User manual TRIMBLE TA-12 INSTALLATION REV D

[. . . ] T INSTALLATION MANUAL TRIMBLE GPS NAVIGATION SYSTEM TASMAN/ARINC-12 (TA-12) Revision D August 2000 Trimble Part No. 2105 Donley Drive Austin, Texas 78758 COPYRIGHT NOTICE Ó 1999 TRIMBLE NAVIGATION LTD. Reproduction of this publication or any portion thereof by any means without the express written permission of TRIMBLE NAVIGATION LTD. For further informqation, contact: Manager, Technical Publications, TRIMBLE NAVIGATION LTD. , Avionics Division, 2105 Donley Drive, Austin, Texas 78758. Telephone (512) 873-9100. TNL TA-12 GPS Receiver T LIST OF EFFECTIVE PAGES Dates of Original and Change pages are: Original: Revision B Revision C Revision D Page Description Front Cover List of Effective Pages Table of Contents Section 1 General Information A i - iv 1-1 1-3 1-4 1-5 1-6 1-7 1-8 2-1 2-4 2-5/6 2-13/14 3-1 3-3 3-4 3-5 3-6 4-1 4-2 4-3 4-4 4-5 5-1 5-4 A-1 A2 A-3 A4 A5 B1 B5 August 1998 April 1999 June 1999 August 2000 Page No. [. . . ] The resistance between each antenna mounting screw and the aircraft fuselage should be less than 1 ohm. 2. 3. 4 Receiver Processor Unit Installation The TA-12 RPU can be mounted at any attitude. Dimensions of the RPU are shown in Figure 2-2. 2. 3. 4. 1 Location The RPU may be installed in any area that provides two inch clearance around the RPU. C, June 1999 TNL TA-12 GPS Receiver 2. 3. 4. 2 Adapter Plate Installation T The adapter plate may be installed in the location previously occupied by an ARINC-743 Alternate Form Factor Receiver. The hex nuts supplied with the mounting hardware kit may then be used to attach the RPU to the adapter plate. 2. 3. 4. 3 Placard Use No additional placards are required as a result of installing the TA-12 RPU. 2. 3. 4. 4 Harness and Cable Fabrication The installing agency must supply and fabricate all external connectors and cables. The length and routing of external cables must be carefully studied and planned before attempting installation of the equipment. Avoid sharp bends or routing the cables too close to aircraft control cables and power sources. When necessary to cross power cables, use extra braided shielding and cross at a right angle. In addition to the standard aircraft tools, the following special tools are required: A. Daniels Pin Crimper P/N M22520/2-01 or equivalent able to crimp 16 AWG and 20 AWG wire. RG-393 Crimp Tool Amp P/N 22015-1 or equivalent (only if RG-393 is used). B. RPU External Wiring Requirements Connector Grounding Lug Wiring Description Wire should be MIL-W-16878E/4 or equivalent. The Grounding lug shall be connected to aircraft ground through a 20-gauge wire attached to the lug with the lug ring supplied (Trimble P/N 12431). Wire should be MIL-W-16878E/4 or equivalent; the power connections require 20- or 22-gauge twisted shielded pairs. The serial communication, ARINC port connections require 22- or 24-gauge twisted shielded pairs. All other input and output connections require 22 or 24 gauge shielded cable. Wire should be MIL-W-16878E/4 or equivalent; the keyfill connections require 22- or 24-gauge wires. J1 J2 J4 Rev. C, June 1999 2-3 T TNL TA-12 GPS Receiver This page intentionally left blank 2-4 Rev. C, June 1999 TNL TA-12 GPS Receiver FMS-1 FMS GEN 429 TXGEN 429 TX+ GPS 2 429 RXGPS 2 429 RX+ GPS 1 429 RXGPS 1 429 RX+ T FMS-2 FMS GEN 429 TXGEN 429 TX+ GPS 2 429 RXGPS 2 429 RX+ GPS 1 429 RXGPS 1 429 RX+ IRS-1 IRS IRS-2 IRS DADS-1 DADS DADS-2 DADS 429 TX429 TX+ 429 TX429 TX+ 429 TX429 TX+ 429 TX429 TX+ ANT-1 TA12-1 ANTENNA ANT-2 ANTENNA TA12-2 TA12 RPU ANTENNA J3 J3 +28V DC +28V DC J3 TA12 RPU J3 ANTENNA POWER GROUND GROUND VIN+ VINN/C J2-55 J2-4 J1-A J1-B J1-C J2-55 J2-4 J1-A J1-B J1-C GROUND GROUND VIN+ VINN/C POWER FMS1 FMS/IRS 1 429 RX+ FMS/IRS 1 429 RXGPS 1 429 TX+ GPS 1 429 TX- J2-34 J2-5 J2-13 J2-2 J2-34 J2-5 J2-13 J2-2 FMS/IRS 1 429 RX+ FMS/IRS 1 429 RXGPS 1 429 TX+ GPS 1 429 TX- FMS1 FMS2 FMS/IRS 2 429 RX+ FMS/IRS 2 429 RXGPS 2 429 TX+ GPS 2 429 429 TX- J2-20 J2-6 J2-14 J2-7 J2-20 J2-6 J2-14 J2-7 FMS/IRS 2 429 RX+ FMS/IRS 2 429 RXGPS 2 429 TX+ GPS 2 429 429 TX- FMS2 IRS1 FMS/IRS 3 429 RX+ FMS/IRS 3 429 RX- J2-41 J2-18 J2-41 J2-18 FMS/IRS 3 429 RX+ FMS/IRS 3 429 RX- IRS1 IRS2 FMS/IRS 4 429 RX+ FMS/IRS 4 429 RX- J2-36 J2-42 J2-36 J2-42 FMS/IRS 4 429 RX+ FMS/IRS 4 429 RX- IRS2 DADS1 DADS 1 429 RX+ DADS 1 429 RX- J2-27 J2-12 J2-27 J2-12 DADS 1 429 RX+ DADS 1 429 RX- DADS1 DADS2 DADS 2 429 RX+ DADS 2 429 RX- J2-28 J2-1 J2-28 J2-1 DADS 2 429 RX+ DADS 2 429 RX- DADS2 DGPS1 DGPS 1 429 RX+ DGPS 1 429 RX- J2-52 J2-54 J2-52 J2-54 DGPS 1 429 RX+ DGPS 1 429 RX- DGPS1 DGPS2 DGPS 2 429 RX+ DGPS 2 429 RX- J2-16 J2-23 J2-16 J2-23 DGPS 2 429 RX+ DGPS 2 429 RX- DGPS2 SPARE GPS 3 429 TX+ GPS 3 429 TX- J2-51 J2-50 J2-51 J2-50 GPS 3 429 TX+ GPS 3 429 TX- SPARE SERIAL RS 232 RX RS 232 TX RS 422 A RX+ RS 422 A RXRS 422 A TX+ RS 422 A TXRS 422 B RX+ RS 422 B RXRS 422 B TX+ RS 422 B TX- J2-33 J2-11 J2-39 J2-8 J2-31 J2-3 J2-45 J2-9 J2-30 J2-15 J2-33 J2-11 J2-39 J2-8 J2-31 J2-3 J2-45 J2-9 J2-30 J2-15 RS 232 RX RS 232 TX RS 422 A RX+ RS 422 A RXRS 422 A TX+ RS 422 A TXRS 422 B RX+ RS 422 B RXRS 422 B TX+ RS 422 B TX- SERIAL STRAPPING SDI 1 SDI 2 J2-44 J2-24 J2-38 J2-40 J2-44 J2-24 J2-38 J2-40 SDI 1 SDI 2 STRAPPING 429 TX SPEED SELECT ARINC 419/429 SELECT 429 TX SPEED SELECT ARINC 419/429 SELECT TIME MARK PULSE OUT+ TIME MARK PULSE OUTHAVEQUICK PPS IN PPS OUT TIMING J2-25 J2-53 J2-19 J2-47 J2-43 J2-25 J2-53 J2-19 J2-47 J2-43 TIME MARK PULSE OUT+ TIME MARK PULSE OUTHAVEQUICK PPS IN PPS OUT TIMING FAULT GNSS FAULT J2-26 J2-26 GNSS FAULT FAULT PY CONTROL PANEL J4-A J4-B J4-C J4-D J4-E J4-F J4-A J4-B J4-C J4-D J4-E J4-F J2-17 J2-46 J4-A J4-B J4-C J4-D J4-E J4-F J2-17 J2-46 J4-A J4-B J4-C J4-D J4-E J4-F PY CONTROL PANEL ZEROIZE SPS/PPS MODE ZEROIZE SPS/PPS MODE KEY STATUS J2-49 +28VDC +28VDC J2-49 KEY STATUS SPARE Reserved N/C N/C N/C Reserved N/C N/C J2-10 J2-21 J2-22 J2-29 J2-32 J2-35 J2-37 S2 KYK-1 AUDIO-6 LP1 KEY STATUS 1 LP2 GNSS FAULT 1 A B C D E F S3 F E D C B A SPS/PPS ZEROIZE LP3 GNSS FAULT 2 LP4 KEY STATUS 2 KYK-2 AUDIO-6 J2-10 J2-21 J2-22 J2-29 J2-32 J2-35 J2-37 Reserved N/C N/C N/C Reserved N/C N/C SPARE TA12 RPU TA12 RPU DRAWING 24835-10-IN-DUAL Figure 2-1. D, August 2000 2-5/6 TNL TA-12 GPS Receiver T 1. 06 TABLE 1 - J2 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 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 SIGNAL NAME DADS2 429 RXGPS1 429 TXRS422 A TXGROUND FMS/IRS 1 429 RXFMS/IRS 2 429 RXGPS2 429 TXRS422 A RXRS422 B RXRESERVED RS 232 TX DADS1 429 RXGPS1 429 TX+ GPS2 429 TX+ RS422 B TXDGPS2 429 RX+ ZEROIZE FMS/IRS 3 429 RXHAVEQUICK FMS/IRS 2 429 RX+ N/C N/C DGPS2 429 RXSDI2 TIME MARK PULSE OUT+ GNSS FAULT DADS1 429 RX+ DADS2 429 RX+ N/C RS422 B TX+ RS422 A TX+ RESERVED RS 232 RX FMS/IRS 1 429 RX+ N/C FMS/IRS 4 429 RX+ N/C 429 TX SPEED SELECT RS422 A RX+ ARINC 419/429 SELECT FMS/IRS 3 429 RX+ FMS/IRS 4 429 RXPPS OUT SDI1 RS422 B RX+ SPS/PPS Mode PPS IN * WAGE ENABLE KEY STATUS GPS 3 429 TXGPS 3 429 TX+ DGPS 1 429 RX+ TIME MARK PULSE OUT DGPS 1 429 RXGROUND 8. 920 8. 15 Z 4X ø. 204 . 57 DATA J2 MIL-C-38999 SERIES 2 16-35 CONFIG PIN RECEPTACLE SEE TABLE I FOR PIN ASSIGNMENTS MATES WITH MS27484T16F35S J4 MIL-C-55116 6 PIN AUDIO SEE TABLE 3 FOR PIN ASSIGNMENTS MATES WITH M55116/4-3 2X 2. 500 5. 00 3. 80 Y 2. 23 J3 ANT RF INPUT SMA JACK MATES WITH SMA PLUG PWR J1 MIL-C-38999 SERIES 2 8-98 CONFIG PIN RECEPTACLE SEE TABLE 2 FOR PIN ASSIGNMENTS MATES WITH MS27484T8F98S 2X 1. 25 . 28 . 93 SEE DETAIL A . 29 . 67 X . 28 8-32 X . 375 LG 1. 40 1. 06 9. 50 2. 07 INTERNAL STAR LOCK WASHER 8-32 UNF NUT DO NOT EXCEED 19 in-lbs TABLE 2 - J1 PIN # SIGNAL NAME TABLE 3 - J4 PIN # A B C D E F SIGNAL NAME KYK REFERENCE KYK ON KYK REQUEST KYK DATA KYK CLOCK NC GND WIRE GROUND TERMINAL A B C Vin + Vin N/C DETAIL A GROUND WIRE INSTALLATION TABLE 4 PART NO. NAME TASMAN ARINC-12 (TA-12) WEIGHT (LBS) 2. 9 VOLTAGE INPUT 22-30. 2 VDC MEETS DO-160C SECTION 16 CATEGORY A CENTER OF GRAVITY ±10% X 4. 75 Y 2. 55 . 95 DRAWING NO 24835-10-IN * Future use 24835-10 Figure 2-2. D, August 2000 2-7/8 TNL TA-12 GPS Receiver T 2. 686 . 05 CG 1. 343 GPS L1/L2 4X ø . 218 . 229 . 385 X 100° EQ SPACED ON 1. 343 B. C. 2. 686 . 10 ø3. 50 DO NOT PAINT 1. 343 CG . 70 . 20 R7. 33 ø1. 25 REF CABLE . 73 . 17 TNC JACK TABLE 1 PART NO WEIGHT 35094 7 oz NOTES 1. USE FASTENERS SUPPLIED WITH ANTENNA TO MOUNT TO VEHICLE. . 26 DRAWING NO 35094-IN Figure 2-3. [. . . ] D, August 2000 TNL TA-12 GPS Receiver T A. A. 1 RTCA/DO-160C Environmental Qualification Forms Receiver/ARINC Unit RTCA/DO160-C Environmental Qualification Form Nomenclature Part Number Manufacturer Address TNL TA-12 GPSSU 24835-10 Trimble Navigation 2105 Donley Drive Austin, TX 78758 USA Para. 4. 0 5. 0 6. 0 8. 0 9. 0 10. 0 11. 0 12. 0 13. 0 14. 0 15. 0 16. 0 17. 0 18. 0 19. 0 20. 0 21. 0 22. 0 23. 0 24. 0 Conducted Tests Category B1 * Category B Category A Category B Category X Category X Category X Category X Category X Category X Category Z Category A Category A Category A Category Z Category V Category Z Category A3E3 Category X Category X Conditions Temperature and Altitude Temperature Variation Humidity Vibration Explosion Waterproofness Fluids Sand and Dusts Fungus Salt Spray Magnetic Effects Power Input Voltage Spike Conducted Audio Conducted Susceptibility Induced Signal Susceptibility Radio Frequency Susceptibility Emission of Radio Freq. Energy Lightning Induced Transient Lightning Direct Icing *The altitude was modified to 51, 000 feet. A, August 1998 A-1 T A. 2 GPS Antenna Nomenclature Part Number TSO Number Manufacturer Address TNL TA-12 GPS Receiver RTCA/DO 160-C Environmental Qualification Form ARINC 743A-2 35094 C-129 Sensor Systems 8929 Fullbright Ave. [. . . ]