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. 35536-00 Prepared by: Trimble Navigation, Ltd. 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. [. . . ] 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. Interconnections of a Typical Dual-Sided Aircraft Installation Rev. 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. TA-12 RPU (P/N 24835-10) Installation and Pin-Out Diagram Rev. 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. GPS Antenna (P/N 35094) Installation Drawing Rev. D, August 2000 2-9/10 TNL TA-12 GPS Receiver T CG 4. 75 4X 1. 50 X 45 . 06 4. 25 5. 250 5. 508 CG 2. 500 THIS IS STUPID 3. 00 2. 750 4X Ø. 163 +. 003 -. 000 INSTALL PEM FH-832-8 FROM FAR SIDE 4X Ø. 200 . 29 . 125 MAT'L THICKNESS 2. 460 6. 460 8. 920 9. 21 TABLE 1 WEIGHT 15oz DRAWING NO. Adapter Plate (P/N 33398) Installation Drawing Rev. D, August 2000 2-11/12 TNL TA-12 GPS Receiver T GPS 1 LOAD KYK PPS GPS 2 LOAD VALID P/Y GPS CONT. PANEL SPS ZERO VALID GPS 1 P/Y GPS KYK ENTRY PANEL GPS 2 Figure 2-5. D, August 2000 2-13/14 TNL TA-12 GPS Receiver T 3. 3. 1 Checkout GENERAL This section contains instructions for the checkout and troubleshooting of the TA-12 after it has been installed on the aircraft. More detailed operating instructions may be found in the FMS Pilots Operating Handbook. 3. 2 INSTALLATION CHECKOUT After all TA-12 aircraft interface wiring is complete, it is desirable to perform a final wiring configuration verification before initially installing and connecting the TA-12 LRUs. CAUTION Destruction of the TA-12 equipment could result if a wiring error in the power input circuits of the TA-12 is not detected and corrected, prior to installing the units. Refer to Figures 2-1 and 2-2 for connector pin configuration. Perform the following installation verification tests before initial installation of TA-12 LRUs. Use correct size pin adapters to monitor leads at each connector. Remove power from all aircraft systems interfacing with the TA-12 prior to performing ohmmeter checks. 3. 2. 1 Continuity Checks Using Figure 2-2, TA-12 RPU (P/N 24835-10) Installation and Pin-out Diagram, verify continuity between each TA-12 pin and its opposite end termination. Resolve all discrepancies in continuity checks > 1 ohm before continuing. 3. 2. 2 Resistance Checks If any appreciable resistance is detected when performing above continuity checks, a poor connection may be indicated. Correct condition and re-verify continuity. 3. 2. 3 No Shorts to Ground Checks Check resistance to ground of each connector pin with ohmmeter set to highest scale. When a path to ground is detected, verify its validity with Figures 2-1 and 2-2. [. . . ] Energy Lightning Induced Transient Lightning Direct Icing A. 3 TA-12 System-Level Pin-Outs The pin-outs for each of the four connectors (J1 through J4) are listed in Tables A-1 through A-4, respectively. Connector J1 Pin-Outs (3-Pin) Pin A B C Signal Name Vin+ VinN/C Description 28 VDC nominal Power Return A-2 Rev. A, August 1998 TNL TA-12 GPS Receiver T Table A-2. Connector J2 Pin-Outs (55-Pin) Pin 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 Signal Name DADS 2 429 RXGPS 1 429 TXRS-422 A TXGROUND FMS/IRS 1 429 RXFMS/IRS 2 429 RXGPS 2 429 TXRS-422 A RXRS-422 B RXreserved RS-232 TX DADS 1 429 RXGPS 1 429 TX+ GPS 2 429 TX+ RS-422 B TXDGPS 2 429 RX+ ZEROIZE ICD-GPS-150 RS-232 Transmit Digital Air Data System ARINC 429 Receive ARINC 429 Transmit ARINC 429 Transmit TIPY RS-422 Transmit Differential GPS ARINC 429 Receive Emergency Zeroize Ground = Ram Clear Open = No Zeroize IRS ARINC 429 Receive HaveQuick Timing Output FMS ARINC 429 Receive Description Digital Air Data System ARINC 429 Receive ARINC 429 Transmit ICD-GPS-150 Aircraft Ground FMS ARINC 429 Receive FMS ARINC 429 Receive ARINC 429 Transmit ICD-GPS-150 RS-422 Receive TIPY RS-422 Receive 18 19 20 21 22 23 24 25 26 FMS/IRS 3 429 RXHAVEQUICK FMS/IRS 2 429 RX+ N/C N/C DGPS 2 429 RXSDI2 TMP OUT + GNSS FAULT Differential GPS ARINC 429 Receive Source Destination Identifier 2 Ground = 1 Open = 0 Time Mark Pulse Output RS-422 Levels General Fault Discrete Output Ground (Sinks 150 mA) = Fault Open = No Fault Faults Detected : GPS Core Failure PPSSM Failure Oscillator Drift Timer Failure A2D Failure Internal Task Failure Antenna Open Antenna Disconnected Rev. 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