ADSE 735 Pitot Static Tester User Manual
Contents
1. 14 9 14 Loto BIECWO PNCUMANG UN t 15 oum MEOS E 15 OO TIU eset 15 el do quss H 16 Lo dd Need T T M 16 Ec NE CUNY c 16 koz OV AN a RN 17 a manc coe advo sie E E d Usu eau DN oru E E v EI eUE M DUE 17 1 8 2 1 1 Management of the serial AK us oido d Yosh ro nd nina 17 ESSA e Sensor WAMAGCINICME T D t TT 17 1 8 2 1 3 Management of the servo controls ss 17 1 822 Management Of SECURES une ian comedi x soie hi entr pote tirer en 18 oo SOFIA ANAN ANA AA AA AA AG 19 2 USING ADSE 739 a AY 21 2 1 Preparing Tor SG AA 21 PANEL zer AA 21 2 12 CCC ACCRO m T 21 2 IG BN PROMO CONIA CT ON M ERE scesasncneeesekiansdieneees 22 2 La PONG UP oc ee Te 27 2 19 Tutning onthe COUDE AA 27 2 2 USNO Ne MENACE een MM 28 2 2 MES C neue ARR ET 28 2222 LE GA AMG NL AAAH AA 29 LEM CIELA ION DOMAIN ee a da ennuis is it ee 30 2 2 2 2 Cr atlonot a MONT domai Mississipi GA eee es 31 2 22 EGU sila GL NT TERT 32 22o COMMONCK E Cr in icio MEE RTT send dd esel seuss 33 A l VI U ue d 34 Z4 a BO Le QI AA AA AA AA TURIS 35 User manual Page3 662. AZp At VZ ft min 1 5 4 Pt dynamic variation Pt channel Unit 150 to 6000 ft min 50 to 1800 m min Range 10 ft or 1 1 3 mor 1 1 Accuracy APt At hPa min 10 to 150 hPa min 2 hPa or t1 1 A Ap At A hPa min 10 to 150 hPa min 2 hPa or t1 1 AVC At kts min 15 to 200 kts min 2 kts or 1 9o 1 AVC At Km h min 30 to 370 km h min 3 7 km h or 1 1 AM At M min 0 05 to 1 M min 0 01M or 1 1 1 on an integration time larger than 3s the greater of these two figures These performances are valid on a volume of 0 to 1 5 liters The ft ft min kts kts min M M min values can be limited by the user through the use of the flight domain function 1 6 Rates of intrinsic leak The intrinsic leak of the ADSE 735 on both channels is less than 0 7 hPa 10 min at 500 hPa without external volume User Manual ED 01 Page 11 66 Pitot Static Tester a ATEQ ADSE 735 1 7 Technical description Capteur Arriv e capteur i vide m Alim entation NO Delta P ligne Vanne L asservie INE Vv Arriv e EV pression delestage Interface vanne utilisateur eTe gt Calculateur Alimentation Figure 2 Block diagram of the ADSE
3. Action Check that the link cable is not damaged and the connectors are properly locked to the RCU and the EPU It the problem persists send the equipment back for repair e Servovalve problem O O Display This message appears immediately following the initialization procedure The pressure information is displayed but the generation is not possible Cause During the self test the initialization of the regulation device does not happen correctly Action Switch off and switch on again the EPU in order to restart the self test If the problem persists send the equipment back for repair e Sensor initialization problem O Display This message appears immediately in an information window following the initialization procedure After validation the software displays the main menu Cause During the self test the initialization of the sensor does not happen correctly Action Switch off and switch on again the EPU in order to restart the self test If the problem persists send the equipment back for repair User Manual Page 58 66 Pitot Static Tester i ATEQ ADSE 735 O e Overpressure on Ps o Display This message appears in Controller Generator mode Ps channel o Cause The pressure in the circuit comes close to the maximum authorized pressure for the sensor This is only possible when the ADSE 735 is connected pneumatically to an external pressure source o Action Switch off the ADSE
4. User Manual Page 42 66 Pitot Static Tester A TEG ADSE 735 2 2 4 Automatic program mode The program mode allows the user to create visualize edit and start an automatic test program Figure 27 Automatic Program menu User Manual Page 43 66 JATEQ OMLCTON 2 2 4 1 Writing a new program File name File name Files existing Figure 28 Entering a program name Figure 29 Control of coherence Manual Leak Level 00 min sec Program name prog Save Del Menu Save Del Menu Figure 31 Example program step nr 2 Figure 32 Example program step nr 3 User Manual Pitot Static Tester ADSE 735 Program Ground Back to the ground stepne i onf lt gt Ground l Measure Level min sec Program name Cini IF DAN Evnmmnlan FINI MAN atan nr A Ps ram Leak test Time 30 mn SEC step n 4 lon 4 lt gt Ground l Measure Manual Leak Level min sec rog Program name p Del Figure 33 Example program step nr 4 Sa Menu Page 44 66 Pitot Static Tester ADSE 735 ATEQ OMLCTONn Steps for writing a flight program a Choose the type of program Ps or Pt a Enter a file name by clicking on the associated field in order to access to the alphanumerical keyboard The list of existing files is given for information A consistency check is performed upon validation o Tfthe field is e
5. micron ADSE 735 Non RV AvionTEq ATE pecececensd Pitot Static Tester ATEQ i ADSE 735 www avionteg com OMLCTON ATE omucron ADSE 735 Pitot Static Tester User Manual Author F PLATEL SE Approved by E DUTITRE ath User manual Page 1 66 Pitot Static Test ATEQ drin omicron Revisions Date Edition Reference Creation November 2005 01 D2 0105 CL A Update trouble August 2006 02 D2 0105 CL B shooting guide Change pics October 2006 03 D2 0105 CL C Starting procedure Change pics March 2007 04 D2 0105 CL D Update Option November 2007 05 D2 0105 CL E Update screen March 2008 06 D2 0105 CL F User manual Page2 66 Pitot Static Test ATEQ ee ADSE 735 Omicron L PRESENTATION nas aa 6 ECC e 6 pole 7 UE Os g Fg os 9 CS AA AA nn ee eee re 8 1 4 Equipment Reference a AA AA AA 8 1 0 Pressure le Kana AA AA 9 1 6 Main units measurement range and accuracy of the generator between 0 C and TAO CA ALAN AA 9 LO Stauc pressure PS pa ENNA DTE 9 1 6 2 Total and differential pressure Pt AP 10 oO Po ayna mie VaN O RERO ET PT 11 POE deir VU AMON T 11 1 7 Rates of la ka la Ei Led 2 LA AA AA AA AA AA 11 1 8 TECANICalkdESENPUONia EEE RER 12 LS NAN DON ahm ANAN m UU T 13 iD oe Ba We AA AA ener eee ee 13 EOT CONVOI arra a c
6. Qftan nr A Ras ta arniind User Manual Page 49 66 Pitot Static Tester i ATEQ ADSE 735 Operating Mode Select an automatic program in the list of existing programs and Validate A window appears explaining the pneumatic connections to be realized depending on the type of program and the configuration of the aircraft Validate by clicking OK Wait during the initialization procedure of the ADSE 735 The step nr 0 x is displayed with the name of the selected program Click on Exec to start the program The step nr 1 is displayed and executed In the example above the step nr 1 corresponds to the generation of 1000 ft at 3000 ft min The ADSE 735 performs a balancing phase executes the pressure instructions then stays at level during the time indicated in the field Level min s Once the level time is over the step nr 2 is displayed and executed In our example the ADSE 735 switches to reader mode during a time corresponding to the level time entered Once the level time is over the step nr 3 is displayed and executed In our example the ADSE 735 switches to the leak test mode In this case the level time happens at the beginning of the step allowing for a stabilization of the pressure in the circuit The leak test starts the Time field is counted down until 00 00 and the result of the leak test is displayed in the unit requested when the program was written In
7. Range limits name Min Max Rate fe 2300 15000 6000 es Lee me Figure 9 Writing a flight domain Figure 10 Alphanumerical Keyboard Upon creation of a flight domain the value fields are pre programmed with the maximum values acceptable by the ADSE 735 The user must a enter a domain name by clicking on the associated field which gives access to an alphanumerical keyboard Erreur Source du renvoi introuvable a modify the values by using the digital keyboard Erreur Source du renvoi introuvable which appears by clicking on the associated field Once all parameters are entered press Save to validate and record the data or press Cancel to abandon the flight domain creation and come back to the Range limits main menu User Manual Page 31 66 Pitot Static Test ATEQ ur co OMLCTON 2 2 2 3 Editing a flight domain Range limits list min Range limits name Min Max Rate s kts vacare m Cancel Save Figure 12 Selecting a file Editing a flight domain happens through a window presenting all existing flight domains except max a Cancel to come back to the Range limits main menu a Validate to edit the selected flight domain a All parameters of this flight domain appear the user can modify the values by using the digital keyboard which appears by clicking on the associated field After entering the data press a Cancel to come b
8. S S S N v O e D Q QU o Q e S TU J qeu ES JOE 7 LO SE LE S8E FE D 2 o C O O NG O 5 On NUN NUN N N amp amp 4 Calibration Calibration Changement des filtres de ventilation Fan filters exchange Changement filtres internes Internal filters exchange V rif ication alimentation interne Internal voltage check V rification pneumatique interne Internal pneumatic check Changement des pi ces en caoutchouc Rubber part exchange Test des lectrov annes Electrov alv es test Test cartes lectroniques Electronic board test Test connecteurs pneumatiques Pneumatic plug test Test connecteurs lectriques Electric plug test R glage vanne modulante Regulation valve adjustment X X XX x xxx Remplacement dalle tactile Touch screen exchange R nov ation des lectrov annes Electrov alv es renov ation Remplacement connecteurs pneumatiques Pneumatic plug exchange Test groupe de pompage Pump group test Changement ventilateurs Fan exchange X UK KA Test des batteries Battery test Changement des batteries Battery pack exchange B R nov ation des lectrovannes 3Ps 3Pt Electrovalves renovation 3Ps 3Pt EU OU X UK X AK KKK KKK KK X M Notes X pour tous les ADSE for all ADSE equipment B pour les ADSE avec option pack batterie for ADSE with battery pack option o
9. with only occasionnal use in very harsh environment In the case of a permanent use in harsh conditions equipment embarked permanently on an aircraft carrier on an airbase in the desert we recommend to divide by two the time between two maintenances 3 3 2 External 3 3 2 1 Housing Clean every month with soft sponge water and mild liquid detergent 3 3 2 2 Front panels and touch screen Clean every week with damp lint free cloth and mild liquid detergent NEVER USE AGRESSIVE DETERGENT OR SOLVENT 3 4 Associated equipment The ADSE 735 is compatible with the Pitot and Static adaptors available on the market Usually the aircraft manufacturer can provide the necessary adaptors The sales department of ATEQ OMICRON is at your disposal to help you source the adaptors corresponding to your needs User Manual Page 63 66 JATEA OMLCTON 3 5 Contacts 3 5 1 Mailing address ATEQ OMICRON 8 route de Chevreuse 78117 Chateaufort France 3 5 2 Telephone numbers Switchboard Telefax Sales Technical department After sales service 01 39 07 50 00 01 39 07 50 19 01 39 07 50 02 01 39 07 50 07 01 39 07 50 05 User Manual Pitot Static Tester ADSE 735 Page 64 66 JATEA OMLCTONn Pitot Static Tester ADSE 735 3 6 Maintenance list for ADSE equipment S OD 8 WA A Q O N Z OSs S So pA O C x o L F L NG oc S d Y o DT D N e O A Y Pa a O 0 5S D FL E
10. 735 and the external pressure source Wait a few minutes until the pressure in the ADSE 735 has come back to the ambient pressure Restart the ADSE 735 The pressure indicated should be equal to the ambient pressure After such an incident it is recommended to check the pressure information with a pressure standard in order to verify that the sensor has not been damaged e Overpressure on Pt o Display This message appears in Controller Generator mode Pt channel o Cause he pressure in the circuit comes close to the maximum authorized pressure for the sensor This is only possible when the ADSE 735 is connected pneumatically to an external pressure source o Action Switch off the ADSE 735 and the external pressure source Wait a few minutes until the pressure in the ADSE 735 has come back to the ambient pressure Restart the ADSE 735 The pressure indicated should be equal to the ambient pressure After such an incident it is recommended to check the pressure information with a pressure standard in order to verify that the sensor has not been damaged e Limits exceeded o Display This message appears in Controller Generator mode Ps channel or Pt channel o Cause The ADSE 735 cannot reach the requested pressure value due to a too important leak of the pneumatic circuit o Action Check the pneumatic circuit of the aircraft or of the connected instrument If the leak comes from the ADSE 735 send
11. Pitot Static Test ATEQ m E Omicron CLASS UN ONANGO a E A ee de ot 37 22 32 2 Generation ne AA 37 2 2 3 2 3 Execution of the flight instruction 38 MUEVE Leak PO a a AA ali den 39 2 2 3 2 5 Return to the ground aa 40 2 2 3 2 6 Exiting the Controller Generator mode Us 40 2 2 3 2 7 Visualizing the flight domain sise 41 2 2 3 3 Pt Generation mam NA OE nne 42 2 2 4 Automatic program mode acsi rana sa aa NAA AG Wassuectesenase 43 2 2 4 1 Writing a new program 11 11111 111 44 2 2 4 2 Visualizing and editing a program ss sssieesieesrreesereeesereeereennnns 47 2 2 4 3 Executing a program with the user interface nne 48 2 2 5 Calibration MO era 52 2 2 5 1 Calibrating the sensor iisiiiieseeneesreereeseeeennesnns 52 2 2 5 2 Use of the Interface ioci rrr a GG aNG AA AG 53 2 2 6 General Information 1 111 NA 55 2 2 6 1 Changing a password sssiiesseeesrreeeesereeeeseeeeenennnse 56 2 2 1 Exiting the software Lama ious on ana Gad T seen 57 Si AFF ENDIK ETE et te Ua nt 58 21 Error 3 Lo AA PAPA AP PAP PAA 58 3 2 Trouble SNOOUN DARAAN aki 60 3 2 1 Problem with the Electro Pneumatic Unit ccececcecseeeeeeeeeeseeeeeseeesseueeseueesaaeeesaeeeseeeeesees 60 3 2 2 Problem with the Remote Control Unit ss 61 3 2 2 1 Message 4 Battery Low and total discharge of the RCU battery 61 322 RODEO amahan
12. aman eo en han na 61 3 5 MAMAN AA AA AA AA aa AA AA 63 ca ul TI MERTK 63 3 9 2 PI MERERETUR 63 Sid Mix eU NO ER T cM 63 3 3 2 2 Front panels and touch screen nennen nennen nennen nnne nns 63 3 4 ASSOCIated je 63 3o Gro i ACCS PT E 64 SREE EE ACG SINT 64 3 9 2 WENO ICIS MOSS de 64 3 6 Maintenance list for ADSE equipment aa 65 User manual Page4 66 Pitot Static Tester ADSE 735 JATEA OMLCTON Introduction e The objective of this user manual is to describe and provide to the users the information necessary for the use of the ADSE 735 PITOT STATIC TESTER e The producer has conceived this equipment to function in full security within the normal use described in the manual e The users of this equipment should have the necessary technical knowledge in order to understand and follow the procedures described in this manual Figure 1 ADSE 735 User manual Page 5 66 Pitot Static Tester a ATEQ ADSE 735 1 PRESENTATION 1 1 General The ADSE 735 Pitot Static Tester allows controlling and calibrating air data equipment altimeter airspeed indicator rate of climb indicator and air data computer It consists of an electro pneumatic unit including the computer the measurement and regulation components the security systems and the user interface The user interface is an RCU based on a PDA technology The interface
13. and Pt channels a Range limits Visualize the flight domain currently selected At the start the screen Connection status Erreur Source du renvoi introuvable appears for a few seconds when the RCU and the EPU establish the connection If the dialog does not happen properly the message Connection problem y appears after one minute Check the connection between the RCU and the EPU If the dialog happens properly the main screen appears giving access to the different functions The user can then a Change the visualization and generation unit through the scrolling menu a Enter the target pressure values a Launch a pressure generation a Switch to a leak test a Go back to the ground a Stop a pressure generation a Visualize the flight domain currently selected User Manual Page 36 66 Pitot Static Tester a ATEQ ADSE 735 2 2 3 2 1 Unit change Changing a unit happens by the selection of the desired unit in the scrolling menu The change is effective once the actual displayed units are refreshed The values of the pressure are then displayed in the desired unit Caution A unit change does not update the target values 2 2 3 2 2 Generation To generate a pressure select the desired unit and enter the altitude and rate of climb values For this select the desired value by clicking on the associated field A digital keyboard appears enter the desired value and validate by pressing Enter Repeat this f
14. exit the application User Manual Page 28 66 Pitot Static Tester A TEG ADSE 735 Q The password to access the calibration mode 2 2 2 Flight range limits Figure 6 Flight Domain or Range Limits Menu The Range limits menu allows to a Select an existing flight domain a Create a new flight domain o Edit an existing flight domain User Manual Page 29 66 Pitot Static Test ATEQ ur ro omuicron 2 2 2 1 Select a flight domain Range limits list Range limits name Min Max Rate ft kts Cancel validat Default Figure 7 Selecting a file Figure 8 Visualizing a file The selection of a flight domain happens through a window presenting all existing flight domains a Cancel allows coming back to the Range limits main menu a Validate allows visualizing the selected flight domain All parameters of this flight domain appear the user can choose between a Cancel to return to the list of flight domains a Validate to select this flight domain immediately but this selection will be lost at the next start of the software a Default to select this flight domain immediately and keep it as domain by default at the start of the system Note 1 The flight domain called max is a reserved flight domain and can neither be modified nor deleted User Manual Page 30 66 Pitot Static Tester ADSE 735 JATEA OMLCTON 2 2 2 2 Creation of a flight domain
15. in the Pitot circuit The Ps channel Black Connector of the ADSE 735 has to be disconnected User Manual Page 24 66 Pitot Static Tester ATEQ ADSE 735 Configuration nr 2 The static circuit of the aircraft IS pneumatically connected only to the altimeter and to the climb rate indicator Ps Pt Altimeter Rate of climb Air speed For altitude simulation i e testing the altimeter and or the climb rate indicator only the Ps outlet Black connector of the ADSE 735 needs to be pneumatically connected to the static circuit of the aircraft User Manual Page 25 66 Pitot Static Tester a ATEQ ADSE 735 e For speed simulation i e testing the speed indicator only the Pt outlet Red connector of the ADSE 735 needs to be connected to the Pitot circuit of the aircraft in order not to generate any overpressure in the Pitot circuit The Ps channel Black Connector of the ADSE 735 has to be disconnected User Manual Page 26 66 Pitot Static Tester a ATEQ ADSE 735 2 1 4 Powering up To turn on the bench simply press the green button situated on the front panel of the case After the equipment has been switched on the computer runs a self check To use the RCU press the POWER button see Erreur Source du renvoi introuvable The RCU turns on and stays in the same configuration as it was at the end of the previous use When the equipment is shipped from the factory the software is already confi
16. order to allow the user to note the result of the leak test the ADSE 735 switches to the standby mode The user has to click on Exec to go to the next step The step nr 4 corresponds in our example to the return to the ground User Manual Page 50 66 Pitot Static Tester ADSE 735 JATEA OMLCTON Note 1 At any time the user can switch to the standby mode by clicking on Pause If the generator is counting down a level time the Pause instruction will be taken into account at the end of the countdown To come back to the execution of the program click on Exec Note 2 At the end of a program the user can exit the program by clicking on 4 Menu or re launch the program by clicking on 4 Exec Note 3 At any time the currently selected flight domain can be visualized by clicking on Lim Note 4 The example shown in this manual is an automatic program for the static channel A program for the Pitot channel can be performed under the same conditions User Manual Page 51 66 Pitot Static Tester 7 ATEQ ADSE 735 2 2 5 Calibration mode The calibration mode is accessible through a password The calibration technician enters n couples of values n lt 40 regularly distributed along the range of use of the sensor 27 to 1500 mb The generator recalculates the curve of the sensor segment by segment by offsetting the gaps on each interval 2 2 5 1 Calibrating the sensor In orde
17. pp She Se pt ht She She ie F Press Ok to continue Exit Figure 15 Test of the static circuit Finiira 1R Tact nf tha Pitat rirriiit After selection of the Ps or Pt channel a message appears indicating to the user which pneumatic link has to be performed to avoid damaging the instruments as specified at paragraph 2 1 3 User Manual Page 34 66 Pitot Static Tester A TEG ADSE 735 2 2 3 2 Ps generation Actual unit Connection state Initialization Launch a pressure generation Pssetpoints Execute d Access to Leak test Leak Ground Menu j i STOP Figure 18 Waiting for the connection Visualize the flight domain at 689 ft mi a 1000 P RENE X Rate 45 oT 2 Ps set points Execute Pssetpoints TU Ps set points Pssetpoint NES points Execute Alt CS at 11000 at 11000 Rate 500 ft mi a j leak Ground LUE Leak Ground Menu TEES ee Figure 20 Balancing Mode Back to main menu User Manual Page 35 66 Pitot Static Tester a ATEQ ADSE 735 Ps set points Execute at ka Leak Ground Menu Domain STOP Figure 22 Tester at ambient pressure The manual mode of the Pitot Static Tester includes three functional modes a Measure Generate Check the status of the generator on the Ps and Pt channels and generate on these channels a Leak test Perform a leak test on the Ps
18. 735 User Manual ED 01 Page 12 66 JATEA OMLCTON 1 7 1 Main box Pitot Static Tester ADSE 735 The housing box contains the metrology the servo controls the user interface management the power supply the vacuum and pressure generation the cables and the remote control unit 1 7 1 1 Front panel On the front panel are to be found 1 Ps pneumatic connector static pressure 1 Pt pneumatic connector total pressure 1 green switch ON OFF 1 power supply connector AC DC 1 connector for RCU connection aspace reserved for the RCU OMtEr on E ADSE 735 Ps Pitot Static Tester pt User Manual Page 13 66 Pitot Static Tester ATEQ ADSE 735 1 7 1 2 Cover The cover includes a bag in which the electric cables and pneumatic hoses can easily be stored User Manual Page 14 66 Pitot Static Tester a ATEQ ADSE 735 1 7 1 3 Electro pneumatic unit The metrological part consists of the pressure sensor several electro valves the servo loop gate the power supply and the computer 1 7 1 3 1 Sensor The pressure sensor derives from the last technical evolutions allowing for cost reductions bound with production rationalization In addition this extremely compact sensor can easily resist mechanical shocks and overpressures The sensor of the ADSE 735 is guaranteed standardwise for use between 10 C and 40 C with an accuracy of 0 01 of the full scale a
19. EQ ADSE 735 2 1 3 Pneumatic connection CAUTION The ADSE 735 is a single channel test device i e it can simulate either altitude or ground speed but it cannot generate simultaneously on the Static and Pitot circuits As a consequence some precautions are to be taken with the pneumatic connections Before using the ADSE 735 please open fully the manual valve on the front panel by unscrewing it then screw it fully This will make sure that no remaining pressure or vacuum is trapped in the pneumatic circuits of the ADSE 735 due to variations of temperature or others causes of pressure variations User Manual Page 22 66 ATEQ Pitot T Configuration nr 1 he static circuit of the aircraft is pneumatically linked to the speed indicator Ps Pt Altimeter Rate of climp Air speed e For altitude simulation i e testing the altimeter and or the climb rate indicator the Ps outlet Black connector of the ADSE 735 needs to be pneumatically connected to the static circuit of the aircraft and the Pt outlet Red connector of the ADSE 735 to the Pitot circuit of the aircraft So the speed indicator remains at zero speed value during the altitude test User Manual Page 23 66 Pitot Static Tester a ATEQ ADSE 735 e For speed simulation i e testing the speed indicator only the Pt outlet Red connector of the ADSE 735 needs to be connected to the Pitot circuit of the aircraft in order not to generate any overpressure
20. ack to the Range limits main menu a Save y to record the selected flight domain Note If the name of the flight domain is modified a new domain file is created User Manual Page 32 66 Pitot Static Tester ATEQ ADSE 735 ATEQ 2 2 3 Controller Generator Pt channel OFE Delta Altitude ft Figure 14 Controller Generator Menu This mode allows generating pressure and vacuum in order to simulate altitude and speed This first window allows choosing the type of generation desired Ps or Pt and to enter the correction parameters for the Ps channel a Correction of Qfe Choice between 1013 25 hPa and atmospheric local pressure a Correction of altitude gap Parameter in feet equal to the difference between the pressure at the level of the test set Ps outlet and the altimeter situated in the aircraft User Manual Page 33 66 Pitot Static Tester JA TEG ADSE 735 2 2 3 1 Pneumatic link CEE LES WARNING CEE LES ok sie Sk se oc oie WARNING oe sie Se oe or oe Speed test Pt Do not plug the Ps circuit of the ADSE735 to the Altitude test Ps If the anemometer is connected to the static circuit of the plane so Connect the Ps and Pt channels on the static and pitot circuits of the plane static circuit of the plane Press Ok to continue Otherwise Connect only the Ps channel of the ADSE735 to the static of the plane See Sie pe Spe Spe che Spe ps Spc che oe
21. allows visualizing and entering the parameters of the Ps or Pt channels unit target value ramp actual value flight programs flight domains The ergonomics of the ADSE 735 is characterized by an excellent reading of the information by an easy management of the configuration parameters Interactive Menus indication of the errors of manipulation Remote Control Unit Personal Data Assistant User Manual ED 01 Page 6 66 Pitot Static Tester a ATEQ ADSE 735 1 2 Applications The ADSE 735 Pitot Static Tester has been especially conceived to simplify the test of air data equipment in aircraft altimeters rate of climb indicators airspeed indicators and air data computers Its internal computer manages the security systems the measurement and regulation components from a user interface which ensures following functions e In MEASUREMENT or GENERATION mode on the Ps or Pt channel gt Measurement or generation of static pressures altitude or ground pressure gt Measurement or generation of total or differential pressures ground speed or pressure gt Timed Measurements of leak rates e In PROGRAMMING mode on the Ps or Pt channel gt Writing of automatic test programs gt Execution of the written programs e Security gt Permanent control of all the parameters of the FLIGHT DOMAIN gt In case of interruption of the facilities like a power supply interruption the pressu
22. andard and a digital keyboard access button The calibration procedure consists of a Generating pressures with a standard controller connected on one of the Ps or Pt pneumatic connectors User Manual Page 53 66 Pitot Static Tester ADSE 735 ATEQ OMLCTONn a Reading the value of the pressure standard and entering it in the Standard field with the digital keyboard which appears by clicking on a Validating the value entered a Validating the calibration once all points pressure values have been entered by clicking on 4 Validate calibration When the calibration is validated o The data are saved in a backup file o The data are sent to the computer which takes into account these new parameters NOTE The user can enter up to 40 pressure values on the whole scale These data must be entered starting from the minimum pressure upwards to the maximal pressure When the data have been successfully transferred to the computer a message Calibration OK appears in the information window If the transfer did not happen properly a message Calibration KO appears The data need to be loaded again Click on the button Load data All data relating to the last calibration and the calibration date appear To validate the data transfer click on 4 Validate y otherwise click on 4 Cancel Erreur Source du renvoi introuvable The data transfer procedure resumes Note 1 If a calibration validation is r
23. back to the ground using the hPa as measurement unit and a climb rate equal to 100 hPa min User Manual Page 45 66 Pitot Static Tester ADSE 735 ATEQ OMLCTON L Generator Mode In this mode the altitude or speed value the climb or acceleration rate and the measurement unit used for the generation need to be entered Once the generation level has been reached the level time entered by the user is counted down before the program goes to the next step Erreur Source du renvoi introuvable LJ Measure Mode The ADSE 735 switches to the pressure measure mode and stops regulating the pressure In this mode the measurement unit can be chosen in which the information shall be displayed as well as the level time before the program goes to the next step Erreur Source du renvoi introuvable Q Leak Test Mode In this mode the ADSE 735 switches into measure mode waits until the pressure stabilizes in the circuit during a time corresponding to the level entered by the user then starts the leak test entered in the Time field and in the entered measurement unit Once the time has been counted down the user is requested to validate so that the program continues to the next step Erreur Source du renvoi introuvable User Manual Page 46 66 Pitot Static Tester ADSE 735 JATEA OMLCTON QI 2 2 4 2 Visualizing and editing a program ae Figure 34 Selecting a program a Select the des
24. cation file a Domain In this directory are recorded all flight domains with a dom extension a Programme In this directory are recorded the prg files which contain the automatic flight program scripts a Parameter In this directory are recorded the files necessary to run the application User Manual Page 20 66 Pitot Static Tester a ATEQ ADSE 735 2 Using the ADSE 735 2 1 Preparing for use 2 1 1 Installation Upon receipt of the equipment please verify the content of the delivery The standard version includes a case containing a 1 RCU Remote Control Unit a Abm long red hose with a STAUBLI pneumatic connector with a red marking a Abm long light brown hose with a STAUBLI pneumatic connector with a black marking a 1 AC power cable a 1 cable for connecting the RCU and the EPU The equipment in option is listed on the enclosed shipping bill 2 1 2 Electrical connection Connect the AC cable between the POWER connector of the ADSE 735 and the 110 240 VAC 50 60 Hz electrical network a For the DC option connect the DC cable between the POWER connector of the ADSE 735 and the DC power supply between 12 and 32V a Connect the Remote Control cable to the RCU and to the RCU connector of the case EPU CAUTION Always check that the cable references and the AC and DC voltages are correct according to the user manual User Manual Page 21 66 Pitot Static Tester a AT
25. equested but less than two calibration points have been validated a control prohibits this validation and an information window is displayed Erreur Source du renvoi introuvable User Manual Page 54 66 Pitot Static Tester A TEG ADSE 735 2 2 6 General Information By clicking on the OMICRON button of the main menu following information is displayed OrLcr ON ADSEZ35 Version 2 0 8 route de chevreuse 78117 Chateaufort FRANCE Phone 331 39 07 50 00 Fax 531 390 0 19 Figure 49 General Information a Cancel brings back to the main menu a Parameters gives access to the modification of o the password requested to exit the remote control unit software access to the underlying operating system o the password to access the calibration mode User Manual Page 55 66 Pitot Static Tester JATEQ ADSE 735 OMLCTONn 2 2 6 1 Changing a password Select password oat E a To exit Select password To calibrate Current password ok fd Cang Core passer Cancel Figure 50 Choosing the password to change Fiaure 51 Fntarina the current New password Save your new password The passwords are Confirm password differents p Cancel Figure 53 Entering the new Cancel password Einrirn BA Cnharanna nmnmntenl varith User Manual Page 56 66 2 2 7 ATEQ OMLCTONn Pitot Static Tester ADSE 735 Select the functio
26. fter pressure temperature electronic correction 1 7 1 3 2 Servo valve The servo valve is designed to regulate the pressure generated by the ADSE 735 This is a dual pressure regulator One regulator is used for regulating vacuum intake the other one is used for regulating pressure intake The orders are transmitted via a lever acting on small valves A motor drives this lever servoed in position and controlled by the computer depending on the difference between the pressure command and the actual pressure in the pneumatic system This servo valve is made of aluminum The sealing parts are made of silicon rubber Adjustment is identical for all valves which can be replaced without a need for adjustment User Manual Page 15 66 Pitot Static Tester a ATEQ ADSE 735 1 7 1 3 3 Power supply Power supply is AC 110 240VAC 50 60 Hz 110 240 VAC 50 to 400 Hz and DC 12 32V in option 1 7 1 3 4 Computer The computer is made of a set of electronic boards connected together by PC 104 bus Q 1 PC board format little board LJ 1 board managing the modulating valve the electro valves and the pressure sensor This set of boards constitutes a system comparable to an IBM PC type computer 1 7 1 3 5 Security The ADSE 735 includes many electronic and physical securities Q In case of an accidental power supply interruption of the system the main electro valve is not supplied with power any more The system returns automatically to a
27. gured and is accessible from the main menu 2 1 5 Turning off the equipment Before switching off the general power supply of the bench LJ Come back to the main menu Q Turn off the RCU by pressing the POWER button see Erreur Source du renvoi introuvable Q Turn of the main unit by pressing the green ON OFF button situated on the front panel of the case LJ Disconnect the power supply User Manual Page 27 66 Pitot Static Tester A TEG ADSE 735 2 2 Using the interface This part presents the different menus and screens of the user interface 2 2 1 Starting the software When the software starts two screens appear successively The first one allows for the initialization of the application and the second one is the main menu omicron Range limits Measure Manual OoOrmtcrom Calibration mode Exit This menu gives access to the different functions of the equipment Range limits Select create or edit a flight domain Measure Manual Access to the manual Ps and Pt generation functions Program Create edit visualize and execute a flight program on the Ps or Pt channel Calibration mode Calibrate the pressure sensor Exit Exit the application Figure 4 Initialization Path Screen E Main M and access to Wihtys Main Menu The OMICFON field gives access to general information on the company and the software There you can change LI The password to
28. ired program a The screens displayed are identical to the screens of the creation mode The user can then edit the program delete or modify existing steps or add new steps a To save the modifications click on 4 Save a To quit without saving click on 4 Menu User Manual Page47 66 Pitot Static Tester ADSE 735 2 2 4 3 Executing a program with the user interface Program name Program name Step N Level min s Step N Level min s o 4 loo foo o l4 loo loo peu Connection state Alt a eee sebo lm Fiqure 37 Selecting a program Figure 35 Waiting for the connection Figure 36 Waiting for the program start Program name Program name prog program name Step N Level min s Level min s Step N Level min s aj oo o5 race 00 05 Eye ool Ps values Lea Ps values BL E we D min cs a mm Ps set points Ps set points Ps set points 4 2 a a4 Lol wo 8000 pa me pooo paj ao EO Domain Menu Pause Domain Menu Pause Domain Menu Pause Figure 38 Step nr 1 Generator Mode Figure 39 Step nr 1 Generator Mode Figure 40 Step nr 1 Generator Mode Balancing phase Running phase NG Level phase User Manual Page 48 66 Pitot Static Tester jare A Figure 41 Step nr 2 Reader Mode Level phase Fimura AR Stan nr 2 Darfnrminn a Figure 44 Step nr 4 Back to ground mS Balancing phase Finiira Ak
29. it back for repair Note To check the leak of the ADSE 735 disconnect it pneumatically from any instrument and start a pressure generation to 500 hPa at 150 hPa min Perform a leak test during 15 minutes The ADSE 735 should not leak by more than 1 hPa User Manual Page 59 66 Pitot Static Tester ADSE 735 JATEG OTi LcT on e Problem with the connection Timeout RS232 Emergency stop o Display This message appears in all modes where the RCU dialogs with the EPU The RCU automatically turns back to the main menu o Cause The serial link between the RCU and the EPU does not work o Action Check the cable for a potential damage Check that the light of green ON OFF button is on Switch off and on the ADSE 735 and try to re establish the link If the problem persists send the ADSE 735 back for repair 3 2 Trouble shooting 3 2 1 Problem with the Electro Pneumatic Unit If during the use of the equipment a power supply breakdown happens or if the ADSE 735 is blocked electronic breakdown power supply problem turn off the system with the green ON OFF button situated on the front panel of the EPU The ADSE 735 then automatically returns to the ambient pressure through a calibrated leak allowing for a return to the atmospheric pressure in all safety for the connected instruments As the RCU has batteries it will continue to work If a dialog was established between the EPU and the RCU it will detect a link problem a
30. mbient pressure by more than 5 hPa the ADSE 735 switches to the generator mode and comes back to the atmospheric pressure in the selected unit using the last selected climb rate The message Ground is displayed at the bottom of the screen Once the pressure is back to the external pressure the ADSE 735 switches to the Measure mode and opens the electro valve to the ambient pressure The message Atmosphere appears in the field Ps status The instrument in test can be disconnected without risk 2 2 3 2 6 Exiting the Controller Generator mode To exit this mode the pressure inside the equipment has to be brought back to the atmospheric pressure first click on Ground Once the atmospheric pressure has been reached click on Menu User Manual Page 40 66 Pitot Static Tester ADSE 735 ATEG mm OMLCT ON 2 2 3 2 7 Visualizing the flight domain Range limits Min Max Rate ft kts M Back STOP Figure 25 Visualizing the selected flight domain At any time the user can click on Domain and visualize the selected flight domain To return to the main screen click on Back User Manual Page 41 66 Pitot Static Tester 7 ATEQ ADSE 735 2 2 3 3 Pt Generation s E eset ponts MEE Figure 26 Pt channel generation The operation of the Pt channel is identical to the Ps channel only the units are different and correspond to the speed units
31. mpty the application returns to the main menu o If the program name already exists a dialog box is displayed indicating the problem After validation the user is requested to enter a new name a Write a program with a maximum of 20 steps a To save the data click on 4 Save a To delete a current program step click on Del a Tocancel the creation of the program click on 4 Menu The data entry screen of the program displays permanently the program name the selected function mode the current step number the total number of steps the choices of function modes and a level time 5 s by default which is also the minimum authorized value Writing a program consists for each step of defining the function mode LJ Ground The ADSE 735 automatically comes back to the ground using the last measurement unit and the last rate of climb validated and then opens the electro valve putting the circuit at atmospheric pressure If the generator is already at atmospheric pressure 5 hPa only the electro valve opening to the atmospheric pressure is activated Once the ADSE 735 has reached the atmospheric pressure the level time entered by the user is counted down before program goes to the next step Erreur Source du renvoi introuvable Note 1 In the case of a request to return to ground when no generation has been performed before but the generator is at a pressure different from the atmospheric pressure the equipment comes
32. n for which the password will be changed Enter the current password for this function when the equipment is delivered the password is the serial number of the equipment If the password entered is wrong a message appears 4 Incorrect password If the password is correct a window appears where the user is requested to enter twice the new password and validate If both passwords are different an error message is displayed If the passwords are identical a window appears requesting to validate the change If the user clicks on 4 Cancel without validating the change is not taken into account Exiting the software To exit the software and access the Pocket PC Windows environment click on 4 Exit and enter the password to exit the remote control software When the equipment is delivered the first time the password is the serial number of the equipment User Manual Page 57 66 JATEG OTi LcT on Pitot Static Tester ADSE 735 3 APPENDIX 3 1 Error messages During the self test and the normal use the ADSE 735 checks different parameters and gives information in case of malfunctions or events potentially generating damage to the ADSE 735 or to the flight instrument currently checked e Error Not connected O Display This message appears after one minute following a connection procedure between the RCU and the EPU Cause The serial link between the RCU and the EPU is not working
33. nd a message will appear in a window forcing a return to the main menu Turn off the RCU Check the power supply of the ADSE 735 and switch it on If the problem persists send the equipment back for repair User Manual Page 60 66 Pitot Static Tester ATEQ ADSE 735 3 2 2 Problem with the Remote Control Unit 3 2 2 1 Message Battery Low and total discharge of the RCU battery If this message appears it can be due to three reasons e The RCU is working autonomously i e the Electro Pneumatic Unit is not working ON OFF light turned off Turn on the EPU to charge the battery block of the RCU e At the start of the ADSE 735 after an interruption of some days in the use of the bench The battery pack of the RCU will recharge during use e During the use of the ADSE 735 with the EPU switched on The battery pack does not charge any more Send the ADSE 735 back for repair If the bench has not been used for weeks the battery of the RCU may be totally discharged The RCU will not start when you press the ON OFF button Connect the cable to the RCU and to the bench and allow for the battery to charge for a few minutes Press the ON OFF button again The RCU will display the screen shown on page 63 Follow the procedure shown page 63 3 2 2 2 RCU blocked In case of a major problem with the RCU follow the first procedure and in case of failure the second procedure e Press the Power button of the RCU for a few second
34. nly M pour les ADSE avec option multi v oies for ADSE with multiple outlet option only P pour ADSE avec pompes internes for ADSE with internal pumps only T pour ADSE avec crans tactiles for ADSE with touch screen User Manual Page 65 66
35. or the Rate of Climb field If one of the set values is outside the flight domain currently selected a message appears in the bottom window and the entered value is automatically replaced by the minimum or maximum authorized value User Manual Page 37 66 Pitot Static Tester a ATEQ ADSE 735 2 2 3 2 3 Execution of the flight instruction In order to execute the instruction click on 4 Execute The information entered in the set value fields are taken into account and the ADSE starts generating Different messages are displayed giving information on the status of the generator e At the end of the initialization phase the message displayed is Measure indicating that the ADSE 735 is in slave mode and that it displays the pressure without generating it When the ADSE 735 is switched to the generator mode it will manage the evolution of the pressure During a first phase called Balancing it will bring the pressure on the generation side to the same value as on the output s side in order to avoid a jump in pressure in the instruments to be tested During the next phase called 4 Running the generated pressure will evolve as requested by the user in the fields Set points The last phase called 4 Ready corresponds to the stabilization of the pressure at the requested pressure value e Note nr 1 You are free to change the altitude or rate of climb target values during the generation Just enter the new ta
36. r to calibrate the sensor of the ADSE 735 you need a pressure standard in a climate controlled room with a temperature regulated between 20 and 25 C e Place the ADSE 735 in the climate controlled room next to the pressure standard e Turn iton e Ifthe main menu does not appear on the screen of the remote control unit start the application ADSE 735 refer to paragraph 1 7 3 e Leave the equipment for at least 30 min to stabilize in temperature User Manual Page 52 66 Pitot Static Tester ADSE 735 JATEA OMLCTON 2 2 5 2 Use of the interface To access the calibration mode click on the field Calibration Mode y and enter the password When the equipment is delivered the password is the serial number of the equipment Sensor N 53949 Sensor N Measure hPa 997 36 83949 Calibration correction Standard hPa Measure hPa 997 21 Etalonnage du 10 10 2006 Validate calibration Load data Calibrated point n 1 40 max Etalon hPa gt Jauge hPa 1013 25 1012 99 900 01 001 45 801 03 700 00 602 30 You must calibrate 2 points minimum to validate 490 78 Figure 46 Calibration main menu Different information are displayed on the screen Erreur Source du renvoi introuvable Q The serial number of the sensor Q The uncorrected pressure measured by the sensor in the Measure field Three buttons are accessible as well as a data entry field St
37. re comes back to the atmosphere through a calibrated leak which ensures a full security of the connected equipment gt Built in self check of all the functions of the ADSE 735 on startup e Calibration gt The calibration of the sensor of the ADSE 735 can be performed in our premises or on site by the personnel of ATEQ OMICRON or by a laboratory owning pressure standards User Manual ED 01 Page 7 66 JATEQ OMLCTON 1 3 Characteristics Power supply Pitot Static Tester ADSE 735 AC 110 240 V 50 60 Hz DC 12 32V in option Operating temperature range 10 C to 50 C Storage temperature 20 C to 60 C Total dimensions of the case Length 440 mm Width 325 mm Height 200 mm Power consumption 1 4 Equipment Reference Designation of equipment 12 kg Less than 100 W Reference Pressure Controller and Generator commercial name ADSE 735 EPU Electro Pneumatic Unit PZ 0096 A RCU Remote Control Unit VZ 0006 A Ps pneumatic hose L 5 m P4 0025 A Pt pneumatic hose Pt L 5 m P4 0026 A AC Power supply cable L 5 m T1 0026 A DC power supply cable L 3 m T1 0027 B RCU cable L 5 m T1 0028 A User Manual ED 01 Page 8 66 Pitot Static Tester a ATEQ ADSE 735 1 5 Pressure sensor The sensor used for the pressure measurement and regulation has following characteristics Channel Unit Mea
38. rget value s and click on 4 Execute to have the generator take into account the new value s User Manual Page 38 66 Pitot Static Tester a ATEQ ADSE 735 2 2 3 2 4 Leak Test Leak test min sec vae we Od es 77 sar Manual Ground Menu Po Domain STOP Figure 23 Leak Test Mode Tim D To switch to the Leak Test mode click on the Leak button of the main screen The ADSE 735 goes automatically to the Measure mode The unit for the leak test is the unit selected in the main screen of the manual mode To configure the test enter the time Click on the field to enter the value in minutes and seconds with the digital keyboard To execute the leak test click on start The time is counted down until O minute and O second and the leak value is displayed in the Leak field During the whole test the Value and Rate vary The leak test can be stopped any time by clicking on the STOP button To come back to the main screen of the manual mode click on the Manual button User Manual Page 39 66 Pitot Static Tester a ATEQ ADSE 735 2 2 3 2 5 Return to the ground Ps values Atmosphere Ps set points Execute Domain STOP Figure 24 Tester at ambient pressure By clicking on Ground the ADSE 735 compares the ambient pressure with the pressure in the circuit If the pressure in the circuit is different from the a
39. s First the RCU turns off and then turns on with the window shown below Click on Soft reset to restart normally Fower Menu Select an option either by tapping or by moving the highlight with the navigation arrows and pressing enter Figure 56 Remote Control Unit Power User Manual Page 61 66 Pitot Static Tester ATEQ ADSE 735 e Ifthe RCU is completely blocked the first solution does not work The battery pack must be disconnected Take out the belt Unlock the battery pack of the RCU with a screwdriver or the pencil by turning both screws in the back of the RCU by a half turn Note The block with the power supply cable is not represented on the picture but it is fastened to the battery block Take out the battery block by sliding it on the RCU as shown on the picture Wait for a few seconds for the initialization Slide the battery block back in place Restart the RCU User Manual Page 62 66 Pitot Static Tester ADSE 735 JATEG OTi LcT on 3 3 Maintenance 3 3 1 Internal Your ADSE 745 is conceived to give you full satisfaction for a large number of years As it contains some components potentially subject to ageing filters membranes we recommend to follow the maintenance plan in the appendix in order to ensure a perfect operation on the long run This maintenance plan si valid for a use in normal conditions of temperature dust moisture and salt
40. so that it does not rely on any intermediary computation to perform the comparison between the requested value and the actual value During the evolution from one point to another the evolution rate is taken into account in order to ensure the best possible rate of climb User Manual Page 17 66 Pitot Static Tester a ATEQ ADSE 735 When the current value comes close to the target value the servo control slows down its evolution until complete stop This slowing down threshold is computed depending on the evolution rate and the pressure The controlling frequency is the same as the frequency of refreshment of the information on the pressure value 1 7 2 2 Management of securities Each time that the system gets started a self test is launched It controls the presence of the different electronic boards the correct operation of the modulating valve and the feed back from the pressure sensor During operation the software controls permanently the pressure in order to detect any problem of overpressure or exit out of the flight domain User Manual Page 18 66 Pitot Static Tester a ATEQ ADSE 735 1 7 3 User Interface The user interface RCU can be used outside under the rain between 30 C and 60 C and can withstand a 1 m fall Only the screen should be protected from impact CAUTION Please use only the fingers or the provided pencil for the touch screen Clean the screen with a moisturized non abra
41. surement range Accuracy Ps Pt hPa 30 to 1100 hPa 0 1 hPa 10 C to 40 C 0 15 hPa 10 C to 50 C RVSM Option The sensor used for this option is guaranteed with an accuracy of 0 01 of the full scale and of the full range temperature 1 5 1 Static pressure Ps Ps Unit Range Accuracy Resolution channe Ps hPa 115 to 1200 hPa 0 1 hPa 0 01 hPa ft 2 300 to 15 000 ft 5 ft at O ft Altitude 60 000 ft in option 7 ft at 5000 ft 1 ft Zp 8 ft at 15 000 ft For RVSM option 3 ft at O ft 8ft at 30 000 ft 32 ft at 60 000 ft m 00 to 5 000 m 15mat0m 18 000 m in option 2 1 mat 1 500 m 1m 2 5 m at 4 500 m For RVSM option imat0m 3 m at 10 000 m 10 m at 18 000 m User Manual ED 01 Page 9 66 ATEQ OMLCTON 1 5 2 Total and differential pressure Pt Pt Range channel P Accuracy Pitot Static Tester ADSE 735 Resolution Pt 115 to 1200 hPa 0 1 hPa 0 01 hPa AP 0 to 300 hPa 0 1 hPa 0 01 hPa 20 to 350 kts 3 5 kts at 20 kts 0 2 kts at 150 kts 0 1 kts at 350 kts 50 to 650 km h 1 2 km h at 100 km h 0 4 km h at 300 km h 0 2 km h at 650 km h User Manual ED 01 Page 10 66 JATEQ OMLCTON 1 5 3 Ps dynamic variation Ps channel Unit Range Pitot Static Tester ADSE 735 Accuracy APs At hPa min 10 to 150 hPa min 1 hPaort1 YV 1
42. tmospheric pressure through a calibrated leak Q The computer controls permanently that the pressure altitude speed values as well as the dynamic variations generated remain consistent with the values of the selected flight domain User Manual Page 16 66 Pitot Static Tester a ATEQ ADSE 735 1 7 2 Software 1 7 2 1 Computer The computer s software is written in Borland C Object The use of such a language allows for the segregation of processes and the permanent control of the different software modules in order to obtain a perfect software quality Following modules are included in the software a Management of the serial link a Management of the sensor a Management of the servo controls a Management of the securities 1 7 2 1 1 Management of the serial link The communication between the RCU and the EPU happens through an RS232 link at 19200 bauds 1 7 2 1 2 Sensor Management The pressure information is refreshed each 110 ms on Ps or Pt This information is provided by direct reading of the sensor by an RS485 link The temperature corrections are integrated in the sensor 1 7 2 1 3 Management of the servo controls As soon as the execution of an order is requested the servo control balances the pressures on each side of the isolating electro valve This balance is controlled by an auxiliary sensor The opening threshold is approximately 1 hPa The servo control is managed in the unit of the sensor hPa
43. zive cloth The RCU works with a rechargeable 3800mAH battery pack This allows in normal conditions of use Standard configuration and working temperature between 15 C and 30 C working autonomously approximately 10 H The battery pack is charged automatically from the moment where the RCU is connected to the ADSE 735 and the ADSE 735 is turned on You will find in the appendix the procedures for trouble shooting in case of malfunctions The software of the RCU has been developed under LabVIEW 7 1 and works under Windows for Pocket PC 2003 It manages the communication with the computer and the transfer of information via the RS232 serial link It allows writing and selecting the flight domains running in manual mode or automatic mode by selecting a prewritten flight program and calibrating the unit User Manual Page 19 66 Pitot Static Tester JA TEG ADSE 735 All files are in the directory of the RCU which can be accessed as follows th er a 16 00 D DS obre 2005 eS Today iner information S File Explorer intments RR Built in Storage Start Menu 01 07 03 Programs 01 07 03 01 07 03 01 07 03 01 07 03 01 07 03 01 07 03 01 07 03 01 07 03 26 10 05 2 01 07 03 ra Programs es F Settings Fe Find cj Startup O System EX ADSE 735 26 01 06 2 07M Figure 3 Access path to the directory This directory contains the executable program and three subdirectories a Adse735 exe Appli
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