Operator`s manual

ManualsBrandsVAL Avionics ManualsMusical equipmentNAV 2000

VAL AVIONICS LTD

NAV 2000

ULTRA-THIN NAVIGATION RECEIVER

Installation and

Operator’s Manual

Release Issue

Oct. 2013

P/N 172203-0

Summary of content (29 pages)

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VAL AVIONICS LTD NAV 2000 ULTRA-THIN NAVIGATION RECEIVER Installation and Operator’s Manual Release Issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L This Page Intentionally Left Blank Release issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L Table of Contents 1 SECTION I - GENERAL INFORMATION........................................................................................................ 4 1.1 1.2 1.3 1.4 1.5 1.6 1.7 2 INTRODUCTION............................................................................................................................ 4 SCOPE ...................................
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 1 SECTION I - GENERAL INFORMATION 1.1 INTRODUCTION Thank you for purchacing our NAV 2000 Navigation Receiver. Here at Val Avionics Ltd., our core design philosophy is based on the ease of installation and use. The NAV 2000 represents a new direction and continued improvement of our product line.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 1.4 SPECIFICATIONS Table 1: Specifications SPECIFICATIONS Environmental VOR Localizer Glide slope CHARACTERISTICS RTCA/DO160D RTCA/DO-196 RTCA/DO-195 RTCA/DO-192 Physical Dimensions: Height Width Depth 1.0 inches (2.54 cm) 6.25 inches (15.88 cm) 9.0 inches (22.86 cm) Weight: 3.00 pounds (1.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 1.5 EQUIPMENT SUPPLIED Table 2: Equipment Supplied PART NUMBER 1.6 0800120 QTY 1 0651020 1 EQUIPMENT REQUIRED BUT NOT SUPPLIED Table 3: Equipment Not Supplied QTY DESCRIPTION 1 Interconnect Wire Harness 1 Headphone Jack 1.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 2 SECTION II - INSTALLATION 2.1 GENERAL INFORMATION 2.1.1 Scope This section of the manual will provide the needed information to successfully complete the installation of your new NAV 2000 Navigation Receiver. Please read this section completely before proceeding with the installation process.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 2.3.3 Wire Harness Fabrication Val Avionics Ltd. recommends that a factory fabricated wire harness (VPN 0751020) be used for the installation of the NAV 2000 Navigation receiver.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 2.3.4.3 Audio The NAV 2000 has one navigation audio output. Although the audio output levels of the receivers are capable of driving a standard headset directly, it is strongly recommended that these audios be coupled to a quality audio selector panel. For complete details, refer to the interconnect wiring diagrams in Appendix B. 2.4 POST INSTALLATION CHECK 2.4.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 3 SECTION III - OPERATION 3.1 GENERAL INFORMATION 3.1.1 Scope This section will provide detailed operating instructions for your new NAV 2000 Navigation Receiver. Please read this section completely to become familiar with all of the features of the unit. 3.1.2 Display Functions 3.1.3 User Controls The user controls consist of two sets of concentric rotary knobs.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 3.1.3.3 Setting a Bearing The bearing on the unit can be selected through one of three ways: Using a mechanical resolver, through the RS-232 input, or through using the basic nav setting. When working with a mechanical resolver, select the desired bearing using the OBS knob.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 3.2.1.1 OBS/Resolver Selection (Rs I) Selecting the OBS input to the unit using the configuration pages has 3 options: SER: Serial input: The unit accepts the OBS over the RS-232 input and changes the deviation outputs accordingly with the inputted data.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 4 SECTION IV - WARRANTY AND SERVICE 4.1 LIMITED WARRANTY The equipment delivered with this Standard Factory Warranty is manufactured by Val Avionics, Ltd. and is guaranteed against defective materials and workmanship for one year from date of original retail purchase.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 5 Appendix A – INSTALLATION DRAWINGS AND CONNECTOR LAYOUT Figure 1: Physical Dimensions Release issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L Figure 2: P1 Connector Pin Out (Drawing Not to Scale) Figure 3: Panel Cut Out Figure 4: Mounting Tray Assembly Exploded View Release issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L Table 4: Rear Connector Pin Functions Pin Release issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 6 Appendix B – WIRING DIAGRAMS Figure 5: NAV 2000 Basic Wiring Diagram Figure 6: NAV 2000 to Nav Indicator Figure 7: NAV 2000 to Nav Converter Release issue Oct.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L This Page Intentionally Left Blank
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N R E C E I V E R I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 7 Appendix C – INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 7.1 MAINTENANCE INSTRUCTIONS Maintenance of the NAV 2000 Navigation Receiver is on condition only. No periodic maintenance is required. VOR calibration, in accordance with 14 CFR 91.171, is required to be checked every 30 days. If unit is found to be out of calibration, send unit in for service.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 8 Appendix D – RS-232 Instruction Listing This appendix includes the interface specifications for the RS-232 serial port. The RS-232 port can be used to input active and standby frequencies as well as using an external serial resolver such as an EFIS system. The interface format conforms to NMEA 0183 message format specifications. 8.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 8.5 Message Formats All messages will conform to the NMEA 0183 proprietary message format as follows. All characters will be standard ASCII characters. No binary data characters will be used. “$”.....................................Start of message character, ASCII “$” (024h) “P”.....................................Proprietary message identifier “MRR” .....................
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 8.6 Message Definitions Input Messages REQUEST DATA OUTPUT This input is used to request an output message to be sent by the NAV 200. Message format: “V” ...............................Message class. This is a VHF NAV message. “24” ..............................Message identifier. ii ....................................
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L Message format: $PMRV27E4N This example command would set the active VOR frequency to 117.100 MHz. This can be interpreted by noting that the ASCII ‘E’ corresponds with 45h, + 30h = 75h, converted to decimal equals 117 for the MHz portion of the command. The kHz portion converts ASCII ‘4’ to 34h, 30h = 4h, x 25 kHz steps = 100 kHz.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L a……………..Transceiver function: N = normal, 0 = unchanged. Example message: $PMRRV29G4M This example command would set the standby VOR frequency to 119.100 MHz. This is interpreted by noting that the ASCII ‘G’ corresponds with 47h, + 30h = 77h, converted to decimal equals 119 for the MHz portions.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L $PMRRV34310 Set the OBS value to 310 degrees. COM VOLUME AND SQUELCH CONTROL This message is used to adjust the volume and squelch levels of the COM unit Message format: "V" ..................... Message class - VHF NAV Message "71" .................... Message Identifier "vs" ....................
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L NAVIGATION VOLUME CONTROL This message is used to adjust the volume level of the NAV unit Message format: "V" ..................... Message class - VHF NAV Message "73" .................... Message Identifier "v" ......................
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L 100. –100 indicates full deflection upwards, 0 indicates no reflection, and 100 indicates full deflection downwards. ff......................... Flags. Eight bits for HNAV and VNAV related flags, represented as two encoded hex digits.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L COMMUNICATIONS ERROR This message is used to indicate a communication error. Message format: “V”..................... Message class. This is a VHF NAV message. “27”.................... Message identifier. e ......................... Error code: (ASCII) “0” = input message checksum error. “1” = unknown message. “2” = error or mismatch in message data.
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V A L A V I O N I C S L T D N A V 2 0 0 0 N A V I G A T I O N S Y S T E M I N S T A L L A T I O N A N D O P E R A T O R ’ S M A N U A L “V”..................... Message class. This is a VHF NAV message. “35”.................... Message identifier. mk ...................... Active frequency: m = MHz, where m = desired MHz frequency – 30h, ranging from 118 to 136 MHz, 162 (i.e., 76h to 88h, A2h); k = (kHz offset / 25 kHz) + 30h, ranging from 000 to 975 kHz steps. mk ......................