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RI-TRP-RR2B-30 Texas Instruments 32mm Glass Transponder 0-RFIDT visit Texas Instruments
RI-TRP-R9WK-03 Texas Instruments 12mm Wedge Transponder 0-RFIDP visit Texas Instruments
RI-TRP-R9QL-20 Texas Instruments 30MM DISK TRANSPONDER 1-RFIDP -25 TO 85 visit Texas Instruments
RI-TRP-WR3P-30 Texas Instruments 23mm Glass Transponder R/W 0-RFIDT visit Texas Instruments
RI-TH1-CB1A-00 Texas Instruments 13.56-MHz Vicinity Card Transponder 0-RFIDP visit Texas Instruments
RI-TRP-DR2B-30 Texas Instruments 32mm Glass Transponder Multipage 0-RFIDT visit Texas Instruments

mode s transponders

Catalog Datasheet MFG & Type PDF Document Tags

S-1403C

Abstract: atc 1400a maintenance manual Avionics S-1403DL/MLD Mode S Accessory Unit The S-1403DL/MLD provides a complete test solution for Mode S and Mode S "Datalink" capable transponders · Easy to operate Operation · , specified by RTCA/DO-181 to the ATC-1400A for testing ATCRBS and Mode S transponders including Data Link , Control Radar Beacon Systems (ATCRBS) and Mode Select (Mode S) transponders. Interconnect The S , defined screens for user specific tests · Two-year limited warranty The S-1403DL/MLD Mode S
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S-1403C atc 1400a maintenance manual S1403c mode s transponders OPERATION MANUAL ATC-1400A S-1403DL S-1403DL/MLD S-1403DL/MLD/ATC-1400A

arinc 629

Abstract: ARINC 629 sim Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a , ), serial-interface-module (SIM) and terminal-controller (TC). The development of ARINC 629, and current mode coupling (CMC
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arinc 629 ARINC 629 sim 00-160C DO-160

KIR 1C

Abstract: KIR-1C Avionics IFF-701 Transponder Test Set The IFF-701 is an 'O' Level/1st Line, portable battery operated test set for testing IFF MK12/Mode S Transponders installed in airborne, naval or land based platforms. The IFF-701 may also be used for 'I' Level/2nd Line filter bench testing. · · Menu driven , Mode S XPDR tests compliant with test requirements of FAR Part 43 Appendix 'F'. Mode S Level 3 · 28.4 cm Width; 36.1 cm Depth; 27.9 cm Height Mode 4 KIR-1C interface, Stored Code operation, Crypto
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KIR 1C KIR-1C stanag 4193 stanag 4193 part V KIT-1C/TSEC battery vietnam factory MK12/M 4193/AIMS

DO-260

Abstract: ATC-601 : Your ATC-601 needs to have version 2.22 or above firmware fitted. Note: All Mode S transponders with , data computer to the Mode S transponder may be verified on the ATC-601 using the Mode S UF4 test. The altitude is displayed in the AC field. Q: What is the resolution/accuracy of the ATC-601 Mode S Altitude data? A: The UF4 test, displays Mode S altitude data to a resolution of 25 ft. The ATC-601 has no , transmission from the air data computer to the Mode S transponder. The ATC-601 just displays the digital data
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DO-260 DO-260A UF-24 ARINC DF11 UF21

stanag 4193

Abstract: KIT-1C/TSEC Avionics IFF-701Ti Transponder/Interrogator Test Set The IFF-701Ti is an 'O' Level/1st Line, portable battery operated test set for testing IFF MK12/Mode S Transponders and MK12 Interrogators installed in airborne, naval or land based platforms. The IFF-701Ti may also be used for 'I' Level/2nd Line , Mode S XPDR tests compliant with test requirements of FAR Part 43 Appendix 'F'. Mode S Level 3 · , parametric test limits to STANAG 4193/AIMS 97-1000 · Mode 4 KIT/KIR-1C interface, Stored Code
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KIT-1C/TSEC IFF-701Ti KIT-1c mode 5 IFF KIt 1C tsec stanag IFF-701T SIM-701

atc 1400a maintenance manual

Abstract: ATC-1400A Avionics SI-1404 MK12/Mode S IFF Accessory Unit SI-1404 provides a comprehensive 3rd Line/Depot Level test solution for next generation MK12/Mode S IFF transponders · Comprehensive Mode S , (Minimum Operational Performance) tests defined in RTCA/DO-181A, required in the Mode S transponder , parametric and protocol testing MK10A (Mode 1, 2, 3/A, C), MK12 (Mode 1, 2, 3/A, 4, C) and MK12/Mode S , Mode S DPSK modulation and monitors replies on Ant A (ATC-1400A). The ATC-1400A provides UUT power and
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DO181A MTL 5541 OPERATION MANUAL SI-1404 ATC1400 atc 1400a IEEE-488 RS-232 SI-1404/ATC-1400A

DD-03206

Abstract: mode s transponders ), Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20 , EDGE S I DE V I EW .0 5 3 2 M IN ( 1 .3 5 ) .0 6 8 8 M AX ( 1 .7 5 ) B .0500 (1.27) . 0 1 3 0 MIN ( 0 .3 3 ) . 0 2 0 0 MAX ( 0 .5 1 ) s e e n o te 7 .0 0 4 0 M IN ( 0 .1 0 ) .0 0 9 8 M AX ( 0 , .2 5 ) 45° S I DE V I E W 0 ° M IN 8 ° M AX L .0 1 6 0 M IN ( 0 .4 0 ) .0 5 0 0 M AX ( 1
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DO160C DD-03206 DD-03206VP-900 03206 discrete-to-digital interface DD-03206VP DD03206VP DO-160C

ifr 6000 maintenance manual

Abstract: RTCA-DO-260A transponders, both conventional ATCRBS and Mode S. In preparation for the installation of new air traffic , instituted required tests for Mode S transponders. FAR (Federal Aviation Regulations) Part 43, Maintenance , Transponder Configurations Mode S Address Blocks (Product Specific List) Mode S Address Blocks (Complete , ATCRS Class B Auto Test Screen Generic ATCRBS Auto Test Screen XPDR Test List Mode S XPDR Test List ATCRBS XPDR A/C Decoder/SLS Test Screen XPDR A/C Spacing Width Test Screen Power and Frequency (Mode S
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ifr 6000 maintenance manual RTCA-DO-260A ATC-600A TCAS-201 IFR 6000 7005-5841-000

ARINC429MESSAGE

Abstract: mode s transponders ) and Mode S Transponders, AC20-131, defines a discrete as "a separate, complete and distinct signal , REF C FIGURE 4. DD-03232 INPUT STRUCTURE HLTflTbT D G D T S Q b TSb TABLE 3. WORD MODE (16 , selected to produce alternating "1"s and "0"s to verify that ail address and data bits are operational , 8/16-bit microprocessor. FIGURE 2 illustrates this interface. The read cycle(s) should be proceeded , Volts, then the DD-03232 is in 8-Bit Mode. The following must also be modified: DO tied to D8 D1 tied to
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ARINC429MESSAGE 32-CHANNEL 00CHSG2 DD-03200 RTCA/DO-160C MIL-STD-883 1-800-DDC-1772

DD-03296FC-100

Abstract: Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a discrete as "a separate, complete , alternating "1 "s and "0"s data to verify that all address and data bits are operational. While these outputs , -bit microprocessor. FIGURE 2 illustrates this interface. The read cycle(s) should be preceeded by polling the device , ) If 8/16* Bits pin is tied to +5 Volts,then the DD-03296 is configured for 8-Bit Mode. The DO D1 D2 D3 , Structure for REF B and REF C II I FIGURE 4. DD-03296 INPUT STRUCTURE 5 TABLE 3. WORD MODE (16
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DD-03296FC-100 96-CHANNEL DDDIS009
Abstract: ), Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20 , alternating "1"s and "0"s data to verify that all address and data bits are operational. While these outputs , -bit microprocessor. FIGURE 2 illustrates this interface. The read cycle(s) should be preceeded by polling the device , ) If 8/16* Bits pin is tied to +5 Volts,then the DD-03296 is configured for 8-Bit Mode. The DO D1 D2 D3 , ) - - 4 > TEA · 10 ns Min TAE-*( ¡ » -IO n s Min I \ _ I -«I I I I -
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DD-03182DC-100 B-07/96-1M
Abstract: Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20 , INTERFACE "R O D S " FEATURES DESCRIPTION APPLICATIONS â'¢ HIRF Layer The DD-03296 device is a , Self-Test â'¢ Soft Failure Reporting Higher MTBUR â'¢ Optional ARINC 429 Output Port In d ic a te s , . Todayâ'™s systems address the interface with tailored circuits for each interface comprised of R-C input , . FIGURE 2 illustrates this interface. The read cycle(s) should be preceeded by polling the deviceâ'™s -
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DD-03182

mode s transponders

Abstract: c3996 Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a discrete as "a separate , USED NOT USED NOT USED NOT USED TEST PATTERN 1's and 0's NOT USED NOT USED TABLE 4. BYTE MODE (8 , alternating "1"s and "0"s to verify that all address and data bits are operational. While these outputs are , illustrates this interface. The read cycle(s) should be preceeded by polling the device's READY bit located , in 8-Bit Mode. The following must also be modified: DO tied to D8 D1 tied to D9 D2 tied to D10 D3
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c3996 7402 PATTERN DIMENSIONS 001D77M MIL-H-38534 B-10/95-2M

ARM-184

Abstract: ASM-663 selects config required for test. For ATCRBS and Mode S Transponders if the class of the transponder is , by the selected config. The Mode S tests are tailored automatically according to reported , automatically determine the Mode S transponder level. The selected config parameters may be displayed by pressing the INFO softkey. Ten predetermined configs are provided to meet ATCRBS, Mode S, MK10, MK12 , data field interpretation! All Mode S Format tests display parameter in engineering units. X PD R ­ U
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ARM-184 ASM-663 1030mhz ARINC 568 AC0820 Transponder ID 48 AN/ASM-663 AN/ARM-184

L25.000

Abstract: of Traffic Alert and C o llision A voidance S ystem s (TC AS II) and Mode S Transponders, AC20 , , built-in self-test autonomy, fault isolation and tolerance at the chip level. In the 96-channel mode, the device loses the capability of taking consen sus on the input states as well as mis m a tc h . T h e s e fe a tu re s are trip le redundant configuration specific. All other features are still available , Output Port DISCRETEIN PU TS 32 OR 9 6 , t,r + '3 SELO SELT _ S E I 2_ 1 MHZ RESET' EN ABLE* A
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L25.000 DD-03201 FC-110

CH85 capacitor

Abstract: Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a discrete as â'a separate , . The deviceâ'™s microprocessor output is an addressable 8bit or 16-bit tri-state port, which selects , , fault isolation and tolerance at the chip level. In the 96-channel mode the device loses the capability , : Input channel to corresponding reference input Input Common Mode Range: Input channel and , μA μA -0.1 -1.0 -1.0 0.1 1.0 1.0 mV -15 15 V VSS VDD Todayâ'™s
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CH85 capacitor J-3/08-0 1-800-DDC-5757 A5976

8065 microprocessor

Abstract: DD-03201FP-200 and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a discrete as "a , tolerance at the chip level. In the 96-channel mode the device loses the capability of taking consensus of , Self-test inputs Input Offset Voltage: Input channel to corresponding reference input Input Common Mode , /Open, Open/Gnd and 28 V/Gnd signals. When using the 32-channel mode, the design uses comparators in a , include: Fault Isolation: In 32-channel mode, triple-redundant com- 96-Channel: 269,326 hrs. 32
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8065 microprocessor DD-03201FP-200 L-10-08-0 L-10/08-0

tic 118

Abstract: 19 03201 01 orthiness Approval of Traffic Alert and Collision Avoidance System s (TCAS II) and Mode S Transponders, AC20 , TEST PATTERN 1's and 0's NOT USED EBB DD-03201 TABLE 4. 32 CHANNEL BYTE MODE (8-BIT BUS) ADDRESS , tolerance at the chip level. In the 96-channel mode, the device loses the capability of taking consen sus of , ell-su ited to data con centrator requirements. FEATURES · Universal Inputs - Configurable A s 28 , inputs a Input Offset Vottage: Input channel to corresponding reference input Input Common Mode Range
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tic 118 19 03201 01 DIODE CH71 6JCR CH95 DD-03201I D-03182DC-1
Abstract: Avoidance Systems (TCAS II) and Mode S Transponders, AC20-131, defines a discrete as â'a separate , . The deviceâ'™s microprocessor output is an addressable 8bit or 16-bit tri-state port, which selects , , fault isolation and tolerance at the chip level. In the 96-channel mode the device loses the capability , : Input channel to corresponding reference input Input Common Mode Range: Input channel and , μA μA -0.1 -1.0 -1.0 0.1 1.0 1.0 mV -15 15 V VSS VDD Todayâ'™s Data Device
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H-9/07-0
Abstract: Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Mode S Transponders, AC20 , . The deviceâ'™s microprocessor output is an addressable 8bit or 16-bit tri-state port, which selects , , fault isolation and tolerance at the chip level. In the 96-channel mode the device loses the capability , Common Mode Range: Input channel and corresponding reference input POWER SUPPLY REQUIREMENTS (Total , V VSS VDD Todayâ'™s systems address the interface with circuits tailored for each Data Device
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F-11/06-0
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