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1.3.5 VOR Specifications (GNS 530 Only) Regulatory Compliance TSO C40c, JTSO-2C40c, RTCA DO-196, EuroCAE ED-22B ICAO Annex 10 Volume I (Radio Navigation Aids) Par. 3.3.8 Receiver Audio Sensitivity At -103.5 dBm (S+N)/N shall not be less than 6 dB. Course Deviation Sensitivity -103.5 dBm or less for 60% of standard deflection. Flag The VOR Course Deviation Flag must be flagged: a) in the absence of an RF signal. b) in the absence of the 9960 Hz modulation. c) in the absence of either one of the
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1.3.6 LOC Specifications (GNS 530 Only) Regulatory Compliance TSO C36e, JTSO-C36e, RTCA DO-195 Class A, EuroCAE ED-46B Annex 10 Volume I (Radio Navigation Aids) Par. 3.1.4 Receiver Audio Sensitivity At -103.5 dBm (S+N)/N shall not be less than 6 dB. Course Deviation Sensitivity -103.5 dBm or less for 60% of standard deflection. Flag The LOC Course Deviation Flag must be flagged: a) in the absence of an RF signal. b) When either the 90 or 150 Hz modulating signals is removed and the other is main
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1.3.7 Glideslope Specifications (GNS 530 Only) Regulatory Compliance TSO C34e, JTSO-C34e, RTCA DO-192, EuroCAE ED-47B Sensitivity -87 dBm or less for 60% of standard deflection. Centering Accuracy 0 ±.0091 ddm or 0 ±7.8 mV. Selectivity The course deviation shall be 0 ddm ±.0091ddm when using the Glideslope Centering Test Signal as the RF frequency is varied ±17 kHz from the assigned channel. At frequencies displaced by ±132 kHz or greater, the input signal shall be at least 60 dB down. Standard
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1.4 LICENSE REQUIREMENTS The following guidance is provided to help ensure the proper licensing of the GNS 530 COM within the United States and its territories. Outside the United States, the operator must verify compliance with any applicable communications regulations for the area in which the equipment is operated. 1. The Telecommunications Act of 1996 effective February 8, 1996 provides the FCC discretion to eliminate radio station license requirements for aircraft. At present, an individu
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The FDE function is built into the GPS 500/GNS 530 and does not require pilot interaction. In contrast, the FDE Prediction Program does require pilot interaction and must be used prior to oceanic/remote area flights to predict FDE availability. The 500 Series Trainer software includes an FDE Prediction Program to meet the requirements for GPS as a primary means of navigation for oceanic/remote operations per N8110.60. The oceanic flight phase occurs on the GPS 500/GNS 530 when more than 200 nau
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2. INSTALLATION 2.1 INTRODUCTION Careful planning and consideration of the suggestions in this section are required to achieve the desired performance and reliability from the 500 Series unit. Any deviations from the installation instructions prescribed in this document shall be accomplished in accordance with the requirements set forth in FAA AC 43.13-2A, and 14 CFR Part 43 Maintenance, Preventive Maintenance, Rebuilding, and Alteration. 2.2 ANTENNA CONSIDERATIONS Antenna installations on pres
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2.2.6 ANTENNA LIMITATIONS Garmin’s GA 56 Antennas are recommended for installations where the airspeed of the aircraft is subsonic. In such installations, GA 56—Mod 1 or later—must be used. See the COM, VOR/LOC, and Glideslope antenna specifications for their limitations. 2.2.7 VHF COM INTERFERENCE OF GPS On many panel-mounted installations, VHF COM transceivers can radiate strong harmonics from the transceiver and its antenna. The 500 Series COM does not interfere with its own GPS section. How
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2.3 RACK CONSIDERATIONS Plan a location which gives the pilot complete and comfortable access to the entire keypad and which is plainly visible from the pilot’s perspective. Installation of remote switches and annunciators may not be required if the 500 Series unit is installed in the pilot’s normal field of view (refer to the FAA letter in Appendix B). Check that there is adequate depth for the rack in the instrument panel. A location away from heating vents or other sources of heat generatio
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Qualified GPS Antenna This antenna must be one of those listed in the accessories list, or meet the following requirements: 1. DO-160C Environmental Conditions The antenna shall meet the environmental conditions listed below and shall conform to the test requirements of RTCA DO-160C. Environmental Condition Category Description o Temperature (operating) F2 -55 to +70 C o (ground survival) F2 -55 to +85 C Altitude F2 55,000 feet o Temperature Variation A 10
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3. INSTALLATION PROCEDURE 3.1 UNIT AND ACCESSORIES The GNS 530 units are available under the following part numbers: 3.1.1 GNS 530 CATALOG UNIT GNS ACCESSORIES COLOR OPERATING MINIMUM P/N P/N 530A (1) VOLTAGE XMIT PWR 010-00182-00 011-00550-00 N N BLACK 28 10 W 010-00182-01 011-00550-00 N Y BLACK 28 10 W 010-00182-10 011-00550-10 N N BLACK 14 or 28 Vdc 10 W 010-00182-11 011-00550-10 N Y BLACK 14 or 28 Vdc 10 W 010-00182-30 011-00550-30 N N GRAY 14 or 28 V (2) 10 W 010-00182-31 011-00550-30 N Y G
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The following installation accessories are available: 1. GPS Antenna Options: • GA 56 Antenna Kit, without cable (Mod 1 or later, Garmin P/N 010-10040-01). • This kit contains the following items: ITEM GARMIN P/N QTY GA 56 ANTENNA SUB-ASSEMBLY 011-00134-00 1 BACKING PLATE 115-00031-00 1 NUT, SELF-LOCKING, #8-32 210-10004-09 4 ANTENNA GASKET 253-00002-00 1 • GA 56 Flange Mount Antenna Kit (Mod 1 or later, Garmin P/N 010-10040-02). • This kit contains the following items: ITEM GARMIN P/N QTY FLANG
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500 SERIES
INSTALLATION MANUAL
TM
GPS 500 and GNS 530A
GNS is a trademark of Garmin Ltd. or its subsidiaries and
may not be used without the express permission of Garmin.
TM
(GNS 530 Shown)
Garmin International, Inc.
190-00181-02, Revision G
May 2003
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© Copyright 1998 - 2003 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 o
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This manual is written for main software version 4.00. Information in this document is subject to change without notice. Visit the Garmin web site (www.garmin.com) for current updates and supplemental information concerning the operation of this and other Garmin products. 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, Subch
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TABLE OF CONTENTS 1. GENERAL DESCRIPTION 1.1 INTRODUCTION .........................................................................................................................................1-1 1.2 EQUIPMENT DESCRIPTION......................................................................................................................1-1 1.3 TECHNICAL SPECIFICATIONS.................................................................................................................1-1 1.4 LICEN
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LIST OF FIGURES FIGURE 2-1. GPS ANTENNA INSTALLATION CONSIDERATIONS .................................................................2-2 FIGURE 3-1. COAXIAL CABLE INSTALLATION ................................................................................................3-4 FIGURE 3-2. GA 56 ANTENNA INSTALLATION DRAWING .............................................................................3-7 FIGURE 3-3. GNS 530 MOUNTING RACK DIMENSIONS ...............................................
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500 SERIES HARDWARE MOD LEVEL HISTORY The following table identifies hardware modification (Mod) Levels for the GPS 500 and GNS 530. 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 adviso
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1. GENERAL DESCRIPTION 1.1 INTRODUCTION This manual describes the physical, mechanical, and electrical characteristics and the installation requirements for the 500 Series (GPS 500 and GNS 530) panel-mounted units. After installation of the 500 Series system, FAA Form 337 must be completed by an appropriately certificated agency to return the aircraft to service. Note: Throughout this document references made to GNS 530 shall equally apply to the GNS 530A except where specifically noted. 1.2 E
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1.3.2 General Specifications Operating Temperature Range -20°C to +55°C. For more details see Environmental Qualification Form. Humidity 95% non-condensing Altitude Range -1,500 ft to 50,000 ft Input Voltage Range 11 to 33 Vdc GPS 500 (011-00562-00, -10) GNS 530 (011-00550-10, -30) Input Voltage Range 22 to 33 Vdc GNS 530 (011-00550-00) Input Voltage Range 28 Vdc GNS 530A (011-00835-00, -10) Power Requirements—P5001 1.8 A @ 27.5 Vdc (maximum) (GNS 530 Main Connector) 3.6 A @ 13.75 Vdc (maximum)
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1.3.4 COM Transceiver Specifications (GNS 530 Only) ** Regulatory Compliance TSO-C37d Class 4 & 6* (3 & 5 for “A” models),TSO-C38d Class C & E, JTSO-2C37e, JTSO-2C38e, RTCA DO-186a ICAO Annex 10 Volume III (Part II – Voice Communications Systems) Par. 2.3.3 Audio Output 100 mW minimum into a 500 Ω load. Audio Response Less than 6 dB of Variation between 350 and 2500 Hz. Audio Distortion The distortion in the receiver audio output shall not exceed 15% at all levels up to 100 mW. AGC Characteristi
