T2000UAV-S Installation & User Manual 01R1-9
Contents
1. To obtain warranty service please email or call the Microair Avionics Phone 6 7 4155 38 F 1 BL 7 4155 39 T2000UAV S Installation and User Manual 01R1 9 Page 24 of 24 24 April 20092. TH S E Install and User Manual EC2002 ALTITUDE ENCODER O O Oo OF Oe 0 O o O a ENCODER POWER ENCODER POWER GROUND A1 A2 A4 Bl B2 B4 Cl c2 C4 D4 DB15 CONNECTOR VIEWED FROM THE SIDE THE WIRES ARE SOLDERED TO SUPPRESSION OUT O SUPPRESSION OUT EXTERNALSTANDBYIN O TH S HE ni EXT STANDBY IN YT III Ta SS A C GROUND O A C GROUND O ET al 14 OR 28V IN O NOTES niani 1 414 OR 28V POWER INPUT TO HAVE A 5 AMP MAXIMUM CIRCUIT BREAKER 2 THE ENCODER STROBE LINE SHOULD 14 25 DB25 CONNECTOR VIEWED FROM THE SIDE THE WIRES ARE SOLDERED TO 28V A C GROUND 14 Or INTERFACE MICROAIR AVIONICS e T2000UAV S TRANSPONDER WIRING DIAGRAM WITH A 30 ALTITUDE ENCODER CN MICROAIR AVIONICS BE GROUNDED T2000UAV S Installation and User Manual 01R1 9 Page 18 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual MICROAIR AK 350 T2000 TRANSPONDER ALTITUDE ENCODER ENCODER POWER ENCODER POWER s ENCODER POWER GROUND GROUND STROBE A1 A2 A4 Bl B2 B4 R5232 RX R 232 TX DB15 CONNECTOR VIEWED FROM THE SIDE THE WIRES ARE SOLDERED TO V a A O 6 me nU SUPPRESSION OUT SUPPRESSION OUT EXTERNAL STANDBY IN EXTERNAL STANDBY IN T TER EXTERNAL IDENT EXTERNAL IDENT A C GROUND A C GROUND 14 OR 28V IN NOTES 14 OR 28V IN 1 14 OR 28V POWER INPUT TO HAVE 5AMP MAXIMUM CIRCUIT B
3. command successful mode Mode C s lt current operational mode gt v 13 6 write successful current voltage returned v 24 8 write successful current voltage returned z lt current software revision gt eg T2000U xx x x x J T T2000UAV S Installation and User Manual 01R1 9 Page 8 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 3 4 1 STANDBY S T To bring the TZ2000UAV S to the standby condition the s parameter is set to value t Then the transponder can then be powered down When the T2000UAV S is restarted it will return in standby The transponder should be commanded to the standby condition when the vehicle is on the ground The transponder is typically set to mode 3A or mode 3A C operation once airborne 3 4 2 MODE 3A S A The T2000UAV S transponder will respond to all mode A interrogations with the identity code set by the c parameter The transponder will also reply to all mode C interrogations with just the framing pulse no altitude data This ensures visibility to TCAS operators while the transponder is operating in mode A 3 4 3 MODE C S C The T2000UAV S will respond to all mode A interrogations with the identity code set by the c parameter and all mode C interrogations with the encoder s altitude data as defined by the a parameter The transponder will reply to both SSR and TCAS interrogations 3 4 4 IDENT I S The ident functi
4. the moment power is applied to the unit There is no software OFF command When power is removed from the T2000UAV S it will not respond to any software command When the T2000UV A S is turned on it is always in standby mode The mode A code will default to the last mode A code used AN Wr IMPORTANT NOTE mr 2 Always bring the T2000UAV S to standby before turning off the power If the transponder is powered off while it is in the process of transmitting ep damage may occur to the internal power supply and or the transmitter Damage of this type is not covered by the warranty A v No mode C code will be outputted until the T2000UAV S is supplied with altitude data either serial or Gillham which can be encoded by the transponder 9 3 SUPPRESSION IN OUT The suppression IN line is wired to other avionics such as DME to suppress the transponder s transmissions at times critical to the other equipment s operation The suppression OUT line does the reverse of the IN line It is wired to other avionic equipment to allow the T2000UAV S to suppress their transmissions at times critical to the T20Q00UAV S operation Seek the advice of a qualified Avionics Technician before attempting to wire out these functions If certified equipment is modified to operate in conjunction with the T2000UAV S installation then the installation of that equipment must be re inspected and re approved before operation 94 EXTER
5. 3 2 3 3 3 4 3 4 1 3 4 2 3 4 3 3 4 4 3 4 5 3 4 7 3 4 8 3 4 9 3 4 10 4 0 5 0 6 0 7 0 8 0 9 0 9 1 92 9 3 9 4 9 5 10 0 11 0 12 0 13 0 14 0 TABLE OF CONTENTS INTRODUCTION T2000UA V S DESCRIPTION T2000UAV S ANTENNA OPTIONS SOFTWARE CONTROL THE UAV S TERMINAL SOFTWARE THE UAV COMMAND STRUCTURE DATA SPEED VALID COMMANDS Standby s t Mode 3A s a Mode C s c Ident i s Altitude a Altitude Source d Encoder Power e Voltage v Reply Annunciator r y Ping Function p T2000UAV S INSTALLATION T2000UAV S TIE DOWN STRAP MODE C ENCODER ANTENNA COAXIAL CABLE WIRING CABLING POWER ON OFF SUPPRESSION IN OUT EXTERNAL STANDBY EXTERNAL IDENT TECHNICAL DRAWING WIRING DIAGRAMS PIN ASSIGNMENTS SPECIFICATIONS LIMITED WARRANTY Install and User Manual oweowowooo L N NAA VN A T2000UAV S Installation and User Manual 01R1 9 Page 3 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 1 0 INTRODUCTION The T2000UAV S is a special version of the T2000 Transponder designed for operation in unmanned aircraft This product is not TSO d due to the OEM nature of the management software The system consisting of the T2000UAV S and the OEM s management software control should collectively be submitted for compliance to TSO C74c as part of the OEM s type certificate The T2000UAV S is based upon the certified T2000SFL transponder and is know
6. 30 ALTITUDE ENCODER T2000UAV S Installation and User Manual 01R1 9 Page 20 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual MICROAIR T2000UAV S TRANSPONDER DB25 SUPPRESSION IN SUPPRESSION IN SUPPRESSION OUT SUPPRESSION OUT WIRE OUT ONLY EXTERNAL STANDBY IN gt EXTERNAL STANDBY IN IF REQUIRED EXTERNAL IDENT EXTERNAL IDENT GROUND GROUND RS 232 RX RS 232 RX RS 232 TX RS 232 TX 14 OR 28V IN 14 OR 28V IN GROUND A C GROUND A C GROUND S 10 TO 33VDC 14 25 DB25 CONNECTOR VIEW FROM REAR NOTES di 14 OR 28V POWER INPUT TO HAVE 5AMP MINIMUM CIRCUIT BREAKER 2 EXTERNAL IDENT SWITCH IF FITTED SHOULD BE MOMENTARY ON ONLY 3 EXTERNAL STANDBY SWITCH IS NORMALLY CLOSED TO GROUND TO OPERATE 4 SUPPRESSION IN LOW GOING HIGH gt 5Vdc lt 20Vdc SUPPRESSION OUT LOW GOING HIGH 5Vdc 3 RS 232 INTERAFCE IS NULL MODEM WITH NO HANDSHAKE MICROAIR AVIONCS 12000UAV S TRANSPONDER med WIRING DIAGRAM AVIONICS SERIAL ALTITUDE DATA INPUT T2000UAV S Installation and User Manual 01R 1 9 Page 21 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 12 0 PIN ASSIGNMENTS The DB plugs for use with the T2000 series Transponders require the following pin assignments PIN 1 PIN 2 PIN 3 PIN 4 PIN 5 PIN 6 PIN 7 PIN 8 PIN 9 PIN 10 PIN 11 PIN 12 PIN 13 PIN 14 PIN 15 PIN 16 PIN 17 PIN 18 PIN 19 PIN 20 PIN 21 PIN 22 PIN 23 PIN 24 PIN 25
7. 9 Microair Avionics T2000UAV S Install and User Manual 70 ANTENNA Mount the transponder antenna as per the manufacturer s installation instructions Try and keep the cable runs as short as possible In a composite airframe a suitable ground plane will be reguired Avoid mounting the antenna inside a fuselage that is all metal or carbon fibre For fiberglass fuselages the antenna may be mounted internally but must still point downwards and have an adeguate ground plane Alternatively an approved dipole strip antenna may be used The dipole strip must be installed in accordance with the manufacturer s instructions To avoid possible interference the antenna must be mounted a minimum of 200mm inches from the T2000UA V S main unit The transponder antenna should be mounted 2metres 78 inches from the DME antenna 1 5 metres 58 inches from the ADF sense antenna and Imetre 39 inches from TCAS antennas 8 0 COAXIAL CABLE The T2000SFL allows for 1 5dB cable loss from the unit to the antenna The installer should consider carefully what type of coaxial cable is to be used so that this loss limit is not exceeded The cable should be terminated with silver plated BNC connectors where possible 3 2mm 1J8 L 6mm 1 16 a i Step 4 y Tft 142W 70dBm RG213 A U 125mm 0 26dB m 575m Mil Spec 5 0 08dB ft 19ft iod 70dBm RG223 U 100mm 0 47dB m 3 2m amp wy onam i Mm 50mm 0 60dB
8. MAND STRUCTURE The T2000UA V S is controlled by a series of simple commands The T2000UAV S can be commanded to set a code and to operate in a particular mode Once the code is set and the operating mode decided the T2000UAV S will operate until another command is received The status the T2000UAV S various operating parameters can be queried A query command returns a value for that particular parameter The operator can address the TAZ000UAV with a command from the command set via an RS232 interface The command reguires the correct syntax to be valid The command string will consist of STXx lt command gt ETX Where STX is the non printable ASCII character 02 ETX is the non printable ASCII character 03 x is a valid command lt command gt maybe either or a string of ASCII characters if the lt command gt is a this will evoke a response for that command 3 3 DATA SPEED The RS232 interface for the T2000UAV S has a data rate of 9600 N 8 1 P where 9600 baud rate of 9600 8 8 data bits 1 1 stop bit P with XON XOFF Refer to section 11 0 for wiring details and pin assignments T2000UAV S Installation and User Manual 01R1 9 Page 7 of 24 1 June 2009 Microair Avionics T2000UA V S 3 4 VALID COMMANDS Install and User Manual Altitude a Read Write r Assigned Code Read Write Assign altitude source d Read Write Encoder power control e Read Write i Ident Read Write p Ping Fu
9. Miecroair Avionies R l i a 8 i r i UN Microair Avionics Pty Ltd Airport Drive Bundaberg Queensland 4670 Australia Tel 61 741 553048 Fax 61 741 553049 e mail sales microair com au MICROAIR Microair Avionics T2000UAV S Install and User Manual About This Document This supplement describes the installation option and software controls for the T2000UAV S transponder operating with software revision TZ20Q00UAV S_1R6 5 Microair reserves the right to amend this supplement as required to reflect any enhancements or upgrades to the T2000 M R 0 M N transponder series Microair Avionics Pty Ltd REVISION STATUS 18 01 06 Separated from the T2000UA V Rev 1 4 manual 1 1 29 03 06 Additional installation data added 1 2 01 04 06 Additional command set data added O1R1 3 04 05 06 Weight data amended OIRI 4 21 11 06 SMA version deleted amp Encoder data added OIR1I 5 24 01 08 N command deleted O1R1 6 12 05 08 Warranty Statement Update 01R1 7 25 02 09 Updated Limited Warranty Statement O1R1 8 24 04 09 Change email to repair microair com au OIR1 9 01 06 09 Ping function amended The T2000UA V S Transponder is not a TSO d product T2000UA V S Installation and User Manual 01R1 9 Page 2 of 24 1 June 2009 Microair Avionics T2000UAV S 1 0 2 0 A 3 0 3 1
10. NAL STANDBY The external standby can be wired to a remote switch When the line is taken to ground the T2000UAV S will return to standby mode and stay there regardless of the value for s parameter The s parameter cannot be queried while the external standby line is grounded Once the external standby line has been released from ground the T2000UAV S will revert to the last s parameter setting 9 5 EXTERNAL IDENT Future development T2000UAV S Installation and User Manual 01R1 9 Page 15 of 24 1 June 2009 Install and User Manual T2000UA V S Microair Avionics 10 0 TECHNICAL DRAWING POM Lect DDO ABS 1 5 T N 2 C A So NV YL hal NS 1 June 2009 Page 16 of 24 T2000UAVV S Installation and User Manual 01R1 9 Microair Avionics T2000UAV S Install and User Manual 11 0 WIRING DIAGRAMS T2000UAV S with EC2002 Altitude Encoder T2000UAV S with AK 350 Altitude Encoder T2000UAV S with A 30 Altitude Encoder T2000UAV S with serial altitude data interface T2000UAV S Installation and User Manual 01R1 9 Page 17 of 24 1 June 2009 Microair Avionics T2000UAV S MICROAIR T2000 TRANSPONDER DB15 8 DB25 iW ENCODER POWER op kaled 3 L Ses a mag 9 Al one 2 a Fm s ares SE Bl E 2 a co _ 9 s MES 10 n N CH oloo o l _ Hb D4 of RS232 RX ome a mii e a NOT WIRED o NOT WIRED o NOT WIRED i 3 SUPPRESSION IN O SUPPRESSION IN
11. NOT WIRED SWITCHED MODE C ENCODER POWER OUTPUT GROUND RS232 RX RS232 TX NOT WIRED NOT WIRED SUPPRESSION IN GILLHAM ALTITUDE A1 GILLHAM ALTITUDE A2 GILLHAM ALTITUDE A4 GILLHAM ALTITUDE B1 GILLHAM ALTITUDE B2 SUPPRESSION OUT EXTERNAL STANDBY IN EXTERNAL IDENT GILLHAM ALTITUDE B4 GILLHAM ALTITUDE Cl GILLHAM ALTITUDE C2 GILLHAM ALTITUDE C4 GILLHAM ALTITUDE D4 POWER GROUND POWER GROUND POWER 14 OR 28 VOLTS DC 10 33 VOLTS POWER 14 OR 28 VOLTS DC 10 33 VOLTS 25 DB25 CONNECTOR VIEW FROM REAR T2000UAV S Installation and User Manual 01R1 9 Page 22 of 24 1 June 2009 Microair Avionics 13 0 SPECIFICATIONS RTCA Compliance Transmitter Receiver Input Power Operational Modes Temperature Dimensions Weight T2000UAV S Install and User Manual DO 144 DO 160D DO 178B Level C 1090MHz 0 2MHz 200W Pulse Output 80nS Rise Time 120nS Fall Time 10 to 72dBm Dynamic Range 1030MHz Centre Frequency SMHz Pass band 3dB 10 33Vdc 100 150mA 28V 150 200mA 14V Standby Mode 3A 4096 codes Mode 3A C 20 C to 55 C Width 6lmm Height 61mm Length 134mm 520g 1 1 Ibs Specifications are subject to change without notice T2000UAV S Installation and User Manual 01R1 9 Page 23 of 24 1 June 2009 14 0 LIMITED WARRANTY Limited Warranty The warranty period for amy Moctar Avionics manufnctured article is nuit uu eae eee MOAR mi is valid for 2
12. REAKER 2 THE ENCODER STROBE LINE SHOULD BE GROUNDED 14 25 gt S DB25 CONNECTOR A af el eye on re VIEWED FROM THE SIDE THE E E S ia i WIRES ARE SOLDERED TO v MICROAIR AVIONICS T2000UA V S TRANSPONDER MICROAIR WIRING DIAGRAM AVIONICS WITH AK 350 ALTITUDE ENCODER T2000UA V S Installation and User Manual 01R 1 9 Page 19 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual MICROAIR A 30 T2000 TRANSPONDER ALTITUDE ENCODER DB15 DB25 ENCODER POWER cis ENCODER POWER ERS IT i H il Ll 2 i O STROBE a Te n nn 2 A2 o 10 3 Oo A2 a lt a ka il 2 T 12 5 a TE an keder a Tt Te c ET TS C2 palad ldd o c2 RR ol a0 tl oe a l Loli a 4 RS232 RX G l a r r At 9 SWYN 6 15 NOT WIRED o NOT WIRED s IY DB15 CONNECTOR NOT WIRED o 1 VIEWED FROM THE SIDE THE WIRES ARE SOLDERED TO 8 SUPPRESSION IN SUPPRESSION IN ND 1 i 0 einen sn WIRED IF REQUIRED EXTERNAL STANDBY IN G rmn n r EXTERNAL STANDBY IN EXTERNAL IDENT 3 p EXTERNAL IDENT A C GROUND n m A C GROUND O fon Y 14 OR 28V IN o a NOTES 14 OR 28V IN r amne i 1 14 OR 28V POWER INPUT TO HAVE 5AMP MAXIMUM CIRCUIT BREAKER i a 2 THE ENCODER STROBE LINE SHOULD BE GROUNDED eens 14 25 S z DB25 CONNECTOR iE ERL VIEWED FROM THE SIDE THE 9 9 S U WIRES ARE SOLDERED TO OF ay a MICROAIR AVIONICS T2000UAV S TRANSPONDER MICROAIR WIRING DIAGRAM AVIONICS WITH A
13. WING MATISO FOR STRAP DETAILS NNNNNNNNNNNNNN NNNNNNNNNNNNNNNNN E Z 7 7 4 5 5 F ina Z A PA Z Z 7 d ERC CONNECTOR ATTACH STRAP TO CROSS MEMBER WITH M3 OR TRAKSPONDER ARTERNA EOUMNALENT SCREWS amp ENSURE THE EG AV 22 TRANSPONDER IS SECURELY RESTRAINED Sra ONS DO KOT 719 SKD HE AE IT MARY MST Be Come Mm MLLMETRES CALE TAT TE GRISE 2 DIAR AOS TWLL Mn TG O bere care TEE WE DES iij TEDDE 200 A MALES eas ATTACH STRAP TO BULKHEAD WITH M3 OR EQUIVALENT SCREWS amp ENSURE THE TRANSPONDER IS SECURELY RESTRAINED r a REFER TO VICROAIA DRAW IAG MAT15 FOR STRAP DETAILS STRAP NOT TO CONTACT LOCK NUTS Q NOT REMOVE CHASSIS LID SCREWS AND USE FOR MOUNTING DB25 COKNECTOR SAKTEKKA GROUND PLANE REFER TO MIEZROAIR DRAWING FUSELAGE VWATXI FOR DETAILS ELLE LLL TRANSPONDER ANTENNA ds DO KOT 71 LAAD 5 EE NT AMSAT AST BE OE ED AVe LAND I M PROJECTION YM DE HER TE OOE ATT NION a et lt Sale Ate STE tE Sea E KAE NS JM PS MM KBM 1 2 aan oe SEMEL TI EA NCES AAS WS dU N s RES Pati sE ins THSBES 1 40 0 AaS il T r x i ae a E T2000UAV S Installation and User Manual 01R1 9 Page 11 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 5 0 T2000UAV S TIE DOWN STRAP Microair recommends a simple tie down strap to hold the transponder in place Drawing MA1156 shows the layout and use of a simple example Never use the case screws as part o
14. connections be run at the time of installation even though they may not be required at this stage Adding additional wiring to the loom at a later stage may be very difficult All wiring should be installed in accordance with FAA AC43 13 1A Chapter 11 or equivalent Microair recommends the following cable types for connection of the TZ000UAV S Power Input 18 AWG TEFZEL 22759 16 16 Red and Black Wire External Connections 22 AWG TEFZEL 22759 16 22 Wire or 22 AWG TEFZEL 27500 22TG1T14 Single core shielded Encoder Power 22 AWG TEFZEL 22759 16 22 Red and Black Wire Encoder Data 22 AWG TEFZEL 22759 16 22 White Wire When terminating the DB plugs for connection to the TAZ000UA V S ensure that the wires are securely soldered to the pins and that each wire 19 separately insulated with heatshrink tubing Tinned wire Soldered with heatshrink Locking bolts tightened The DB 25 plug are to be secured to the T2000UAV S with machine screws or thumb screws The DB 15 should also be secured to the encoder either with screws or mechanical sliding lock if fitted to some types of encoder If your encoder is fitted with a slide locking mechanism the encoder manufacturer s plug should be used to ensure correct locking action T2000UAV S Installation and User Manual 01R1 9 Page 14 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 92 POWER ON OFF The T2000UAV S has no ON OFF control function The unit is on from
15. f the mounting system for the transponder Always locate the strap over the chassis at a point which remains clear of the filter lock nuts O NOT REMOVE CHASSIS LID SCREWS AND USE FOR MOUNTING STRAP NOT TO CONTACT LOCK NUTS STRAP ASSY DETAIL BLANK LAYOUT SCALE 1 2 SCALE THE ORANG 12 COPYRIGHT ANO MIET MOT BE COPED gt E JW RL Bed mi ii 2000U AV S FE 3 7 TERAL 20 X 1 5 ALUMINIUM STRIP HE DOAN STRAP GRADE 5005 a NATURAL 6 0 MODE C ENCODER Mount the mode C blind encoder as per the manufacturer s installation instructions All wiring can be run back to the T2000UAV S for connection refer wiring diagram The power for the encoder is supplied from the T2000UAV S This power is switched when the T2000UAV S is turned on I IMPORTANT NOTE a N L Most encoder manufacturers advise of a warm up period for their product before altitude data is supplied The period can typically be up to 10 minutes wm v Where the OEM intends to use their own barometric altitude data source it should comply to TSO C88a standard to be sure of compatibility with the T2000UAV S Although it is unlikely that the encoder source in a UAV installation will reguire switched power from the T2000UAV S it is recommended that the ground be wired with the data lines in all cases This will ensure correct signal operation of the Gillham code T2000UA V S Installation and User Manual 01R1 9 Page 12 of 24 1 June 200
16. his data report to the T2000UAV S no slower than 1Hz Where the altitude data cannot be detected from the assigned source or the data cannot be encoded no altitude data will be outputted The mode C response will be framing pulses only The T2000UAV S will question the altitude data with a via the RS232 serial interface T2000UAV S Installation and User Manual 01R1 9 Page 9 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 3 4 7 ENCODER POWER E When using an altitude encoder it may be desirable to only have it powered up when the transponder is operating in mode C This may save power as most encoders will typically draw 125 to 150mA when operating The operator should allow up to 7 minutes for the encoder to warm up before valid altitude data is outputted from the encoder 3 4 8 VOLTAGE V The T2000UAV S will report the current vehicle bus voltage by polling the v parameter To use this function operator must first set the reference bus voltage by setting v 1 for 14V operation or v 2 for 28V operation 3 4 9 REPLY ANNUNCIATOR R Y A conventional transponder normally has an annunciator of some type typically a flashing LED to indicate the rate of reply to SSR interrogations This indication represents whether the transponder has made a reply to a sweep The rotational speed of the radar is 100 deg sec hence the Annunciator should flash every 3 6 seconds The equivalent fu
17. m 2 5m 2 0 18dB ft Sn ae 70dBm 50mm 0 68dB m 2 2m awe 0 21dB ft h 142W 10dBm 50mm 0 47dB m 3 2m 2 0 14dB ft 10ft 142W 70dBm IMPORTANT NOTE Do not exceed the minimum bending radius Tight bends will introduce losses in the cable which may affect the performance of the transponder When fixing the coax cable in the airframe do not strangle the cable with tight cable ties This can distort or damage the coax screen T2000UAV S Installation and User Manual 01R1 9 Page 13 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 9 0 WIRING The T2000UAV S Transponder receives primary power 14V or 28V dc from the aircraft s power source Power connections voltage and circuit breaker requirements are shown on the wiring diagram The length of the power supply wires to parallel pins should be approximately the same length so that the best distribution of current can be effected Microair recommends that the encoder be installed and wired in accordance with the manufacturer s installation instructions It is very important to secure all D series plugs via their security screws before operation Aircraft vibration may disconnect a D series plug if it not secured Where possible the antenna coaxial cable should be run separately to all other wiring on the aircraft from the transponder 9 1 CABLING Microair recommends that wiring for all of the TA000UAV S functions and
18. n to comply with the following Environmental RTCA DO 160D Software RTCA DO 17 B Transponder Function RTCA DO 144 Transmitter Operation FCC Approval T2000UA V S Installation and User Manual 01R1 9 Page 4 of 24 1 June 2009 Microair Avionics T2000UAV S 2 0 T2000UAV S DESCRIPTION The UAV S version of the T2000SFL has no display The chassis has been truncated by having the display housing milled off The front face is plated off and sealed A command set allows the UAV s flight management system to have full functional control over the transponder The RS 232 interface is accessed from the DB 25 connector on the rear face of the chassis The T2000UAV S requires a standard Gillham code altitude encoder to supply altitude data over a 10 line parallel interface Install and User Manual The T2000UAV S features remote switching options available from the rear DB 25 connector for remote standby and remote ident functions 2 1 T2000UAV S ANTENNA OPTIONS The T2000UAV S can be supplied with a standard BNC connector located on the rear face of the chassis adjacent to the DB 25 The T2000UAV S can be supplied with a standard TNC connector located on the rear face of the chassis adjacent to the DB 25 T2000UAV S Installation and User Manual 01R1 9 Page 5 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 3 0 SOFTWARE CONTROL The T2000UAV S can be c
19. nction r Reply Annunciator Operational Status Read Write Bus Voltage Read Write Z Software Revision a a xxxxx where xxxxx altitude in feet a amp where amp altitude in feet c 2212 set code to 2212 c ask for assigned code d g set altitude source Gillham d s set altitude source Serial e o set encoder power always ON e c set encoder power mode C only e i s Squawk Ident i ask for current ident status s t command standby mode s a command Mode A operation s c command Mode C operation s ask for current operational mode v set bus voltage to 14V v 2 set bus voltage to 28V a lt current altitude data gt eg 1234F a xxxxx writes altitude data in feet to T2000UAV a invalid altitude data c 2212 code write successful c lt current assigned code gt d g altitude source Gillham d s altitude source Serial d lt current altitude source setting gt e o Encoder power on in both mode A and C e c Encoder power on in mode C only e lt current encoder power state gt i 1 1 Ident active O Ident inactive i lt current Ident state gt p y yes ping cycle was successful p n no ping was not successful is sent if a reply was made in the last 3 6 seconds no annunciation character is sent r lt current reply annunciation state gt s t command successful mode standby s a command successful mode Mode 3A s c
20. nction for the T2000UAV S is the r command which activates the reply annunciator When activated r y the TAZO00UAV S will send a single character if there was a reply made in the preceding 3 6 seconds When not activated r n no character is sent The operator can query the status of the reply annunciator function r and the TZ2000UAV S will reply with the current function state 3 4 10 PING FUNCTION P The ping function is a self test of the RF sections of the transponder without the need for a transponder test set The T2000UA V S will respond to the ping command p by emitting a narrow invalid pulse from the transmitter and detecting the same pulse back through the receiver If the TZ000UA V S is able to complete the transmission cycle p y is returned to the operator If the TZ000UAV S is not able to complete the transmission cycle p n is returned to the operator A Y i F The ping function will only operate if the transponder is in mode a or C lt The ping function will not operate while the transponder is in standby mode T2000UAV S Installation and User Manual 01R1 9 Page 10 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 4 0 T2000UAV S INSTALLATION 3 USELAGE TRAP KOT TO CONTACT LOCK KUS FO KOT REVOVE CHASSIS LID SCREWS AND USE FOR MOUNTING DB25 COBMKECTOR ANTENNA GROUND PLANE FER TO MICROAIR DRAWING REFER TO VICROAIR DRAWIAG WN CE rindi DRA
21. on is performed at the request of ATC to squawk ident To initiate the ident function the parameter is set to s The T2000UAV S will switch to ident mode which will add an additional data bit to the outgoing replies The additional data bit makes the transponder return on the ATC display flash to assist the controller with identification The transponder will remain in ident mode for 18 seconds and then return to the previous mode of operation 66599 1 3 4 5 ALTITUDE A The T2000UAV S will reply with the current mode C value If the T2000UAV S is configured to operate with an altitude encoder the T2000UAV S will reply with the current barometric altitude from the encoder If the T2000UAV S is configured to operate with a serial altitude data source the TZ000UA V S will reply with the last received altitude data value 3 4 6 ALTITUDE SOURCE D The T2000UAV S can accept altitude data for the mode C response either from a Gillham d g for 10 line parallel source or from a serial d s for RS232 source When d g is selected the T2000UA V S will look to the 10 line Gillham input for data from an altitude encoder When d s is selected the T2000UAV S will look for altitude data to be passed via the a command on the RS232 serial data link The altitude data source shall send the a lt altitude value gt where the altitude value is between 1000 and 62000 feet in increments of 100 feet The altitude data source should issue t
22. ontrolled by issuing of commands in the form of ASCII characters sent and received over an RS232 interface The command set can be used to either poll the transponder of the status of a parameter or to command a function to a particular setting 3 1 THE UAV S TERMINAL SOFTWARE The T2000UAV S is supplied with terminal software to which it is capable of issuing all commands and polling for all parameters The terminal software is a simple EXE file and is compatible with windows 98 through to windows XP operating systems T2000U4 Terminal Software exe The terminal software is capable of issuing all of the commands to either poll for any of the parameters or to set any of the parameters to discrete values 5c Microair UAY Control U File Setup Operational Function System Parameters f Standby Mode Mode C Assigned Code SFI Status U pe rational Status Assigned Code APL Voltage Interrogation Status Interrogation Status CIW 2ey On Off SPI Status Low Voltage Setpoint High Voltage Setpoint m Altitude AIC Voltage High YVoltageSetpoint Ping Control Low Voltage Setpoint Firmware version Ping Operation Manual Command Comm Port w Connect Auto Sequence Label Control Panel Microair Avionics Pry Ltd T2000UAV S Installation and User Manual 01R1 9 Page 6 of 24 1 June 2009 Microair Avionics T2000UAV S Install and User Manual 3 2 THE UAV COM
23. years or the mi E AVIONICS In the absence of original Proof of Purchase the warranty will be valid for 2 years from Date of Factory Shipment as determined by Microair Avionics For Factory R ti offered for sale the warranty period commences from Date of Purchase amd is valid for 12 months Microair Avionics will at it sole discretion repair or replace any components which fail m mormal use such repairs or replacement will be made at no charge to the customer for parts or labour The customer shall be responsible for amy transportation costs for return of this product to Mircroair Pry Lid or an approved Microair Service Centre This warranty does not cover failures due to abuse misuse accident unmuthorised alteration or repairs cared out by parties other than Microair Aviomies or an approved Microair Avionics Service Centre This wamanty does not cover failures where the product has not been installed or operated in accordance with the Provisions of the User and Installanm E r LIABILITY ARISING UNDER DE OTHERWISE THIS WARRANTY GIVES YOU SPECIFI LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE AND COUNTRY TO COUNTRY HER t RESULTING FROM THE USE MISUSE OR Mricrenir Avionics may at it discretion refer product returns for repair or service to a service facility closest to you Microair Avionics reserves the right to repair or replace the product or software or offer a full refund of the purchase price at its sole discretion
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