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Funkwerk 800ATC-(200)-(200), Operation And Installation

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Funkwerk 800ATC-(200)-(200) Operation And Installation Download Page 4

TRT800 / P/N 800ATC-(200)-(200)  

Operation and Installation 

 

 
 4 

Document-No: 03.2102.010.71e / Revision: 2.02

3.8.3

 

Antenna Wiring............................................................22

 

3.9

 

Post-Installation Check ..........................................................22

 

3.10

 

Starting Up .............................................................................23

 

3.11

 

Accessories............................................................................23

 

3.12

 

Drawings ................................................................................24

 

3.12.1

 

Dimensions..................................................................24

 

3.12.2

 

Mounting Advices ........................................................24

 

4

 

SETTINGS .......................................................................................25

 

4.1

 

Overview ................................................................................25

 

4.1.1

 

Error Logging...............................................................25

 

4.1.2

 

ICAO 24-Bit Aircraft Address (AA)...............................25

 

4.1.3

 

Aircraft Category (AC) .................................................26

 

4.1.4

 

Flight-ID (FID)..............................................................26

 

4.1.5

 

Option Ground-Switch .................................................27

 

4.1.6

 

Reply Information - Speed Category (RI) ....................27

 

4.1.7

 

Serielle Schnittstelle (RS232)......................................28

 

4.2

 

Configuration..........................................................................29

 

4.2.1

 

Setup Steps.................................................................29

 

4.2.2

 

Functions Overview.....................................................32

 

5

 

APPENDIX .......................................................................................34

 

5.1

 

Technical Data .......................................................................34

 

5.2

 

Environmental Conditions ......................................................36

 

 
 

Summary of Contents for 800ATC-(200)-(200)

Page 1: ...TRT800 Mode S Transponder P N 800ATC 200 200 Operation and Installation Document No 03 2102 010 71e ...

Page 2: ...d hint in section 4 2 1 Corrections after internal review 2 02 02 08 2010 Corrections after internal review Added information on connectors List of Service Bulletins SB Service Bulletins have to be inserted into this manual and to be enlisted in the following table SB No Rev Nr Issue Date Insertion Date Name Survey of Variants Part Number Description P N 800ATC 200 200 Version with LCD Display one...

Page 3: ...election 13 2 6 Squawk Setting 13 2 7 VFR Squawk 14 2 8 ID Special Position Identification SPI Squawk Ident 14 2 9 Error Codes 14 3 INSTALLATION 15 3 1 Notes 15 3 2 Telecommunication data 15 3 3 Scope of Delivery 15 3 4 Unpacking and Inspecting of the Equipment 16 3 5 Mounting 16 3 6 Equipment Connections 17 3 6 1 Electrical Connections 17 3 6 2 Static Air Port 18 3 7 Wiring 19 3 7 1 Conductor Cro...

Page 4: ... 24 3 12 2 Mounting Advices 24 4 SETTINGS 25 4 1 Overview 25 4 1 1 Error Logging 25 4 1 2 ICAO 24 Bit Aircraft Address AA 25 4 1 3 Aircraft Category AC 26 4 1 4 Flight ID FID 26 4 1 5 Option Ground Switch 27 4 1 6 Reply Information Speed Category RI 27 4 1 7 Serielle Schnittstelle RS232 28 4 2 Configuration 29 4 2 1 Setup Steps 29 4 2 2 Functions Overview 32 5 APPENDIX 34 5 1 Technical Data 34 5 2...

Page 5: ... Advices whose non observance can cause damage to the device or other parts of the equipment Supplementary information 1 2 Abbreviations Abb Meaning Explanation FID Flight ID Flight plan number or if not assigned registration number of aircraft SPI Special Position Identification Activation on request by controlers Squawk Ident transmits SPI Pulse for 18 seconds which highlights the respective tra...

Page 6: ...andling of return shipments please follow the instructions of the input guide Reshipment RMA provided at the Service Area within the Funkwerk Avionics web portal www funkwerk avionics com Any suggestions for improvement of our manuals are welcome Contact service funkwerk avionics com Informations on softwareupdates are available at Funkwerk Avionics ...

Page 7: ... Radar Interrogations o Mode A replies with a Squawk one of 4096 possible Codes e g flight plan number Squawk assigned by a Controler or the VFR Squawk 7000 o Mode C replies including encoded flight level o Mode S replies including aircraft address and flight level o Extended Squitter containing additional information on position and velocity IDENT capability for activating the Special Position Id...

Page 8: ...2102 010 71e Revision 2 02 2 OPERATION 2 1 Controls ON OFF Squawk Ident activate deactivate VFR Change Active Ù Standby Squawk Select Operation Mode Cursor adjustment Rotary Knob for adjusting values at the cursor position Operation Mode Mode Standby Squawk Active Squawk ...

Page 9: ... standby Squawk 2 works as cursor back button opposite function of the cursor button during entering values and also for navigating backwards through the configuration menu see 4 2 1 IDENT 1 Squawk Ident sends Ident marking SPI for 18 s in normal mode see section 2 8 2 configuration of Flight ID FID in standby mode press button for 5 s MODE Select transponder mode ACS A S or Standby see section 2 ...

Page 10: ...e Device Name Software Version Firmware Version If more than one aircraft address FID exist select the correct entry with the rotary knob and confirm with If there is no external memory TRT800EM connected or no 24bit address defined 000000 the message CRADLE OFF appears and the transponder is not working as Mode S device but as Mode A C transponder The transponder starts in standby mode see sectio...

Page 11: ...RX DC Transmit Failure Low current Internal error FPG FPGA Failure Internal error BAT Battery Power too low maybe battery generator fault IDT transmits Ident Marking SPI ID Squawk Ident has been pressed active for 18 s FL010 FLerr Flight Level Invalid altitude measuring Flight Level in 100 ft steps Beyond 1000 35 000 ft C Mode gets active ACS Opertional Mode STBY A S ACS AC A Modes see section 2 5...

Page 12: ...ntains the 24bit address AA and the aircraft category AC marked by a line above the numbers as well as the Flight ID FID without any line above the numbers cursor digits 1 to 6 ICAO 24 bit Aircraft Address AA HEX format digits 7 to 8 Aircraft Category AC digit 9 to 16 Flight Identification FID This screen will appear for 5s and will be left automatically afterwards 2 4 2 Configure Flight ID Press ...

Page 13: ...nsmitted neither on C nor on S requests All other Mode S data as well as Mode A replies are transmitted If no 24 bit address AA was defined or entered as 000000 the transponder workes as Mode A C transponder in that case the following Modes are possible apart from Standby AC Æ Mode A C Transponder replies only on Mode A and Mode C interrogations A Æ Mode A Transponder replies only on Mode A interr...

Page 14: ...with In order to store the current active Squawk as new VFR Squawk replacing the factory setting 7000 Press and hold until an S is indicated approx 3 s after relasing the button VFR is shown 2 8 ID Special Position Identification SPI Squawk Ident Press ID to activate transmission of the special position identification pulse with every reply within 18 seconds IDT appears on the display By pressing ...

Page 15: ...appropriate manufacturer s instructions 3 2 Telecommunication data Depending on your national telecommunications legislation the following data may be required when applying for the aircraft radio station license Manufacturer Funkwerk Avionics GmbH Type Designation TRT800 EASA Number EASA 21O 045 Transmitter Power Output 71 W Frequency 1090 MHz Emission Designator 12M0M1D 3 3 Scope of Delivery Par...

Page 16: ...om Funkwerk Avionics GmbH Select a position away from heat sources Care for adequate convection cooling Leave sufficient space for the installation of cables and connectors Avoid sharp bends and wiring close to control cables Leave sufficient lead length for inspection or repair of the wiring of the connector containing the memory so that when the mounting hardware for the rear connectors is remov...

Page 17: ...ulse that is sent to the other equipment to suppress transmission of a competing transmitter for the duration of the pulse train transmission The transponder transmission may be suppressed by an external source and vice versa To activate mutual suppression connect the SUPP_I O signal to the according signals of the other equipment 3 6 1 2 Ground Switch If a Ground Switch is connected and activated...

Page 18: ...n connect LIGHT to GND or leave it unconnected Illumination can be varied using an input voltage dimmer or switch from 0 V UB connected to LIGHT 0V for off UB for full brightness inbetween linear 3 6 2 Static Air Port Install a silicon soft tube fitting the 5 mm static air port at the backside of the transponder and secure plumbing with appropriate clamps ...

Page 19: ...Cross Section Power Supply Power GND AWG20 0 62 mm Signals AWG22 0 38 mm The conductors must be approved for aircraft use 3 7 2 TRT800EM External Memory Refer to 3 6 1 3 Background Illumination Ground Switch FLY GND If a ground switch is connected in on ground state pin 15 must be connected to GND otherwise leave Pin 15 open ...

Page 20: ...ocument No 03 2102 010 71e Revision 2 02 3 7 3 TRT800EMSS External Memory with RS232 Ground Switch FLY GND If a ground switch is connected in on ground state pin 15 must be connected to GND otherwise leave Pin 15 open Refer to 3 6 1 3 Background Illumination ...

Page 21: ... be taken into account in such a way that no reduction of the performance of any other system will occur Install only certified antennas 3 8 2 Installation Recommendation Take note of the antenna manufacturer s instructions The usually deployed Dipol or Blade antennas necessarily require a high frequency capable solid metal ground plane at the antenna base For installation in composite aircrafts g...

Page 22: ...be protected against moisture to avoid loss of efficiency 3 9 Post Installation Check All steering and control functions of the aircraft are to be examined in order to exclude disturbances by the wiring The most important factor in the transponder configuration is the setting of the ICAO address see section 4 2 1 Attenuation from antenna to transponder at 1090 MHz must not exceed 1 5 dB A certifie...

Page 23: ...ector TRKABEL2 Antenna cable 2 5 m 8 2 ft TNC Æ BNC RG 142 1 075 dB TRKABEL3 Antenna cable 4 0 m 13 2 ft TNC Æ BNC RG 142 1 72dB TRKABEL4 Antenna cable 6 5 m 21 3 ft TNC Æ BNC RG 142 2 8 dB CI 105 Transponder DME Antenna TSO C66b C74c CI105 Comant Industries Inc Height 3 25 Weight 90 g 0 2 lbs AV22 Bar antenna The TRT800 starts in Standby Mode indicated with STBY In order to change into operationa...

Page 24: ...3 12 Drawings 3 12 1 Dimensions 20mm 15 mm 170 mm TRT800 TRT800H 65 mm 65 mm Ø 57 mm Static Air Antenna Power RS232 3 12 2 Mounting Advices Connections Area 80 mm Panel Cut out 47 0 mm 47 0 mm 57 5 mm 4 x Ø 4 mm Ø Connector plug has to be clamped with both spring locks Fixing clips spring left right ...

Page 25: ... GPS Receiver to support ADS B Out All of these data are configurable in the Setup refer to section 4 2 1 and are stored in the external memory modul integrated within the housing of the D Sub connector included in the delivery The cable with this connector shall remain in the aircraft even if the unit is removed to ensure that the ICAO 24bit aircraft address is fixed to the aircraft 4 1 1 Error L...

Page 26: ... lbs Motor Glider D Kxxx 1A Balloon Airship 22 Aircraft 15 500 lbs 75 000 lbs 1B Paratrooper 27 Rotorcraft Only one of the Codes mentioned in the table above must be used 4 1 4 Flight ID FID Per ICAO regulation Mode S data must contain a valid flight identification FID to ensure that the correlation between flight plan and radar data will work automatically FID setting is required to correspond to...

Page 27: ...nd declared in the configuration the transponder is able to acknowledge on ground and in flight state In on ground state stand by mode is activated With a connected ground switch see section 3 6 1 2 the transponder automatically changes into Standby mode once the gear touched the ground For this the Setup must be configured accordingly For a detailed description of the Setup progress please refer ...

Page 28: ... setting of the GPS receiver not required o NexNav NNL 3101 setting of the GPS receiver not required o KLN94 Bendix King KLN 89B KLN 94 KMD 150 9600 Bd setting of KLN89B KLN94 Standard RS232 Sentence setting of KMD 150 Type 1 Sentence o NMEA Format 4800 Bd setting data format RMC is expected to minimize the amount of data other sub formats are to be avoided Comm A B support 38400 Bd Data format fo...

Page 29: ...Beside the 24bit address and the FID one record stores also the settings made for the serial interface GPS COMM A B and also for the optionally installed Ground Switch A stringently required input is the speed category RI of the respective aircraft see section 4 1 6 Reply Information Speed Category RI All those data are stored in one record If more than one records exist a record can be selected o...

Page 30: ... the ICAO 24 bit address 6 Initially the Cursor is located at the first digit in the lower line The first six digits define the ICAO 24 Bit Aircraft Address In order to enter your 24bit address select the repective letter or number by usage of the rotary knob moves the cursor rightwards moves the cursor leftwards It is important to enter the ICAO 24 Bit Aircraft Address correctly 7 With digits 7 a...

Page 31: ...he rotary knob you can now select yes if a Ground Switch is installed if not select no and proceed with step 11 11 Press at this stage the respective speed category shall be selected by using the rotary knob see section 4 1 6 12 Press at this stage a GPS receiver for ADS B Out can be selected Selectable by rotary knob 13 Press with further Records can now be created and configured as described in ...

Page 32: ... at the corresponding counter value Proceed analog to the steps 1 to 4 described in the table in section 4 2 1 The lower line contains the ICAO 24 Bit Aircraft Address AA the Aircraft Category AC und die Flight ID FID AA and AC are marked by a line above the numbers Digits 1 6 ICAO 24 Bit Aircraft Address HEX Format Digits 7 8 Aircraft Category Digits 9 16 Flight ID FID Counter Function 1 4 Just D...

Page 33: ...Ground Switch Info turn rotary knob to select option Yes No press to enter the next menu item changes are kept in memory but are not yet active press to return to the previous menu item Speed Category with respect to the maximum airspeed of the aircraft enter the corresponding value see 4 1 6 with the rotary knob press to enter the next menu item changes are kept in memory but are not yet active p...

Page 34: ... RTCA DO 160D RTCA DO 178B Software Level D Temperature Ranges Operation 20 C to 55 C für 30 min 70 C Storage 55 C to 85 C Altitude Range 15 000 ft Speed Range 175 kt TAS Shock 6 G Operation 20 G crash safety Environmental Categories RTCA DO 160D Env Cat C1Z CAA SM XXXXXXZBAAA TT M B3F3 XXA Power Supply 10 VDC 16 VDC 0 40 A 13 8 VDC typ 0 70 A 13 8 VDC max 10 W max Fuse External 2A slow blow fuse ...

Page 35: ... 1 5 dB Squitter ADS B transmitted at random intervals uniformly distributed over the range from 0 8 to 1 2 seconds full self verification of data and occurrence Mode S Elementary Surveillance ICAO 24 bit Aircraft Address Hex Code aircraft address as assigned by national aviation authority FID Flight ID Flight Plan call sign or aircraft registration marking Capability Report Reports the available ...

Page 36: ...ng 4 5 4 Z No auxiliary cooling required Altitude 4 6 1 C1 35 000 ft Temperature Variation 5 0 C 2 C change rate minimum per minute Humidity 6 0 A Shock 7 0 A 6 G operational shocks 20 G Crash Safety Test Type R in all 6 directions Vibration 8 0 S Vibration Curve M Explosion Proofness 9 0 X No test required Water Proofness 10 0 X No test required Fluids Susceptibilities 11 0 X No test required San...

Page 37: ... 160D Sectio n Cat Condition Susceptibility Induced Signal Susceptibility 19 0 A Radio Frequency Susceptibility 20 0 TT Emission of RF Energy 21 0 M Lightning Induced Transient Susceptibility 22 0 B3F 3 Lightning Direct Effects 23 0 X No test required Icing 24 0 X No test required Electrostatic Discharge ESD 25 0 A ...

Page 38: ...Funkwerk Avionics GmbH Gewerbestraße 2 D 86875 Waal Germany phone 49 8246 9699 0 fax 49 8246 1049 E mail service funkwerk avionics com www funkwerk avionics com ...

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