each wire prior to crimping. 2. Insert newly crimped pins and wires (3, 4) into the appropriate connector housing (5) location shown in the figure below. 3. Apply the spacer (2) by wrapping it around the PCB Board (1) making sure to insert the plastic connector mounted on the board into the hole provided in the spacer. 4. Plug the four-conductor wire harness (3) into the connector on the PCB Board (1). 5. Insert into the backshell (6) recess, PCB Board (1) with pad (2) in position. 6. Attach cover (7) to backshell (6) using screws (8). Figure 3-5. Configuration Module Installation GWX 68 Installation Manual 190-00286-01 Page 3-9 Preliminary Revision 1 3.4 Unit Installation The GWX 68 is designed to be rigidly mounted in the nose section of the aircraft. If the nose section is not accessible, pod mounting is possible. The bulk head or antenna mounting plate must be very close to perpendicular to the aircraft center line. The selected location must have adequate clearance for the full antenna sweep and tilt range. See Appendix A for outline and installation drawings. The nose section does not need to be pressurized. NOTE It is crucial to the performance of the GWX 68 weather radar system that care be taken in alignment of the GWX 68 unit with respect to the aircraft. 1. Refer to Figure A-1 mount the GWX 68 using the hardware provided. 2. Assemble the GWX 68 connector kit, see Section 3.3. 3. Check unit for clearance in all extreme positions. 4. Ensure wiring harness is routed in such a way that it can not be struck by or interfere with the unit movement through the full sweep and tilt range. 3.5 Post Installation Configuration & Checkout NOTE The GWX 68 does not provide valid outputs until the aircraft post installation configuration procedures are completed. When installed as part of the G1000 integrated cockpit system, the GWX 68 must have FAA approved configuration data. Configuration data is loaded to the GWX 68 from an aircraft-specific G1000 Software Loader Card. Settings are predetermined for a specific aircraft and are typically contained within the file named TBD. The GDU 1040 PFD serves as the graphics user interface to the installer configuring the system. For basic configuration information, refer to the G1000 Line Maintenance and Configuration Manual, Garmin part number 190-00303-04. For actual aircraft installation/checkout, use only aircraft manufacturer approved checkout procedures. For GWX 68 installations operating with a Garmin MX20, refer to MX20 Installation Manual, 560-1025-09. 3.6 Continued Airworthiness For sample Instructions for Continued Airworthiness (ICA) for the GWX 68 installed as part of the G1000 integrated cockpit system, see the G1000 ICA Sample, Garmin part number 190-00303-07. Other than for regulatory periodic functional checks, maintenance on the GWX 68 is on condition only. Refer to the G1000 Line Maintenance and Configuration Manual, Garmin part number 190-00303-04. Page 3-10 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 4 SYSTEM INTERCONNECTS 4.1 Pin Function List 4.1.1 P400 View of J400 connector from back of unit 15 12 13 14 10 11 1 2 3 4 5 6 7 8 9 30 29 28 27 26 25 24 23 22 21 20 19 18 17 16 44 43 42 41 40 39 38 37 36 35 34 33 32 31 Pin 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 Pin Name CONFIG MODULE GROUND RESERVED RESERVED ARINC 453 OUT A ARINC 453 OUT B RESERVED AIRCRAFT POWER 1 RESERVED AIRCRAFT POWER 1 AIRCRAFT POWER 2 RESERVED AIRCRAFT POWER 2 POWER GROUND RESERVED POWER GROUND CONFIG MODULE DATA CONFIG MODULE POWER ROLL ATTITUDE HI ROLL ATTITUDE LO 26 VAC GYRO REF LO 26 VAC GYRO REF HI ARINC 429 IN 2 A ARINC 429 IN 2 B RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED CONFIG MODULE CLOCK PITCH ATTITUDE HI PITCH ATTITUDE LO ETHERNET IN A ETHERNET IN B I/O
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Out Out
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In
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In In
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In
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I/O Out In In In In In In
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Out In In In In GWX 68 Installation Manual 190-00286-01 Page 4-1 Preliminary Revision 1 Connector P400, continued Pin Name ETHERNET OUT A ETHERNET OUT B ARINC 429 IN 1 A ARINC 429 IN 1 B RESERVED RESERVED RESERVED RESERVED RADAR REMOTE POWER OFF Pin 36 37 38 39 40 41 42 43 44 I/O Out Out In In
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In 4.2 Power 4.2.1 Power Functions This section covers the power input requirements. 4.2.1.1 Aircraft Power Pin Name AIRCRAFT POWER 1 AIRCRAFT POWER 1 AIRCRAFT POWER 2 AIRCRAFT POWER 2 POWER GROUND POWER GROUND Connector P400 P400 P400 P400 P400 P400 Pin 7 9 10 12 13 15 I/O In In In In
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Pins 7 and 9 of P400 are internally connected to form AIRCRAFT POWER 1. Pins 10 and 12 of P400 are internally connected to form AIRCRAFT POWER 2. AIRCRAFT POWER 1 and AIRCRAFT POWER 2 are diode ORed to provide power redundancy. 4.2.1.2 Remote On/Off Pin Name RADAR REMOTE POWER OFF Connector P400 Pin 44 I/O In For G1000 installations RADAR REMOTE POWER OFF must be grounded to pin 15 of P400 (POWER GROUND). Page 4-2 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 4.3 Serial Data 4.3.1 Serial Data Electrical Characteristics 4.3.1.1 ARINC 429/453 Pin Name ARINC 453 OUT A ARINC 453 OUT B ARINC 429 IN 1 A ARINC 429 IN 1 B ARINC 429 IN 2 A ARINC 429 IN 2 B 4.3.1.2 Ethernet HSDB Pin Name ETHERNET IN A ETHERNET IN B ETHERNET OUT A ETHERNET OUT B Connector P400 P400 P400 P400 P400 P400 Connector P400 P400 P400 P400 Pin 4 5 38 39 22 23 Pin 34 35 36 37 I/O Out Out In In In In I/O In In Out Out The Ethernet high speed data bus (HSDB) meets the hardware aspects of IEEE standard 802.3 for 10 base T Ethernet communications. 4.4 Configuration 4.4.1 Configuration Module Pin Name CONFIG MODULE GROUND CONFIG MODULE DATA CONFIG MODULE POWER CONFIG MODULE CLOCK 4.5 Auto Pilot 4.5.1 Flight Instruments Pin Name ROLL ATTITUDE HI ROLL ATTITUDE LO PITCH ATTITUDE HI PITCH ATTITUDE LO Connector P400 P400 P400 P400 Connector P400 P400 P400 P400 Pin 1 16 17 31 Pin 18 19 32 33 I/O
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I/O Out Out I/O In In In In Inputs pitch and roll attitude information from AFCS. Expected nominal input voltage is 50mV/degree. GWX 68 Installation Manual 190-00286-01 Page 4-3 Preliminary Revision 1 4.5.2 26 Volt AC Reference Pin Name 26 VAC GYRO REF LO 26 VAC GYRO REF HI Expected nominal input voltage is 400 Hz, 26VRMS. Connector P400 P400 Pin 20 21 I/O In In Page 4-4 Preliminary Revision 1 GWX 68 Installation Manual 190-00286-01 APPENDIX A OUTLINE & INSTALLATION DRAWINGS MAX. AZIMUTH 45 ANGLE PRELIMINARY 4.600.022 116.840.56 AZIMUTH AXIS 6.815.064 173.091.63 RIGHT ANGLE CONNECTOR BULKHEAD MOUNTING SURFACE 4.951.029 125.750.74 TILT AXIS 10.00 254.0 4X 211-64214-22 1/4-28 SOCKET HEAD CAP SCREWS MAX SPHERICAL RADIUS R6.548 166.32 12" ANTENNA
.25 6.4 6.750 171.45 3.375 85.73 UP 4X .265 6.73 THRU 2.47 62.7
.30 7.6 3.312 84.12 6.624 168.25 NOTES:
1. DIMENSIONS: INCHES[mm]
2. 12" ANTENNA SHOWN MAX. TILT 30 ANGLE MAX SPHERICAL RADIUS R5.530 140.46 10" ANTENNA GWX 68 Installation Manual 190-00286-01 Figure A-1. GWX 68 Outline Drawing Page A-1 (Page A-2 blank) Preliminary Revision 1 APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual 190-00286-01 Figure B-1. GWX 68 Typical G1000 Interconnect Wiring Diagram Page B-1 (Page B-2 blank) Preliminary Revision 1 APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual 190-00286-01 Figure B-2. GWX 68 Typical MX20 Interconnect Wiring Diagram Page B-3 (Page B-4 blank) Preliminary Revision 1 APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual 190-00286-01 Figure B-3. GWX 68 Analog Stabilization Interconnect Wiring Diagram Page B-5 (Page B-6 blank) Preliminary Revision 1 APPENDIX B INTERCONNECT DRAWINGS GWX 68 Installation Manual 190-00286-01 Figure B-4. GWX 68 AHRS Stabilization Interconnect Wiring Diagram Page B-7 (Page B-8 blank) Preliminary Revision 1
1 | PILOT MANUAL | Users Manual | 3.40 MiB |
G1000TM hazard avoidance pilots guide for the Cessna Citation Mustang Preliminary 190-00498-00_0A.indd 1 3/1/2005 10:33:38 AM Revision Date of Revision Revision Page Range Description Draft 03/01/05 7-1 7-53 Initial release. Record of Revisions Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 2 3/1/2005 10:33:38 AM Preliminary WEATHER 7.1 WEATHER CAUTION: GDL 69A NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays and relative age of the data that can be received, NEXRAD weather data should not be used for short-range avoidance of weather. WARNING: Use of any GDL 69A Weather Product for thunderstorm penetration is prohibited. Weather information provided by the GDL 69 is approved only for weather avoidance, not penetration. This document describes the Hazard Avoidance features of the G1000 system. The main hazards to ight safety are ying in or near weather, ying in close proximity to the terrain and other ight trafc in close proximity. The information contained in this section assumes un-
derstanding of the G1000 Multi Function Display. This section is divided into groups as follows:
Weather GDL 69A (XM Weather) GWX 68 WX 500 Stormscope TAWS/Terrain Terrain Proximity TAWS (Terrain Awareness Warning System) Trafc TIS (Trafc Information System) TAS (Trafc Advisory System) 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-1 190-00498-00_0A.indd 1 3/1/2005 10:33:39 AM Preliminary WEATHER GDL 69A WEATHER AND DIGITAL Radio IDs AUDIO ENTERTAINMENT The GDL 69A is a remote sensor that is capable of re-
ceiving XM Weather and displaying it on the G1000 Multi Function Display and the Primary Flight Display Inset Map. The GDL 69A is also capable of receiving XM Radio Services. XM Weather and XM Radio operate in the S-
band frequency range to provide continuous uplink capa-
bilities at any altitude throughout North America. The GDL 69A are shipped with a Data Radio ID and an Audio Radio ID. You must obtain the Radio IDs of your receiver(s) before subscribing to XM services. The IDs are attached to the XM Satellite Radio Activation Instructions sheet included with the unit. They are also printed on a label on the back of the unit and are displayed on the XM Information Page. Contact the installer if you are unable to locate the Radio IDs. Activating XM Radio Services NOTE: Before the GDL 69A can be used, the unit must be activated by XM Satellite Radio. The XM Satellite Radio Activation Instruction Sheet con-
tains important information required to initiate XM Satellite Radio Subscription for the GDL 69A. This sheet was given to the aircraft owner at the time of delivery. NOTE: Refer to the G1000 Option pilots guide for information on the XM entertainment radio segment of the GDL 69A. To activate the XM Radio Weather Service:
1. Turn the large FMS knob to select the Auxiliary Page Group. Turn the small FMS knob to display the AUX - XM Page. 2. Press the INFO softkey to display the XM Information Page. 3. Contact XM Satellite Radio through the Internet or by telephone. Follow the directions provided by XM Satellite Radio. 4. Verify that the desired services are activated and press the DONE softkey. 5. Turn the large FMS knob to highlight YES or NO. Press the ENT key to complete activation. 7-2 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 2 3/1/2005 10:33:39 AM Preliminary WEATHER Audio Radio ID DONE Softkey Data Radio ID Weather Products INFO Softkey Figure 7.1.1 XM Information Page 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-3 190-00498-00_0A.indd 3 3/1/2005 10:33:39 AM Preliminary WEATHER GDL 69 WEATHER Flight Information Services (FIS) weather information provided by the GDL 69 is displayed on the following MFD Maps and Pages:
Navigation Map Page (NEXRAD and XM Light-
ning only) Complete GDL 69 capabilities include:
Graphical NEXRAD Data (NEXRAD) Graphical METAR Data (METAR) Textual METAR Data Textual Terminal Aerodrome Forecasts (TAF) Weather Data Link Page (complete GDL 69 capa-
City Forecast Data bility) Nearest Pages (NEXRAD and XM Lightning only) Airport Information Page (NEXRAD and XM Lightning only) Flight Planning Maps (NEXRAD and XM Light-
ning only) Graphical Wind Data (WIND) Graphical Echo Tops (ECHO TOP) Graphical Cloud Tops (CLD TOP) Graphical Lightning Strikes (XM LTNG) Graphical Storm Cell Movement (CELL MOV) AUX - Trip Planning Map (NEXRAD and XM NEXRAD Radar Coverage (displayed with Lightning only) WPT - Weather Information Page - part of the WPT - Airport Information Page (METAR and TAF information only) FIS weather information is also displayed on the Pri-
mary Flight Display Inset Map. See the G1000 PFD Pilots Guide for more information. NOTE: Temporary Flight Restrictions (TFRs) are displayed on all pages. Cell Movement is always displayed with NEXRAD data. NEXRAD data) SIGMETs/AIRMETs (SIG/AIR) Surface Analysis including City Forecasts (SFC) County Warnings (COUNTY) Freezing Levels (FRZ LVL) Hurricane Track (CYCLONE) Temporary Flight Restrictions (TFR) NOTE: FIS (also known as Flight Information Services - Broadcast, or FIS-B) supplies real-time weather information and other ight advisory information for enhanced situational awareness, 24 hours a day, 7 days a week. 7-4 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 4 3/1/2005 10:33:40 AM Preliminary WEATHER Displaying Weather Data on the Navigation Map Page When appropriately congured, the Navigation Map Page displays NEXRAD, Cell Movement, TFRs and XM Lightning data. This capability improves situational awareness, which makes it easier to relate storm activity to airports, navaids, obstacles and other ground references. To display weather data on the Navigation Map Page:
1. 2. Press the MAP softkey. Press the NEXRAD or XM LTNG softkey to dis-
play the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page. Navigation Map Page Weather Control Softkeys The following softkeys control the display of GDL 69 weather data on the Navigation Map Page:
NEXRAD pressing the NEXRAD softkey displays NEXRAD weather and coverage information. The NEXRAD option is mutually exclusive with the TOPO, TERRAIN and STORMSCOPE options. That is, when NEXRAD is activated, TOPO and/or TERRAIN and/or STORMSCOPE are turned off. XM LTNG pressing the XM LTNG softkey displays XM lightning information. XM Lightning is mutu-
ally exclusive with the STORMSCOPE option. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-5 190-00498-00_0A.indd 5 3/1/2005 10:33:40 AM Preliminary WEATHER NEXRAD Weather NEXRAD Storms/Legend Cell Movement Status XM Lightning Status NEXRAD Softkey XM Lightning Softkey Figure 7.1.2 Navigation Map Page Displaying NEXRAD Weather 7-6 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 6 3/1/2005 10:33:40 AM Preliminary WEATHER Figure 7.1.3 Map Setup Options Navigation Map Setup Options The crew can customize the display of GDL 69 weather data on the Navigation Map Page by using the Map Setup Weather Group Options Menu. The following options are available:
NEXRAD DATA - Turns the display of NEXRAD data and radar coverage on or off and selects the desired display range. XM LTNG - Turns the display of XM Lightning on or off and selects the desired display range. NOTE: Stormscope (when installed) and all GDL 69 Weather Products are mutually exclusive. Stormscope is not a GDL 69 Weather Product. CELL MOVEMENT - Turns the display of storm cell movement on or off. The Cell Movement option is only shown when NEXRAD is turned on. NOTE: In Figure 7.1.3, the Stormscope menu options are only shown when the Stormscope unit is installed. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-7 190-00498-00_0A.indd 7 3/1/2005 10:33:41 AM Preliminary WEATHER To customize the Navigation Map Page:
1. On the Navigation Map page, press the Menu key. 2. While the Map Setup selection is highlighted 3. on the Page Menu, press the ENT key. Turn the small FMS knob to display the group selection window. Turn the FMS knob to select the Weather Group and press the ENT key. 4. While the Map Setup menu is displayed, turn the large FMS knob to highlight and move between the product selections. When an item is highlighted, turn the small FMS knob to select the desired option and press the ENT key. Displaying Weather Data on the Nearest Pages In addition to the Navigation Map Page, the Nearest Pages displays Stormscope, NEXRAD and XM Lightning data. Figure 7.1.4 Weather Display on the Nearest NDB Page 7-8 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 8 3/1/2005 10:33:41 AM Preliminary Displaying METAR and TAF on the Airport Information Page METAR and TAF text is displayed on the Airport In-
formation Page when the WX softkey is pressed. Once the WX softkey is pressed the page title changes from WPT - Airport Information to WPT - Weather Infor-
mation. The METAR data is rst displayed in a decoded fashion, then the raw text is displayed. TAF information is only displayed in its raw form. NOTE: METAR is the Aviation Routine Weather Report, generally standard around the world. Temperatures are given in Celsius. The atmo-
spheric pressure is reported in hecto pascals everywhere but the US where it is reported in inches of mercury. Standard temperature and atmospheric pressure are 59 F (15C) and 29.92 in. Hg (1013.2 hPa). 2. 3. WEATHER
`
NOTE: TAF is an airport forecast, generally stan-
dard around the world. TAF forecasts signicant weather changes, temporary changes, probable changes and expected changes in weather condi-
tions. To display METAR and TAF text on the Air-
port Information Page:
1. Turn the large FMS knob to select the WPT Page Group. Turn the small FMS knob to select the Airport Information Page. Press the WX softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-9 190-00498-00_0A.indd 9 3/1/2005 10:33:42 AM Preliminary WEATHER METAR Text TAF Text WX Softkey Figure 7.1.5 METAR and TAF Text Displayed on the Airport (Weather) Information Page 7-10 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 10 3/1/2005 10:33:42 AM Preliminary WEATHER Displaying Weather Data on the AUX Trip Planning Page Map Displaying Weather Data on the Flight Plan Page Maps NEXRAD and XM Lightning Data can be displayed on the AUX - Trip Planning Page Map by pressing the NEXRAD and XM LTNG softkeys. NEXRAD and XM Lightning Data can be displayed on the Flight Plan Page Maps by pressing the NEXRAD and XM LTNG softkeys. Figure 7.1.6 AUX - Trip Planning Page Map Displaying NEXRAD Weather Figure 7.1.7 Stored Flight Plan Page Map Displaying Weather Data 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-11 190-00498-00_0A.indd 11 3/1/2005 10:33:43 AM Preliminary WEATHER Displaying Weather on the Weather Data Link Page The Weather Data Link Page displays all available weather products. The display of the weather data can either be selected by softkeys located at the bottom of the display or through the Weather Data Link Setup menu. To select the Weather Data Link Page:
1. Turn the large FMS knob to select the Map Page Group. Turn the small FMS knob to select the Weather Data Link Page. 2. Figure 7.1.8 Weather Data Link Page 7-12 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 12 3/1/2005 10:33:43 AM Preliminary Weather Data Link Page Softkeys NEXRAD Limitations WEATHER Certain limitations exist regarding the NEXRAD radar displays. Some, but not all, are listed here for the crews awareness:
NEXRAD base reectivity does not provide sufcient information to determine cloud layers or precipita-
tion characteristics (hail vs. rain, etc). NEXRAD base reectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD site cannot depict high altitude storms at close ranges, and has no information about storms directly over the site. The resolution of displayed NEXRAD data is 2 kilo-
meters. Therefore, when zoomed in on the display, each square block is 2 kilometers. The intensity level reected by the square will be the highest level sampled within the 2 kilometer square area. NEXRAD Intensity Colors are used to identify the different NEXRAD echo intensities (reectivity) measured in dBZ (decibels of Z). Reectivity is the amount of transmitted power returned to the radar receiver. Reectivity (designated by the letter Z) covers a wide range of signals (from very weak to very strong). So, a more convenient number for calculations and comparison, a decibel (or logarithmic) scale (dBZ), is used. The dBZ values increase as the strength of the signal returned to the radar increases. The following softkeys perform the GDL 69A weather functions on the Weather Data Link Page:
NEXRAD press the NEXRAD softkey to show NEXRAD weather and radar coverage information
(both are activated at the same time). Composite data from all of the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reectivity from the individual radar sweeps. The display of the information is color-coded to indicate the weather level severity. The update rate is every ve minutes. Refer to the legend for a description of the color code. NOTE: WSR-88D weather surveillance radar or NEXRAD (NEXt generation RADar) is a Dop-
pler radar system that has greatly improved the detection of meteorological events such as thunderstorms, tornadoes and hurricanes. An extensive network of NEXRAD stations provides almost complete radar coverage of the conti-
nental United States, Alaska and Hawaii. The unobstructed range of each NEXRAD is 124 nautical miles. NEXRAD Abnormalities There are possible abnormalities regarding displayed NEXRAD images. Some, but not all, of those include:
Ground Clutter Strobes and spurious radar data Sun strobes, when the radar antenna points directly at the sun Interference from buildings or mountains, which may cause shadows Military aircraft deploy metallic dust which can cause alterations in radar scans 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-13 190-00498-00_0A.indd 13 3/1/2005 10:33:44 AM Preliminary WEATHER ECHO TOP press the ECHO TOP softkey to show RADAR COVERAGE The display of Radar Cover-
the location, elevation and direction the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo. The information is derived from NEXRAD information and indicates the highest altitude at which precipitation is falling. ECHO TOPS and Radar coverage are activated at the same time. ECHO TOPS are mutually exclusive from both NEXRAD and CLOUD TOPS, that is, when ECHO TOPS is activated, NEXRAD and CLOUD TOPS are removed. Refer to the Legend for a descrip-
tion of the ECHO TOPS coding. The update rate is every 7.5 minutes. age is always active when NEXRAD and ECHO TOPS are selected and indicates the currently available NEXRAD Radar coverage and ECHO TOPS areas by showing the area in a grayish-
purple color where information is not being collected. Areas where radar capability exists, but is not active or is off-line, will not be shown as available. Areas where radar coverage is not avail-
able will be shown in grayish-purple. The update rate is every ve minutes. CLD TOP press the CLD TOP softkey to show the cloud top altitude determined from satellite imagery. Refer to the legend for a description of the CLOUD TOPS color coding. The update rate is every 15 minutes. NOTE: Cloud Tops and Echo Tops use the same color scaling to represent altitude. Turning on both products at the same time is not allowed. LTNG pressing the LTNG softkey shows the loca-
tion of cloud-to-ground lightning strikes. The update rate is every ve minutes. NOTE: Strike location falls within a 2 km region. Therefore, the exact location of the strike is not displayed. 7-14 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 14 3/1/2005 10:33:44 AM Preliminary WEATHER NOTE: AIRMETs are broadcast for weather phenomena that potentially affect all aircraft. AIRMET (acronym for AIRmans METeorological information) gives valuable information about the following conditions: moderate icing, mod-
erate turbulence, sustained winds 30 knots or greater at the surface, widespread area with a ceiling of less than 1,000 feet and/or visibility less than 3 miles and extensive obscurement of mountains. These are important to light aircraft, that have limited ight capabilities due to lack of equipment and/or instrumentation. CELL MOV pressing the CELL MOV softkey shows the storm cells identied by the ground-
based system. The movement is depicted by an arrow. The update rate is every 12 minutes. SIG/AIR pressing the SIG/AIR softkey shows SIGMET and AIRMET information to advise the crew of potentially hazardous weather. The advisory covers an area of at least 3,000 square miles at any one time. The update rate is every 12 minutes. NOTE: SIGMETs are broadcasted for hazardous weather that is considered of extreme importance to all aircraft. SIGMETs (acronym for SIGni-
cant METeorological information) warn of the following weather hazards: severe icing, severe and extreme turbulence, dust storms, sandstorms or volcanic ash lowering visibility to less than 3 miles. A Convective SIGMET (WST) is issued for hazardous convective weather (such as torna-
does, thunderstorms, hail) and covers severe or greater turbulence, severe icing and low-level wind shear. A localized SIGMET is a signicant weather condition occurring at a localized geo-
graphical position. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-15 190-00498-00_0A.indd 15 3/1/2005 10:33:44 AM Preliminary WEATHER When enabled, the following AIRMETs can be displayed:
Icing Turbulence IFR conditions Mountain obscuration Surface winds Refer to the legend for a description of the color coding. METAR press the METAR softkey to display METARs (METeorological Aviation Reports). METARS are shown as colored ags at airports providing METAR reports. Refer to the legend for a description of the color code. The update rate is every 12 minutes. LEGEND press the LEGEND softkey to display the Weather Legend Window. Turn the FMS knob to scroll up or down through the legend list. Press the FMS knob or the ENT key to remove the legend display. The Weather Legends Window describes the graphic symbols and color coding of the information for each product that is active. Figure 7.1.9 Weather Legends Window To view the available legends:
1. Press the LEGEND softkey to display the avail-
able legends. 2. Turn either the small or large FMS knob to scroll through the legends if more are available than t in the window. 3. To return to the previous page and remove the legend window, press the LEGEND, ENT, CLR key, or the FMS knob. OR 4. On the Weather Data Link Page, press the LEGEND softkey which displays the Page Menu Options. Turn either the large or small FMS knob to select Weather Legend and press the ENT key. 7-16 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 16 3/1/2005 10:33:45 AM Preliminary MORE WX press the MORE WX softkey to display the following group of softkeys for additional weather control:
FRZ LVL press the FRZ LVL softkey to display contour lines for freezing levels. The update rate is every 12 minutes. WEATHER NOTE: City Forecast and METAR information is only displayed within the installed Aviation Database service area. SFC pressing the SFC softkey for Surface Analysis shows current or forecast conditions. The city forecasts information is combined with the surface conditions. The SFC softkey label changes to reect the forecast time selected. Forecasts are available for intervals of 12, 24, 36 and 48 hours. The update rate is every 12 minutes. NOTE: When no data is shown at a given altitude for any of the weather features, the data for that altitude has not been received or the data is out of date and has been removed from the display. Wait for the next update. The update rate is every 12 minutes. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-17 190-00498-00_0A.indd 17 3/1/2005 10:33:45 AM Preliminary WEATHER WIND press the WIND softkey to show wind speed and direction at a selected altitude from the ground up to 42,000 feet in 3,000 foot increments. The WIND softkey label changes to reect the winds aloft altitude selected. The update rate is every 12 minutes. CYCLONE pressing the CYCLONE softkey shows the current location of cyclones (hurricanes) and their projected track at various time intervals. The update rate is every 12 minutes. COUNTY pressing the COUNTY softkey provides specic public awareness and protection weather warnings for Tornado, Severe Thunderstorm and Flood conditions provided by the National Weather Service (NWS). Refer to the Legend for a description of the county warning icon. The update rate is every 5 minutes. 7-18 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 18 3/1/2005 10:33:45 AM Preliminary Weather Data Link Page Setup The crew can customize the display of XM Weather data on the Weather Data Link Page using the Weather Setup Menu. To customize the display of weather data on the Weather Data Link Page:
1. On the Weather Data Link Page, press the Menu key. 2. While the Weather Setup selection is high-
lighted on the Page Menu, press the ENT key. If necessary, turn the small FMS knob to select Weather Setup and then press the ENT key. 3. While the Weather Data Link Setup Menu is displayed, turn the large FMS knob to high-
light and move between the product selections. Turn the small FMS knob to select an option for each selection and press the ENT key. WEATHER Figure 7.1.10 Weather Data Link Page Menu Map Panning Information-Weather Data Link Page Map panning moves the map beyond its current limits without adjusting the map range. When the panning function is selected by pushing the joystick, a panning arrow ashes on the Weather Data Link Page. Panning over AIRMETs, County Warnings, TFRs, Echo Tops, METARs, SIGMETs and Cell Movement displays text information for the selection. This information is displayed in the same location as the map pointer information on the Navigation Map Page. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-19 190-00498-00_0A.indd 19 3/1/2005 10:33:45 AM Preliminary WEATHER To display information for selected weather products:
1. Push in the joystick to display the panning arrow. 2. Move the joystick to place the panning arrow on AIRMETs, TFRs, METARs or SIGMETs. Press the ENT key to display pertinent information for the selected product. Note that pressing the ENT key when pan-
ning over an AIRMET or a SIGMET displays an information box that gives the actual text of that alert. Panning over an airport with METAR information does not display more information but allows the crew to press the ENT key and select that Airports Information Page and displays the actual text. Pressing the ENT key when panning over a TFR displays TFR specic information for the panned TFR. Panning Information Map Panning Arrow Figure 7.1.11 Panning on the Weather Data Link Page 7-20 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 20 3/1/2005 10:33:46 AM Preliminary WEATHER Weather Product Symbols Figure 7.1.12 depicts the symbol for each weather product (read from left to right). When a weather prod-
uct is active, the product symbol is displayed in the lower right of the screen. NEXRAD Cloud Top/Echo Top XM Lightning Cell Movement SIGMETs/AIRMETs METARs City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 7.1.12 Weather Product Symbols 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-21 190-00498-00_0A.indd 21 3/1/2005 10:33:46 AM Preliminary WEATHER Weather Product Age The times for each of the enabled products are displayed on the right side of the display. Times are based on Zulu times when the data was assembled on the ground, not the time the data was received by the FIS sensor. When the age of a weather product is greater than half of the expiration time, the product time will change from cyan to amber in color. Current weather products use an age stamp, Age: _ _ _ in minutes. Reported (forecasted) weather products use a date/time stamp; _ _/_ _ /_ _:_ _. Weather Product Expires After n Minutes SIGMETs/AIRMETs City Forecasts County Warnings Cyclone Warnings Echo Tops Freezing Levels METARs Lightning NEXRAD Radar Coverage Cell Movement Surface Analysis TFRs Winds Aloft TAFs Clouds Tops 60 60 60 60 30 60 90 30 30 30 30 60 60 60 60 60 7-22 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 22 3/1/2005 10:33:46 AM Preliminary GDL 69 Troubleshooting Although it is the responsibility of the facility that in-
stalled the GDL 69A to correct any hardware problems, the crew can perform some quick troubleshooting steps to nd the possible cause of a failure. First, ensure that the owner/operator of the aircraft in which the GDL 69A is installed has subscribed to XM Ra-
dio and that it has been activated. Perform a quick check of the circuit breakers to ensure the GDL 69A has power applied. If a failure still exists, review the messages listed in the table at the end of this section. The advisory mes-
sages may provide insight to a possible failure. For troubleshooting purposes, the Status, Serial Num-
ber and Software Version numbers for the GDL 69A are displayed in the LRU Information Window on the System Status Page. WEATHER To select the System Status Page:
1. Turn the large FMS knob to select the AUX Page Group. 2. Turn the small FMS knob to select the System Status Page. Figure 7.1.19 LRU Information Window 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-23 190-00498-00_0A.indd 23 3/1/2005 10:33:47 AM Preliminary WEATHER Message Description CHECK ANTENNA XM Radio Page, the active channel is replaced with this message UPDATING XM Radio Page, the active channel is replaced with this message NO SIGNAL XM Radio Page, the active channel is replaced with this message ; also displayed on the Weather Data Link Page when the signal strength is too low for the receiver LOADING XM Radio Page, the active channel is replaced with this message OFF AIR XM Radio Page, the active channel is replaced with this message
--- (XM Radio Page, the active channel is replaced with this message ) WEATHER DATA LINK FAILURE Weather Data Link Page, displayed in the center of the screen in yellow ACTIVATION REQUIRED Weather Data Link Page, displayed in the center of the screen in yellow Antenna is not connected Updating encryption code Loss of signal Acquiring channel audio or information Channel not in service Missing channel information No communication with the GDL 69 within the last ve minutes XM Data receiver is not activated Table 7.1.1 Advisory Messages 7-24 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 24 3/1/2005 10:33:47 AM Preliminary WEATHER Table 7.1.3 shows six different colors associated with levels of ground mapping return intensity. Ground Mapping Return Color None Least Reective Moderate Return Heavy Return Very Heavy Return TBS Black Cyan Yellow Magenta Red Blue Table 7.1.3 Ground Mapping Colors GWX 68 AIRBORNE WEATHER RADAR The GWX 68 Airborne Weather Radar System provides weather detection and ground mapping capability. The primary function of the weather radar system is to nd storms along the ight path. Weather detection gives the crew the ability to recognize potentially dangerous thun-
derstorm cells. The GWX 68 weather radar system also provides ground mapping, giving the ability to distinguish land-
scape features and bodies of water. Weather radar return strength is shown in six different colors to show intensities of rainfall (black, green, yellow, red, magenta, and white). Table 7.1.2 shows six different colors associated with the levels of rainfall or storm intensity. Rainfall Rate Color Very Heavy Rainfall Heavy Rainfall Medium Rainfall Light Rainfall No Rainfall TBS Magenta Red Yellow Green Black White Table 7.1.2 Weather Radar Rainfall Rate Colors Ground mapped radar return strength is shown using the colors black, cyan, yellow, magenta, and blue. In the ground mapping mode, internal parameters are selected to increase returns from ground targets and decrease re-
turns from weather targets. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-25 190-00498-00_0A.indd 25 3/1/2005 10:33:47 AM Preliminary WEATHER Operating Modes The G1000 controls and softkeys supply all the con-
trols and functions to operate the weather radar. The ra-
dar antenna is automatically stabilized in pitch and roll axes. The crew can manually adjust the radar tilt, gain and range. The crew selects the different weather radar modes. OFF Deenergizes the weather radar subsystem. STBY The radar is in standby, the antenna scan stopped, the transmitter inhibited. STBY is shown on the PFD and MFD. The RT (Receiver Transmitter) has a warm-up period of approxi-
mately 60 seconds. If any active mode is selected before this period, the WAIT legend will be shown on the PFD and MFD. WX When selected, the radar is in the weather detection mode. Weather data is shown on the MFD. GMAP (GROUND MAPPING) In this mode, returns from ground targets and decrease returns from weather targets are shown. TEST In this mode, a test pattern is shown on the MFD to verify system operation. A TEST legend is shown on the MFD. The transmitter radiates microwave energy because it is on. 7-26 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 26 3/1/2005 10:33:47 AM Preliminary WEATHER Figure 7.1.20 Radar Initializing 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-27 190-00498-00_0A.indd 27 3/1/2005 10:33:48 AM Preliminary WEATHER When TEST mode is selected, a test pattern is shown on the MFD to verify system operation. Figure 7.1.21 Radar Test Pattern 7-28 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 28 3/1/2005 10:33:48 AM Preliminary WEATHER Figure 7.1.22 Radar Fail 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-29 190-00498-00_0A.indd 29 3/1/2005 10:33:48 AM Preliminary WEATHER Figure 7.1.23 Sector Scan at +26 Degrees 7-30 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 30 3/1/2005 10:33:49 AM Preliminary 7.2 TAWS/TERRAIN TAWS/TERRAIN PROXIMITY PAGE TAWS/Terrain Proximity Page Operations There are two terrain/obstacle viewing options avail-
able (relative to the position of the aircraft), an ARC (120) display and a 360 default display. TAWS/TERRAIN To change the viewing mode between 360 and ARC:
1. 2. Select the TAWS/Terrain Proximity Page Press the VIEW softkey. Then press the ARC softkey. To return to the 360 degree viewing display press the 360 softkey, OR:
Press the MENU key. The page menu is displayed with View Arc or View 360 highlighted. Press the ENT key on the desired selection. 3. 4. To change the map range on the TAWS/Ter-
rain Proximity Page:
1. Turn the joystick clockwise to zoom out or turn the joystick counter-clockwise to zoom in. Map ranges are 1 nm, 1/2 nm, 2.5/5 nm, 5/10 nm and 12.5/25 nm, 25/50 nm, 50/100 nm and 100/200 nm. CAUTION: Terrain and obstacle data are pro-
vided only as an aid to situational awareness. Aural messages or textual annunciations are displayed to the crew during ight operations regarding the presence of terrain or obstacles. The TAWS/Terrain Proximity Page displays the follow-
ing information:
Current aircraft location. Range marking rings (1 nm, 1/2 nm, 2.5/5 nm, 5/10 nm, 12.5/25 nm, 25/50 nm, 50/100 nm and100/200 nm). Heading Box (North Up, Track Up, DTK Up, HDG Up). Heading on the TAWS/Terrain Proxim-
ity Page displays HDG Up map data unless there is no valid heading. Additional TAWS only information:
TAWS annunciator box terrain alerts for both warnings/caution situations and TAWS status information. North arrow indicator, when not orientated in North-Up display. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-31 190-00498-00_0A.indd 31 3/1/2005 10:33:49 AM Preliminary TAWS/TERRAIN Figure 7.2.1 Terrain Scale Displaying Obstacle Data The TAWS/Terrain Proximity Page displays obstacle data with heights greater than 200 feet Above Ground Lev-
el (AGL) located at their geographical position throughout the world. Obstacles are displayed in two levels:
CAUTION WARNING Each level is associated with a color. The G1000 will adjust colors on the TAWS/Terrain Proximity Page automatically as the aircraft altitude changes. Obstacle Color RED YELLOW Indication WARNING: Obstacle height is at or above 100 below the current aircraft altitude. CAUTION: Obstacle height is between 100 and 1000 below the current aircraft altitude. Obstacle Shapes Unlighted Obstacle
(Height is less than 1000 AGL) Lighted Obstacle
(Height is less than 1000 AGL) Unlighted Obstacle
(Height is greater than 1000 AGL) Lighted Obstacle
(Height is greater than 1000 AGL) 7-32 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 32 3/1/2005 10:33:50 AM 1000'AGLAircraftAltitude100'ThresholdPreliminary TAWS/TERRAIN Navigation Map Display Conditions The Map Setup Page Menu has OBSTACLE DATA and TERRAIN DATA feature On/Off options. The Terrain Ob-
stacle features are summarized in the table below:
Terrain Feature OFF OFF Obstacle Feature OFF ON ON ON OFF ON Navigation Map Page NO OBSTACLES DISPLAYED CAUTION AND WARNING OBSTACLES DISPLAYED CAUTION AND WARNING OBSTACLES DISPLAYED SAFE, CAUTION, AND WARNING OBSTACLES DISPLAYED Displaying Terrain Data on the Navigation Map Page Terrain data can be displayed on the Navigation Map Page by pressing the TERRAIN softkey. Terrain symbol-
ogy (mountain icon) appears next to the map range in the bottom right corner of the page indicating the presence of terrain data on the map. To display terrain data on the Navigation Map Page:
1. 2. Press the MAP softkey. Press the TERRAIN softkey. Press the TERRAIN softkey again to remove terrain data from the Navigation Map Page. NOTE: Obstacles are only displayed at certain map zoom ranges, on certain map elds, and will only be displayed if an obstacle database is loaded in the system. NOTE: The table above is only for the Navigation Map Page. The Terrain Proximity Page always shows ONLY caution and warning obstacles. TERRAIN softkey Figure 7.2.2 TERRAIN Softkey NOTE: Terrain data can also be displayed by using the On/Off Navigation Map Page option. See the Navigation Map Page setup section for details. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-33 190-00498-00_0A.indd 33 3/1/2005 10:33:50 AM Preliminary TAWS/TERRAIN TAWS Garmins Terrain Awareness Warning System (TAWS) satises TSO-C151b Class B requirements for certica-
tion. Class B TAWS is required for all Part 91 aircraft operations with 6 or more seats and for Part 135 turbine aircraft operations with 6 to 9 passenger seats (FAR Parts 91.223, 135.154). Garmin TAWS greatly increases situ-
ational awareness and aids in reducing accidental Con-
trolled Flight Into Terrain (CFIT). Figure 7.2.3 shows the Navigation Map Page with ter-
rain features. In order to operate properly, the Garmin TAWS/Terrain system requires a valid 3D GPS position solution and a valid terrain/airport terrain/obstacle database. CAUTION: It is always the ultimate responsibility of the crew to navigate safely throughout the course of ight. Garmin TAWS is designed to be an aid to situational awareness, not to be relied on as a primary source of terrain and obstacle avoidance. Figure 7.2.3 Obstacles on Navigation Map Page 7-34 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 34 3/1/2005 10:33:51 AM Preliminary TAWS/TERRAIN System Compairison Garmin TAWS and TERRAIN share several common operational characteristics. Table 7.2.1 com-
pares the features and abilities of the two systems:
Function TSO-C151b Class B Certied TAWS/TERRAIN Display
( Shows terrain elevations relative to the aircraft ) Visual Alerting
( Includes popup alerting ) Aural Alerting External Visual Alerting Capability Reduced Terrain Clearance (RTC) Avoidance
( Forward Looking Terrain Avoidance (FLTA) sub-function ) Imminent Terrain Impact (ITI) Avoidance
( Forward Looking Terrain Avoidance (FLTA) sub-function ) Premature Descent Alert (PDA) Excessive Rates of Descent
( Ground Proximity Warning System (GPWS) Alerting sub-function ) Negative Climb Rate/Altitude Loss After Takeoff
( Ground Proximity Warning System (GPWS) Alerting sub-function ) Five Hundred Voice Callout
( Ground Proximity Warning System (GPWS) Alerting sub-function ) Inhibit Capability
( Inhibits FLTA and PDA visual and aural alerting ) Manual System Test Capability Worldwide Terrain Database Airport Layer Database Obstacle Database Table 7.2.1 TAWS/TERRAIN Feature Comparison TAWS Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Terrain No Yes Yes No No Yes Yes Yes No No No Yes No Yes Yes Yes 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-35 190-00498-00_0A.indd 35 3/1/2005 10:33:51 AM Preliminary TAWS/TERRAIN Basic Operation Power Up During power-up of the G1000 unit, terrain/airport terrain/obstacle database versions and area of coverage are displayed along with a disclaimer. At the same time, the TAWS/TERRAIN system self-test begins. An aural mes-
sage plays upon test completion:
TAWS System Test, OK, if the system passes the test. TAWS System Failure, if the system fails the test. A failure of the test is annunciated for both TAWS and TERRAIN, if the self-test fails. Database Updates Terrain/airport terrain/obstacle databases are updated periodically with the latest terrain/airport terrain/obstacle data. Visit the Garmin website to check for newer versions of terrain/airport terrain/obstacle databases. Updated ter-
rain data cards may be obtained from the Garmin website or by calling Garmin at one of the numbers listed in the front of this document. Display Page Operation TAWS and TERRAIN appears in the Navigation Map. To display terrain data on the Navigation Map Page:
1. 2. Press the MAP softkey. Press the TERRAIN softkey. Press the TERRAIN softkey again to remove terrain data from the Navigation Map Page. TAWS/TERRAIN/PROXIMITY Page Terrain information, aircraft ground track and GPS-de-
rived MSL altitude are displayed on the screen. Altitude is shown in increments of 20 feet or in increments of 10 meters, depending on unit conguration. The G to right of the MSL altitude display is a reminder that altitude is GPS-derived. There are two main display settings from which the crew can choose:
360 View Birds eye view from above aircraft depicts surrounding terrain on all sides. 120 View Birds eye view of terrain ahead of and 60 to either side of the aircraft ight path. NOTE: The TAWS/TERRAIN/PROXIMITY Page gives a Heading Up display orientation, as indi-
cated by the HDG label shown on the display. To change the TAWS/TERRAIN display view-
ing angle between 360 and 120:
1. Select the TAWS/Terrain Proximity Page 2. 3. 4. Press the VIEW softkey. Then press the ARC softkey. To return to the 360 degree viewing display press the 360 softkey, OR:
Press the MENU key. The page menu is displayed with View Arc or View 360 highlighted. Press the ENT key on the desired selection. 7-36 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 36 3/1/2005 10:33:51 AM Preliminary Terrain/Obstacle Database Areas of Coverage TAWS/TERRAIN Failure Alert TAWS/TERRAIN The following areas of coverage are available in each database. Regional denitions may change without no-
tice. TAWS/TERRAIN database versions may be viewed by going to AUX System Status Page. Pop-up terrain alerts are displayed only when the TER-
RAIN Page is not being viewed. Pop-up terrain alerts do not appear on the TERRAIN Page. Worldwide (WW):
Latitudes: S60 to N75 Longitudes: W180 to E180 Americas (AME):
Latitudes: S60 to N75 Longitudes: W180 to W30 Atlantic (ATL):
Latitudes: S60 to N75 Longitudes: W30 to E90 Pacic (PAC):
Latitudes: S60 to N75 Longitudes: E60 to E180 United States (US):
Limited to the United States plus some areas of Canada, Mexico, Caribbean, and the Pacic. The TAWS/TERRAIN system continually monitors sev-
eral system-critical items, such as database validity, hard-
ware status and GPS status. Should the system detect a failure, one of the following messages is issued:
No Alert or Status Terrain Not Available Terrain Test Terrain Inhibited Terrain Failure Figure 7.2.4 TAWS Failure Messages The TAWS/TERRAIN Page displays TERRAIN FAILED. For TAWS units, the aural message TAWS System Failure is issued along with the TER FAIL an-
nunciation. TAWS/TERRAIN Not Available Alert Garmin TAWS/TERRAIN requires a 3D GPS navigation solution along with specic vertical accuracy minimums. Should the navigation solution become degraded, if the terrain/airport terrain/obstacle databases are not available, or if the aircraft is out of the database coverage area, the annunciation TER N/A is given in the annunciation win-
dow. The aural message Terrain Not Available is issued along with the TER N/A annunciation. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-37 190-00498-00_0A.indd 37 3/1/2005 10:33:51 AM Preliminary TAWS/TERRAIN Forward Looking Terrain Avoidance RTC/ITI Severity Levels The Forward Looking Terrain Avoidance alert (FLTA) is used by TAWS and is composed of two sub-functions:
Reduced Required Terrain Clearance (RTC) Avoidance Provides alerts when the aircraft ight path is above terrain, yet is projected to come within minimum clear-
ance values shown in Table 7.2.2. When an RTC alert is issued, a potential impact point is displayed on the TAWS/
TERRAIN Proximity Page. Imminent Terrain Impact (ITI) Avoidance Provides alerts when the aircraft is below the elevation of a terrain cell in the aircrafts projected path. ITI alerts are accompa-
nied by a potential impact point displayed on the TAWS/
TERRAIN Proximity Page. The alert is given when the projected vertical ight path is calculated to come within minimum clearance altitudes in Table 7.2.2. During the nal approach phase of ight, RTC/ITI alerts are automatically inhibited when the aircraft is below 200 AGL while within 0.5 nm of the approach runway or is below 125 AGL while within 1 nm of the runway. Phase Of Flight Level Flight Descending Enroute Terminal Approach Departure 700 ft. 350 ft. 150 ft. 100 ft. 500 ft. 300 ft. 100 ft. 100 ft. Table 7.2.2 Minimum Terrain Clearance Values for RTC/ITI Alerts CAUTION: Estimated potential impact in approximately 60 seconds after pop-up alert and annunciation. For TAWS, RTC/ITI caution alerts are accompanied by the aural message Cau-
tion Terrain; Caution Terrain OR Terrain Ahead; Terrain Ahead. WARNING: Estimated potential impact in approximately 30 seconds after pop-up alert and annunciation. For TAWS, RTC/ITI warning alerts are accompanied by the aural message Terrain, Terrain; Pull Up, Pull Up OR Terrain Ahead, Pull Up; Terrain Ahead, Pull Up. 7-38 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 38 3/1/2005 10:33:52 AM Preliminary TAWS/TERRAIN alerting ends at 0.5 nm from the runway thresh-
old OR at an altitude of 125 AGL while within 1 nm of the threshold. ILS Approach Loaded PDA alerting begins when FAF is the active waypoint AND the aircraft is within 15 nm of the destination airport. Once the aircraft intercepts the glideslope, PDA will alert the crew if the aircraft descends 0.7 degrees below the glideslope. PDA alerting ends 0.5 nm from the runway threshold OR at an altitude of 125 AGL while within 1 nm of the threshold. CAUTION: The above annunciation and pop-up terrain alert are displayed during a PDA alert. For TAWS, the PDA alert is accompanied by the aural message Too Low, Terrain. Premature Descent Alerting (PDA) Garmin TAWS/TERRAIN issues a Premature Descent alert when the system detects that the aircraft is signi-
cantly below the normal approach path to a runway. The PDA alert mode is functional only during descent to land. There are three different scenarios to consider with PDA:
No Approach Loaded PDA alerting begins when the aircraft is within 15 nm of the destina-
tion airport and ends when the aircraft is either 0.5 nm from the runway threshold OR is at an altitude of 125 AGL while within 1 nm of the threshold. During the nal descent, algorithms will set a threshold for alerting based on speed, distance and other parameters. Non-Precision Approach Loaded PDA alert-
ing begins when FAF is the active waypoint AND the aircraft is within 15 nm of the destination air-
port. Again, algorithms are used to set a threshold for alerting based upon various parameters. PDA 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-39 190-00498-00_0A.indd 39 3/1/2005 10:33:52 AM Preliminary TAWS/TERRAIN Figure 7.2.5: Example of PDA alert threshold for ILS approach The threshold for the Non-Precision Approach PDA de-
scent is computed by algorithms based on varying ight conditions. Final Approach Fix 200' below FAF Altitude Runway Threshold CAUTION 0.5 nm 15 nm Figure 7.2.6: Example of Non-Precision Approach PDA alert threshold. 7-40 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 40 3/1/2005 10:33:54 AM RunwayThresholdFinalApproachFix200'belowFAFAltitude15nmCAUTIONPDAAlertis0.7BelowGlideslopeGlideslopeIntercept0.5nmPreliminary TAWS Alerts Excessive Descent Rate Severity Levels TAWS/TERRAIN CAUTION: The annunciation and pop-up terrain alert are accompanied by the aural message Sink Rate. The following features are required to meet Class B re-
quirements for a TAWS system per TSO-C151b. TAWS provides aural voice alerts along with regular display an-
nunciation. With each alert type shown is an accompany-
ing aural alert as well. Excessive Descent Rate Alert (EDR) The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is deter-
mined to be closing (descending) upon terrain at an excessive speed. Figure 7.2.7 shows the parameters for the alert as dened by TSO-C151b. i
) t e e F
(
n a r r e T e v o b A t h g e H i 5000 4500 4000 3500 3000 2500 2000 1500 1000 500 0
"SINK RATE"
WARNING: The annunciation and pop-up terrain alert are accompanied by the aural message Pull Up.
"PULL UP"
"PULL UP"
2000 6000 4000 8000 Descent Rate (FPM) 10000 12000 Figure 7.2.7: Excessive Descent Rate Graph 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-41 190-00498-00_0A.indd 41 3/1/2005 10:33:55 AM Preliminary TAWS/TERRAIN Negative Climb Rate After Takeoff Alert
(NCR) Alert Priority and Aural Alert Message Summary The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the crew when the system determines that the aircraft is losing altitude (clos-
ing upon terrain) after takeoff. The aural message Dont Sink is given for NCR alerts, accompanied by an annun-
ciation and a pop-up terrain alert on the display. Five-Hundred Aural Alert The purpose of the aural alert message Five-hundred is to provide an advisory alert to the crew that the aircraft is ve-hundred feet above terrain. When the aircraft de-
scends within 500 feet of terrain, the aural message Five-
hundred is heard. There are no display annunciations or pop-up alerts that accompany the aural message. TSO-C151b requires the establishment of an internal priority scheme for alerts. In this way, the more important alerts will override lesser alerts. Table 7.2.3 shows the alert priority level in the Garmin TAWS system and gives a summary of the aural messages. The aural alert is congurable for either male or female voice. Different alert text phrases are available for several alerts. Contact a Garmin authorized service center for fur-
ther information on conguring the alert system. TAWS System Test Garmin TAWS provides a manual test for the ight crew. With this feature, the crew can verify proper opera-
tion of the aural and visual system annunciation. To manually test the TAWS system:
1. At the TAWS Page, press MENU. 2. Select the Test Terrain? option. 3. Press ENT to conrm the selection. An aural message is played giving the test results:
TAWS System Test, OK, if the system passes the test. TAWS System Failure, should the system fail the test. NOTE: TAWS System Testing is disabled during ight. 7-42 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 42 3/1/2005 10:33:55 AM Preliminary TAWS/TERRAIN Priority 1 2 3 4 5 6 7 8 9 Alert Type Excessive Descent Rate Alert Warning Terrain Awareness Warning: RTC ITI Alerts Obstacle Awareness Warning: ROC, IOI Aural Message Pull Up Terrain, Terrain; Pull-Up, Pull-Up Or Terrain Ahead, Pull-Up; Terrain Ahead, Pull-Up Obstacle, Obstacle; Pull-Up, Pull-Up Or Obstacle Ahead, Pull-Up; Obstacle Ahead, Pull-Up Terrain Awareness Caution: RTC, ITI Alerts Caution, Terrain; Caution, Terrain Obstacle Awareness Caution: ROC, IOI PDA Caution Alert Altitude Callout 500 Excessive Descent Rate Alert Caution Negative Climb after Takeoff Alert Or Terrain Ahead; Terrain Ahead Caution, Obstacle; Caution, Obstacle Or Obstacle Ahead; Obstacle Ahead Too Low, Terrain Five-hundred Sink Rate Dont Sink or Too Low, Terrain Table 7.2.3: TAWS Alert Summary 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-43 190-00498-00_0A.indd 43 3/1/2005 10:33:55 AM Preliminary TAWS/TERRAIN This page intentionally left blank. 7-44 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 44 3/1/2005 10:33:55 AM Preliminary 7.3 TRAFFIC TRAFFIC MAP PAGES The Trafc Map Page displays the following informa-
TIS (TRAFFIC INFORMATION SYSTEM) tion:
TRAFFIC TIS is a system used for detecting and tracking aircraft in the vicinity of your own aircraft. When ATC radar interrogates aircraft transponders, the replies are analyzed to determine range, bearing and the relative altitude of the intruder. The trafc is then displayed to the ight crew on the MFD. CAUTION: TIS is unable to detect any intruding aircraft without an operating transponder. NOTE: Trafc Information Service (TIS) is not available in all areas. TRANSPONDER STATUS BAR TIS surveillance data is up-linked by Air Trafc Con-
trol (ATC) radar through the GTX 33 Mode S Transpon-
der. The Transponder Status Bar displays the transponder code, reply symbol and mode of operation on the Inset Map (PFD) and the Navigation and Trafc Map Pages on the MFD (refer to the MFD Pilots Guide). In order to receive and display TIS trafc information, the GTX 33 must not be in GND mode or STBY mode. Figure 7.3.1 Transponder Status Bar When trafc is displayed within the TIS volume, the word TRAFFIC appears on the PFD. Figure 7.3.2 shows the Trafc Annunciation on the PFD. Current aircraft location, surrounding TIS trafc, and range marking rings. The current trafc mode (OPERATE, STANDBY). A trafc alert message (FAILED, DATA FAILED, NO DATA, UNAVAILABLE). Trafc display banner (AGE 00:, TRFC COAST, TA OFF SCALE, TRFC RMVD, TRFC FAIL, NO TRFC DATA, TRFC UNAVAIL, TRAFFIC). To select the Trafc Map Page:
1. Select the MAP group of pages. Turn the small FMS knob to select the Trafc Map Page. To display trafc on the Navigation Map Page:
1. 2. Press the MAP softkey. Press the TRAFFIC softkey. Press the TRAFFIC softkey again to remove trafc. NOTE: Traffic and terrain data can also be displayed by using the On/Off Navigation Map Page option. See the Navigation Map Page setup section for details. Figure 7.3.3 shows the Trafc Map Page on the MFD. Trafc symbols are similarly displayed on the Naviga-
tion map page. The trafc symbols are shown relative to other displayed features. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-45 190-00498-00_0A.indd 45 3/1/2005 10:33:55 AM Preliminary TRAFFIC Trafc Annunciation Trafc Mode Trafc Figure 7.3.2 Trafc Annunciation on PFD Map Range Own Aircraft Figure 7.3.3 Trafc Map Page 7-46 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 46 3/1/2005 10:33:56 AM Preliminary TIS Symbology TIS trafc is displayed on the Trafc Map Page simi-
larly to TCAS symbology. The main difference between TIS and TCAS is the source of surveillance data. TCAS uses an airborne interrogator with a half-second update rate. TIS uses the terminal Mode S ground interrogator and its Data Link to provide approximately a ve-second update rate. The range accuracy of TIS and TCAS is simi-
lar. Appendix E describes the Trafc Information Service in detail. The Trafc Advisory (TA) solid yellow circle indicates that trafc meets the TA advisory criteria. The presence of TA trafc beyond the selected display range is indicated by one half of a yellow circle at the edge of the display. The position of the half-symbol represents the bearing of the trafc. Altitude separation from your aircraft is displayed above the target symbol if the trafc is above your alti-
tude or below the symbol if they are below. Altitude trend is displayed as an up arrow (+500 ft/min), down arrow
(-500 ft/min) or no symbol if less than 500 ft/min rate in either direction. Trafc Ground Track is indicated on the Trafc Map Page by a Track Vector. The track vector line is pro-
jected from the TA symbol at the angle of the TA relative track. Proximate trafc is shown as a white diamond with a solid box inside. Other trafc is displayed as a hollow white diamond. Proximate trafc and other trafc sym-
bols indicate that trafc is not yet considered a threat, so no Trafc Advisory is generated. TRAFFIC Category Symbol Other Trafc Proximate Trafc Trafc Advisory, Out of Range Trafc Advisory Trafc Map Page Operations Power-Up Test The TIS interface performs an automatic test during power-up. If the system passes the power-up test, the standby screen is displayed on the Trafc Map Page. If the system passes the power-up test while the aircraft is airborne, trafc is immediately displayed on the Trafc Page in the operating mode. If the system fails the power up test, the NO DATA, DATA FAILED or FAILED message is displayed. The FAILED message indicates the GTX 33 tran-
sponder has failed. The DATA FAILED message indicates data is being received from the GTX 33 but a failure was detected in the data stream. The NO DATA message indicates that data is not being received from the GTX 33. Contact a Garmin authorized service center for repair. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-47 190-00498-00_0A.indd 47 3/1/2005 10:33:57 AM Preliminary OPERATE when the Trafc Map Page displays OPERATE in the status box on the Trafc Map Page, the TIS system is operational and displays trafc on the Trafc and Map Pages. The crew can switch between the standby (STBY) and operate (ON) modes to manually override automatic op-
eration using the page menu or softkeys. To switch between operating modes:
1. 2. Press the MODE softkey. Press the STBY or ON softkey to switch between modes. STANDBY or OPERATE is displayed in the status box located in the upper left corner of the Trafc Map Page, OR:
Press the MENU key. The page menu is displayed with Standby Mode or Operate Mode highlighted. Press the ENT key on the desired selection. 3. TRAFFIC Changing the Map Range To change the map range:
1. Turn the joystick clockwise to zoom out or turn the joystick counter-clockwise to zoom in. Map ranges are 2 nm, 6 nm and 12 nm. NOTE: If the intruder aircraft is non-altitude reporting only the range and bearing will be displayed. Operating Mode Once the aircraft is airborne the system switches from ground or standby mode to operating mode. The G1000 displays OPERATE in the upper left hand corner of the display and begins to display trafc on the Trafc or Map Page. The TIS Trafc Advisory (TA) should alert the crew to look for intruding aircraft any time a yellow circle trafc symbol appears and voice warning is announced. Conduct a visual search for the intruder. Maintain visual contact to ensure safe separation. When the aircraft is on the ground the system switches from operating mode to ground or standby mode. The Trafc Map Page displays GND or STANDBY. STANDBY when the Trafc Map Page displays STANDBY in the status box on the Trafc Map Page, the TIS system is in standby mode and cannot display trafc data. GND when the Trafc Map Page displays GND in the status box on the Trafc Map Page, the TIS system does not display trafc data. The GTX 33 does not reply to Mode A or Mode C interroga-
tions but does send Mode S acquisition replies. The ground mode is entered automatically. It is not a crew selectable mode. 7-48 Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00 Draft 190-00498-00_0A.indd 48 3/1/2005 10:33:57 AM Preliminary TRAFFIC TRFC RMVD - the TRFC RMVD banner indicates that trafc has been removed from the display due to the age of the data. Data is too old to coast when the time period is 12-60 seconds from the last receipt of a TIS message. The crew should be aware that trafc may be present but not shown. TA OFF - the TA OFF scale banner displayed in the lower left corner of the display indicates that a trafc advisory is outside the selected display range. The trafc advisory off-range banner is removed when the trafc advisory is within the selected display range. TRAFFIC - on the PFD, when the system receives a trafc advisory a ashing TRAFFIC alert is displayed in the upper left hand portion of the display. The PFD inset map also automatically displays trafc data. CAUTION: TIS warns the crew with voice and visual trafc advisories whenever it predicts an intruder to be a threat. The display and advi-
sories are intended only for assistance in visu-
ally locating the trafc and lack the resolution and coordination ability necessary for evasive maneuvering. Always attempt to visually clear the airspace before maneuvering your aircraft in response to a TA. See Appendix E for detailed TIS information. TIS Audio Alert A TIS audio alert is generated whenever the number of TAs on the Trafc Map Page display increases. Limiting audio to TAs only reduces the amount of nuisance alert-
ing due to proximate aircraft. For example, when the rst TA is displayed, the crew is alerted audibly. As long as a single TA aircraft remains on the TIS display, no further audio alert is generated. If a second TA aircraft appears on the display, a new audio alert is sounded. If the number of TAs on the TIS display decreases and then increases, a new audio alert is sounded. The TIS audio alert is also generated whenever TIS service becomes unavailable. The volume of the audio alerts and the choice between a male or female voice is congured during installation. The following TIS audio alerts are available:
Trafc - TIS trafc alert is received. Trafc Not Available - TIS service is not available or out of range. TIS Trafc Status The MFD indicates the following TIS trafc status to the ight crew. Trafc Banner AGE - if trafc data is not refreshed within 6 seconds, an age indicator (i.e., AGE 00:06) is displayed in the lower left corner of the display, when displaying trafc. After another 6 seconds, if data is still not received, the trafc is removed from the display. The quality of displayed trafc is reduced as the trafc data becomes stale. TRFC COAST - the TRFC COAST (trafc coast-
ing) banner located above the AGE timer indicates that displayed trafc is held even though the data is stale. The quality of displayed trafc is reduced. 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 7-49 190-00498-00_0A.indd 49 3/1/2005 10:33:57 AM Preliminary 190-00498-00 Draft Garmin G1000 Hazard Avoidance Pilots Guide for the Cessna Citation Mustang 190-00498-00_0A.indd 3 3/1/2005 10:33:57 AM Preliminary Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00498-00 Rev. A 3/1/2005 10:34:04 AM 2005 Garmin Ltd. or its subsidiaries 190-00498-00_0A.indd 4
frequency | equipment class | purpose | ||
---|---|---|---|---|
1 | 2005-05-27 | 9300 ~ 9500 | TNB - Licensed Non-Broadcast Station Transmitter | Original Equipment |
app s | Applicant Information | |||||
---|---|---|---|---|---|---|
1 | Effective |
2005-05-27
|
||||
1 | Applicant's complete, legal business name |
Garmin International Inc
|
||||
1 | FCC Registration Number (FRN) |
0005088588
|
||||
1 | Physical Address |
1200 E. 151st. Street
|
||||
1 |
Olathe, KS
|
|||||
1 |
United States
|
|||||
app s | TCB Information | |||||
1 | TCB Application Email Address |
T******@TIMCOENGR.COM
|
||||
1 | TCB Scope |
B3: Maritime & Aviation Radio Services equipment in 47 CFR parts 80 & 87
|
||||
app s | FCC ID | |||||
1 | Grantee Code |
IPH
|
||||
1 | Equipment Product Code |
0060200
|
||||
app s | Person at the applicant's address to receive grant or for contact | |||||
1 | Name |
D****** K********
|
||||
1 | Title |
Manager Environmental and Regulatory Affairs
|
||||
1 | Telephone Number |
91344********
|
||||
1 | Fax Number |
913 3********
|
||||
1 |
d******@garmin.com
|
|||||
app s | Technical Contact | |||||
n/a | ||||||
app s | Non Technical Contact | |||||
n/a | ||||||
app s | Confidentiality (long or short term) | |||||
1 | Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | Yes | ||||
1 | Long-Term Confidentiality Does this application include a request for confidentiality for any portion(s) of the data contained in this application pursuant to 47 CFR § 0.459 of the Commission Rules?: | No | ||||
if no date is supplied, the release date will be set to 45 calendar days past the date of grant. | ||||||
app s | Cognitive Radio & Software Defined Radio, Class, etc | |||||
1 | Is this application for software defined/cognitive radio authorization? | No | ||||
1 | Equipment Class | TNB - Licensed Non-Broadcast Station Transmitter | ||||
1 | Description of product as it is marketed: (NOTE: This text will appear below the equipment class on the grant) | AIRCRAFT MOUNTED WEATHER RADAR TRANSMITTER | ||||
1 | Related OET KnowledgeDataBase Inquiry: Is there a KDB inquiry associated with this application? | No | ||||
1 | Modular Equipment Type | Does not apply | ||||
1 | Purpose / Application is for | Original Equipment | ||||
1 | Composite Equipment: Is the equipment in this application a composite device subject to an additional equipment authorization? | No | ||||
1 | Related Equipment: Is the equipment in this application part of a system that operates with, or is marketed with, another device that requires an equipment authorization? | No | ||||
1 | Is there an equipment authorization waiver associated with this application? | No | ||||
1 | If there is an equipment authorization waiver associated with this application, has the associated waiver been approved and all information uploaded? | No | ||||
app s | Test Firm Name and Contact Information | |||||
1 | Firm Name |
Rogers Labs, Inc.
|
||||
1 | Name |
S****** R******
|
||||
1 | Telephone Number |
91383********
|
||||
1 | Fax Number |
91383********
|
||||
1 |
r******@micoks.net
|
|||||
Equipment Specifications | |||||||||||||||||||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Line | Rule Parts | Grant Notes | Lower Frequency | Upper Frequency | Power Output | Tolerance | Emission Designator | Microprocessor Number | |||||||||||||||||||||||||||||||||
1 | 1 | 87 | 9300.00000000 | 9500.00000000 | 7500.0000000 | 1097.0000000000 ppm | 8M00PON |
some individual PII (Personally Identifiable Information) available on the public forms may be redacted, original source may include additional details
This product uses the FCC Data API but is not endorsed or certified by the FCC