GE ADTS552F User Manual

GE ADTS552F User Manual

Air data test sets
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GE
Digital Solutions
GE Air Data Test Sets
Adts542F/552F/553F/554F
User Manual K0553 Revision D
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Summary of Contents for GE ADTS552F

  • Page 1 To buy, sell, rent or trade-in this product please click on the link below: https://www.avionteq.com/GE-ADTS-554F-RVSM-Pitot-Static-Test-Set.aspx Digital Solutions GE Air Data Test Sets ADTS542F/552F/553F/554F User Manual K0553 Revision D...
  • Page 2 © 2015 General Electric Company. All Rights Reserved. Specifications are subject to change without notice. GE is a registered trademark of General Electric Company. Other company or product names mentioned in this document may be trademarks or registered trademarks of their respective companies, which are not affiliated with GE.
  • Page 3 Copies of this manual are available in the following languages: French, German, Spanish, Por- tuguese, Chinese, Japanese, Italian and Polish. Hand terminal GUI can also be operated in the following languages: French, German, Span- ish, Portuguese, Chinese, Japanese, Italian and Polish. Contact your local GE Sales office for more details.
  • Page 4 The Bluetooth® wireless technology word mark and logos are registered trademarks owned by Bluetooth® SIG, Inc. and any use of such marks by GE is under license. Other trademarks and trade names are those of their respective owners. For the list of GE approved service centres, go to: www.gemeasurement.com...
  • Page 5 ADTS5XXF device and the user's body must be maintained at all times. ADTS542F/ADTS553F/ADTS554F: Contains Transmitter Module FCC ID: QOQWT41. ADTS552F: FCC ID: 2AAVWADTS552F-01 ADTS Touch This device has been tested and found to comply with the limits for a class A digital device, pursuant to Part 15 of the FCC rules.
  • Page 6 FCC ID: 2AAVWADTSTOUCH-02. CANADA ADTS542F/ADTS552F/ADTS553F/ADTS554F Under Industry Canada regulations, this radio transmitter may only operate using an antenna of a type and maximum (or lesser) gain approved for the transmitter by Industry Canada.
  • Page 7 ADTS542F/ADTS553F/ADTS554F: Contains IC ID: 5123A-BGTWT41 - dipole antenna: 50 ohms, 2.3dBi gain ADTS552F: IC ID: 12097A-ADTS552F01 - patch antenna: 50 ohms, 6.662dBi gain ADTS542F/ADTS552F/ADTS553F/ADTS554F Conformément à la réglementation d'Industrie Canada, le présent émetteur radio peut fonctionner avec une antenne d'un type et d'un gain maximal (ou inférieur) approuvé pour l'émetteur par Industrie Canada.
  • Page 8 This device complies with Industry Canada licence-exempt RSS standard(s). Operation is sub- ject to the following two conditions: This device may not cause interference. This device must accept any interference, including interference that may cause undesired operation of the device. contains IC ID: 12097A-ADTSTOUCH01 ADTS Touch Conformément à...
  • Page 9 This radio transmitter (12097A-ADTSTOUCH02) has been approved by Industry Canada to operate with the antenna types listed below with the maximum permissible gain indicated. Antenna types not included in this list, having a gain greater than the maximum gain indi- cated for that type, are strictly prohibited for use with this device.
  • Page 10 CHINA ADTS542F: CMIIT - 2015DJ5155 ADTS552F: CMIIT – 2015DJ6744 ADTSTOUCH: CMIIT – 2015DJ5598 KOREA 해당 무선설비는 운용 중 전파혼신 가능성이 있음...
  • Page 11 Abbreviations The following abbreviations may be used in this manual, the abbreviations are the same in the singular and plural. Ampere Absolute a.c. Alternating current ADTS Air Data Test Set Aircraft Maintenance Manual Altitude Alt1 Altitude static channel 1 Alt2 Altitude static channel 2 ARINC Air Radio Incorporated...
  • Page 12 Hour High breaking capacity Mercury Hecto metre Hertz Indicated airspeed That is International Electrotechnical Commission Inch inHg Inches of mercury Kilogram Kilometre Knots Liquid crystal display Metre Milliampere Mach Speed ratio to the speed of sound Maximum mbar Millibar Minute or minimum Millimetre Miles per hour Millivolts...
  • Page 13 Pounds per square inch Personal computer Total pressure (Pitot) Pitot pressure channel 1 Pitot pressure channel 2 Differential pressure Pt1-Ps1 Local atmospheric pressure Barometric pressure at sea level Reference Return Goods Authorization (Druck procedure) Root mean square Rate of climb RS232 Serial communications protocol Rate...
  • Page 14 GLOSSARY Adjust To bring to a more satisfactory state; to manipulate controls, levers, linkages, etc. to return equipment from an out-of-tolerance condition to an in-tolerance condition. Align To bring into line; to line up; to bring into precise adjustment, correct relative position or coincidence.
  • Page 15 Replace Remove an item and fit a new or a serviced item. Reset To put back into a desired position, adjustment or condition. Service To perform such operations as cleaning, lubricating and replenishing to prepare for use. Test Ascertain by using the appropriate test equipment that a component or system functions correctly.
  • Page 16 Conversion Chart Pressure UNITS FACTOR (hPa) Pressure UNITS FACTOR (hPa) mbar O @ 20°C 0.978903642 1000.0 O @ 20°C 97.8903642 0.01 0.0980665 Pa (N/m kg/m 980.665 kg/cm 10.0 torr 1.333223684 10000.0 1013.25 mmHg@ 0°C 1.333223874 68.94757293 cmHg@ 0°C 13.33223874 0.4788025898 lb/ft mHg@ 0°C 1333.223874...
  • Page 17: Table Of Contents

    Table of Contents Chapter - 1 INTRODUCTION............................ADTS542F..............................ADTS552F..............................ADTS553F..............................10 ADTS554F..............................12 Dual Hand Terminal ..........................18 Chapter - 2 Packaging ..............................21 Packing for Storage or Transportation.................... 23 Returned Goods Procedure ........................25 Pneumatic Pressure Connections...................... 27 Positioning the ADTS..........................29 Chapter - 3 Preparation..............................
  • Page 18 Chapter - 6 Introduction..............................133 Standard serviceability test........................135 ADTS leak check............................137 Fault codes and error messages ....................... 139 Chapter - 7 Specification ..............................156...
  • Page 19: Introduction

    Chapter - 1 Introduction...
  • Page 20 INTRODUCTION INTRODUCTION The GE family of Air Data Test Sets (ADTS) provide accurate air data to test two, three and four-channel systems. The manufacturer has designed this equipment to be safe when operated using the procedures detailed in this user manual.
  • Page 21: Adts542F

    ADTS542F ADTS542F Figure 1-1: ADTS542F General Arrangement Key to Figure 1-1: Pitot (Pt) pressure port Static (Ps) pressure port ADTS Touch docking connector Test set status indications (see below): a: Power on and self test b: Battery pack status (if fitted) c: Bluetooth®...
  • Page 22: Adts552F

    ADTS542F Key to Figure 1-1: Power cable connector Fuses Test set status indications: Power on and self test: - Off (power Off) - Standby (Yellow) - Self test in progress (Green (flashing)) - Pass/Ready (Green) - Fault (Red) Battery pack status (if fitted):- For LED indications, see section 5.4 “ADTS5xxF battery pack” Bluetooth®...
  • Page 23 ADTS552F ADTS552F The ADTS552F incorporates all the features of the ADTS542F but with an optional communica- tions board, which is located below the cover (10). Figure 1-2: ADTS552F General Arrangement Cover for, optional, communications board K0553 Revision D [EN] English...
  • Page 24: Adts553F

    ADTS553F ADTS553F The ADTS553F incorporates all the features of the ADTS552F but with an additional Static (Ps2) port (11), making it a three channel test set. Figure 1-3: ADTS553F General Arrangement Static (Ps2) port K0553 Revision D [EN] English...
  • Page 25: Adts554F

    ADTS554F ADTS554F The ADTS554F incorporates all the features of the ADTS553F but with an additional Pitot (Pt2) port (12), making it a four channel test set. Figure 1-4: ADTS554F General Arrangement Pitot (Pt2) port K0553 Revision D [EN] English...
  • Page 26 ADTS T OUCH ADTS Touch The ADTS Touch is used to control all required functions. The ADTS Touch can be positioned (docked) on the ADTS or used as a hand held mobile unit via an umbilical cable or using Blue- tooth®...
  • Page 27 ADTS T OUCH The top edge of the ADTS Touch screen features a set of status indicators (A). The status indicator icons show: Figure 1-6: Status Indicators Status indications (from left to right): Battery icon Battery charge level indication is only visible when a battery is fitted to the ADTS Touch Bluetooth®...
  • Page 28 ADTS T OUCH Measure/Control mode: toggle function. The blue indicator identifies the currently selected function: - Indicator left: Measure mode. - Indicator right: Control mode. Pressure/Aeronautical units selection: toggle function. The blue indicator identifies the currently selected function: - Indicator left: Pressure units. - Indicator right: Aeronautical units.
  • Page 29: Dual Hand Terminal

    ERMINAL Dual Hand Terminal The ADTS553 and ADTS554 can be operated with two hand terminals (either ADTS TOUCH or ADTS TOUCH-ER units). Only one of the units (the ‘Master’) can control the ADTS. The second unit (the ‘Slave’) operates as a display when the Master is connected. The hand terminals can be connected to the controller in three ways: •...
  • Page 30 ERMINAL Figure 1-8: ADTS Touch Slave [EN] English K0553 Revision D...
  • Page 31 Chapter - 2 Installation...
  • Page 32: Packaging

    ACKAGING Packaging On receipt of the ADTS check the contents of the packaging against the following lists: Standard ADTS5xxF ADTS Touch Mains cable K0554, Installation and Safety Guide. Options The following options are included, but not limited to : ADTS Touch batteries ADTS Touch extension cable Power supply adaptor and cables Threaded adaptors...
  • Page 33: Packing For Storage Or Transportation

    ACKING FOR TORAGE OR RANSPORTATION Packing for Storage or Transportation To store the ADTS or to return it for calibration or repair carry out the following procedures: The ADTS should be at zero/ambient pressure. Disconnect the hose assemblies and stow in the accessory bag.
  • Page 34 ACKING FOR TORAGE OR RANSPORTATION [EN] English K0553 Revision D...
  • Page 35: Returned Goods Procedure

    Should the ADTS require calibration or become unserviceable, it can be returned to the GE approved service department. Please contact the GE Service Department, either by 'phone, fax or E-mail, to obtain a Returned Goods Authorization (RGA) number or (Return Material Authorization [RMA] in USA), providing the following information: Product (i.e.
  • Page 36 ETURNED OODS ROCEDURE Power Supply Connection The unit must be connected to the correct electrical power supply as stated, adjacent to the power connector. A qualified technician (see page i) must carry out the following procedure. A power isolation device must be accessible at all times. This device can be considered as disconnecting the ADTS power cable or building wall isolation switch.
  • Page 37: Pneumatic Pressure Connections

    NEUMATIC RESSURE ONNECTIONS Pneumatic Pressure Connections When not in use, blanking caps must be fitted to Ps/Pt ports. : When carrying out a leak test, a leak of the blanking cap affects the performance of the NOTE ADTS. The ADTS uses the following AN pneumatic connectors: •...
  • Page 38: Positioning The Adts

    ADTS OSITIONING THE Positioning the ADTS CAUTION TO OPERATE, PLACE THE ADTS ON A HORIZONTAL SURFACE WITH THE FRONT PANEL UPPER- MOST, THIS ALLOWS THE WATER IN THE WATER FILTER TO VENT. WATER CAN CONTAMINATE THE ADTS MANIFOLD AND AFFECT ADTS PERFORMANCE. : In control mode, the water drain, located on the left-hand side of the unit near the cooling NOTE vent, produces a flow of air and some water.
  • Page 39 ADTS OSITIONING THE CAUTION OBSERVE THE APPROPRIATE SAFETY INSTRUCTIONS AND TESTING PROCEDURES DETAILED IN THE AIRCRAFT MAINTENANCE MANUALS AND COMPONENT MAINTENANCE MANUALS. Figure 2-1: ADTS Positioning : Enter a positive correction factor when ADTS is below the aircraft reference. Enter a negative NOTE correction factor when ADTS is above the aircraft reference.
  • Page 40 Chapter - 3 Operation...
  • Page 41: Preparation

    REPARATION Preparation WARNING OBSERVE SAFETY PRECAUTIONS STATED IN LOCAL ORDERS AND THE AIRCRAFT OR EQUIP- MENT SERVICING PROCEDURES. CAUTION IT IS THE RESPONSIBILITY OF THE USER TO MAKE SURE THAT THE PNEUMATIC CONTROL RANGE LIMITS ARE SET BELOW THE MAXIMUM OPERATING LIMITS OF THE EQUIPMENT UNDER TEST.
  • Page 42 REPARATION Make sure the air vents do not become obstructed. Connect the required hoses to the ADTS that are necessary for the test procedures to be carried out. Fit the necessary adaptors for aircraft testing to the hoses. : When connected, take care not to kink or stand on the hoses. NOTE Fit blanks to all the adaptor test points.
  • Page 43: Power-Up Routine

    Table 3-1: Test set status indications If the self test fails (red Fault indication), or for any other reason the test set is considered to be unserviceable, contact GE and return the test set to the GE or GE approved service centre. K0553 Revision D...
  • Page 44: Dashboard

    OWER UP ROUTINE During the Power-up routine, the following screen is displayed showing a Progress bar at the bottom of the screen: Figure 3-1 : ADTS power-up self test screen The ADTS power-up self test screen is displayed for a short time followed by the Dashboard. Wireless connection Wireless connections can only be made on ADTS units which have the Wireless option previously enabled.
  • Page 45 OWER UP ROUTINE Wireless Connection on ADTS542/552F To establish a wireless connection: Ensure that the ADTS Touch is not positioned on the docking connector of the ADTS, or connected to the ADTS using the umbilical cable connector. Switch the ADTS Touch ON. From Dashboard >>...
  • Page 46 OWER UP ROUTINE If the serial number of the ADTS for connection is not in the list, then close the list by touching the "cross" icon. Select New scan for devices. Wait while a search for active devices is performed. 10) Select the required serial number device from the list and touch the "tick"...
  • Page 47: Pitot Static

    ASHBOARD Dashboard The Dashboard shows the top-level menu items, which are: - PITOT STATIC - EPR - SETTINGS - TOOLS - TEST SEQUENCE Figure 3-3: Dashboard K0553 Revision D [EN] English...
  • Page 48 ASHBOARD Figure 3-4: Test Sequence Pitot static EPR see section Engine Pressure Ratio (EPR) Settings Tools Test sequence (swipe horizontally to view) (see section Test sequence) [EN] English K0553 Revision D...
  • Page 49 ITOT TATIC Pitot Static When Pitot Static is selected on the dashboard, the resulting screen will clearly display whether the ADTS is currently controlling the pressures at the Ps and Pt ports (CONTROL) or passively measuring the pressures at the Ps and Pt ports (MEASURE). The condition immediately after power up is always MEASURE, so as to protect any connected systems.
  • Page 50 ITOT TATIC Figure 3-6: Measure mode screen - Multi Channel You can switch the system between aero units and pressure units using the toggle control (4). Control mode When CONTROL mode is selected at icon (1), the ADTS pumps and pressure control functions are activated but will not cause any change in the current pressures unless requested by the oper- ator.
  • Page 51 ITOT TATIC This baseline Pitot Static control screen will typically be used to actively exercise the connected aircraft or system over the required Ps/Pt parameter test range. Figure 3-7: Control mode screen - Single Channel Figure 3-8: Control mode screen - Multi Channel K0553 Revision D [EN] English...
  • Page 52 ITOT TATIC ALT, CAS and Mach The following controls are available when “Aeronautical” units are selected: Figure 3-9: Numbered keypad screen - ALT (ALT1, ALT2 on ADTS553/554) Displays the currently selected altitude. To change the altitude value: Touch the “Aim” value (1) to highlight it. Use the numbered keypad to input the new value.
  • Page 53 ITOT TATIC Figure 3-10: Nudge Increment/Decrement factor selection - Select the new factor (7) from the list. The new factor is selected and the increment/decre- ment factor panel closes. - Touching the up/down controls (5/6) will increment/decrement the “Rate Aim” value by the new factor.
  • Page 54 ITOT TATIC - Ps (Ps1, Ps2 on ADTS553/554) Displays the currently selected pressure. To change the pressure value: Touch the “Aim” value (1) to highlight it, a numbered keypad is displayed. Use the numbered keypad to input the new value. If required, change the rate of change value by touching the “Rate Aim”...
  • Page 55: Rate Timer Mode

    IMER MODE Rate Timer mode To access this screen tap and drag the whole MEASURE or CONTROL screen across to the left The pre-defined time period has an associated wait period that allows pressures to settle before the timing starts. The wait period counts down to zero before the time period starts. Figure 3-11: Rate timer panel - Single Channel K0553 Revision D [EN] English...
  • Page 56 IMER MODE Figure 3-12: Rate timer panel - Multi Channel The Rate Timer starts an internal timer for a pre-defined set of times. On the completion of the time period, the display shows the average rate of change over the time period. To set the WAIT period: On the Rate Timer panel, tap “WAIT (1) to highlight it, the Set Time panel opens.
  • Page 57 IMER MODE On the Set Time panel, select the required “hours”, “minutes” and “seconds” (2). Tap the “Tick” icon (3), the Set Time panel closes and the new time is displayed in the Rate Timer panel. Taping the “Cross” icon (4), cancels the action and closes the Set Time panel. To set the “TEST”...
  • Page 58 IMER MODE Figure 3-14: Measured average rates of change To stop or reset the timer, tap the “cross” icon (7). The timer is reset, the elapsed time indi- cator is white and the word “Idle” is displayed. [EN] English K0553 Revision D...
  • Page 59: Settings

    ETTINGS Settings From Dashboard >> Settings. The Settings screen opens showing the available controls. : The ADTS contains some PIN protected menus. A list of factory default PIN codes can be NOTE found in section PIN codes and PIN protection. The following table is a settings menu overview: Settings menu overview Intensity...
  • Page 60 ETTINGS Settings menu overview Regional settings Date - Date format Time - Time format Language Area of use Screen rotation Bluetooth® Autoconnect * This menu and its submenus are only available when the On/Standby toggle switch is set to On. ** The configuration can only be changed when the On/Standby toggle switch is set to Standby.
  • Page 61 ETTINGS - Pressure units Shows the current selection. To change the pressure units setting: Tap the pressure units panel. Tap the required units radio button. The units radio button panel closes and the pressure units panel shows the selected units. - Aero units Shows the current selection.
  • Page 62 ETTINGS Figure 3-15: PS1 - PS2 Limit (3 Channel Only) - Airspeed mode Shows the current selection. To change the setting: Tap the airspeed mode panel. Tap the required units radio button: - CAS: selects the Calculated Airspeed mode and closes the airspeed mode panel. - TAS: opens the True Airspeed sub-panel containing two additional items: - True Airspeed Temperature: shows the currently selected temperature.
  • Page 63 ETTINGS - Edit limits - Create new limits - Delete limits. View limits - ADTS Max (ADTS552F/553F/554F): Minimum altitude -3000 feet Maximum altitude 60000 feet (65000 feet optional *) Minimum CAS -100.0 knots Maximum CAS 650.0 knots Minimum Ps 35.00 mbar Maximum Ps 1400.00 mbar...
  • Page 64 Maximum ROC 6000 feet/min Maximum RtPs 500.00 mbar/min Maximum RtQc 500.00 mbar/min Alt correction ±100.0 feet ARINC - Max Aero (ADTS552F/553F/554F): Minimum altitude -3000 feet Maximum altitude 60000 feet (65000 feet optional *) Minimum CAS 0.0 knots Maximum CAS 650.0 knots Minimum Ps 71.72 mbar(56.40 mbar optional *)
  • Page 65 ETTINGS * Extended Altitude (EALT) option will be made available through pin number. - Fixed wing: Minimum altitude -1000 feet Maximum altitude 50000 feet Minimum CAS 0.0 knots Maximum CAS 450.0 knots Minimum Ps 115.97 mbar Maximum Ps 1051.00 mbar Minimum Qc 0.00 mbar Maximum Qc...
  • Page 66 ETTINGS Maximum Mach 0.700 Mach Maximum ROC 3000 feet/min Maximum RtPs 109.85 mbar/min Maximum RtQc 109.85 mbar/min Alt correction ±100.0 feet ARINC - ADS Probe: Minimum altitude -2000 feet Maximum altitude 50000 feet Minimum CAS 0.0 knots Maximum CAS 450.0 knots Minimum Ps 91.00 mbar Maximum Ps...
  • Page 67 ETTINGS Edit limits When selected, this function requires you to enter a PIN code. An existing limit set can be edited using this function. To edit limits: Tap Edit limits, a numbered keypad is displayed. Enter your PIN number and tap the “tick” icon. The Edit limits panel opens. Taping the “cross”...
  • Page 68 ETTINGS Delete limits When selected, this function requires you to enter a PIN code. To delete limits: Tap Delete limits, a numbered keypad is displayed. Enter your PIN number and tap the “tick” icon. The Delete limits panel opens. Taping the “cross”...
  • Page 69 ETTINGS Configuration The Unit Configuration ( 2 Channel, 3 Channel or 4 Channel modes) can be changed by selecting the appropriate radio button in the right hand menu. Note that this menu option is only active when the unit is switched to Standby mode. Regional settings Opens a sub-menu containing four items: - Date...
  • Page 70 ETTINGS - Language Shows the current language setting. To change the language setting: Tap the language panel. Tap the required language radio button. The language radio button panel closes and the language panel shows the selected language. - Area of use Shows the current area of use setting.
  • Page 71: Tools

    OOLS Tools From Dashboard >> Tools to display the Tools screen. : The ADTS contains some PIN protected menus. A list of factory default PIN codes can be NOTE found in section PIN codes and PIN protection. The Tools screen opens showing the available controls. The following table is a tools menu over- view: Tools menu overview Calibration (Calibrate sensors)
  • Page 72 OOLS Save/Recall ADTS Touch settings Save ADTS settings Recall ADTS settings Delete ADTS settings Copy all files from USB Copy all files to USB Restore last ADTS settings Default Settings ADTS Manuals Safety Manual User Manual Customer documents Test Sequences Calibration (Calibrate sensors) To access this function you will be required to enter your PIN.
  • Page 73 OOLS Calibration (Software upgrade) To access this function you will be required to enter your PIN. This function is used to implement software upgrades for the ADTS Tap and the ADTS following installation of updated software. The “Calibration” sub-menu contains the following items: ADTS Touch software upgrade •...
  • Page 74 OOLS - Battery: status information about the battery in use. - ADTS Opens the “ADTS status” window containing the following items: - Sensors Shows related sensor status information as follows: - Ps: sensor Ps status. - Pt: sensor Pt status. - Source: sensor source status.
  • Page 75 OOLS To view the status information for the ADTS Touch or ADTS: Touch the image on the screen for the item of interest (1) or (2). Information related to that item is displayed. Touch the displayed information panel to close the panel. - Software installed Information about the installed software and version numbers.
  • Page 76 OOLS - ADTS boot ROM. - Bluetooth - Support Contact information for technical support. You can also get support at: www.gemeasure- ment.com Save/Recall ADTS Touch settings Opens the “Save/Recall User Setup” sub-menu. The “Save/Recall User Setup” sub-menu contains the following items: - Save ADTS Touch settings Opens the “Save settings as”...
  • Page 77 OOLS - Copy all files from USB Allows you to copy files saved on a USB device: Touch the “Copy all files from USB” panel. A dialog appears asking the question “Are you sure you want to copy all the files from the USB?”, “Any files with the same name will be overwritten”, “Yes”...
  • Page 78 OOLS Figure 3-17: ADTS manuals screen Customer documents Touching “Customer documents” displays a list of available customer specific documents installed on your ADTS. Touching the screen on one of the documents results in the display of that document. When a document is displayed, touching the “cross” icon, in the top right corner, closes the document window.
  • Page 79: Go To Ground

    O TO GROUND Go to ground The Aircraft Status icon controls all the active channels on the instrument to ground status. The channels on the ADTS553F and ADTS554F, a multichannel system may be at different altitudes, they will take different times to get to ground status. This is represented on the hand terminal display by two aircraft, which displays the status of the Ps1, Pt1 and Ps2, Pt2 channels whilst they are transitioning to ground status.
  • Page 80 O TO GROUND Figure 3-19: Go to ground main screen - Multiple Channel To change the “Rate: - Tap the “Rate” window (1), the Set Rate panel is displayed. [EN] English K0553 Revision D...
  • Page 81 O TO GROUND Figure 3-20: Set rate panel - Use the numbered keypad to input the new go to ground rate. - Tap the “tick” icon on the keypad (2). The keypad closes and the new rate is displayed. - Tapping the “Cross” icon on the keypad (3), cancels the action and closes the Set Rate panel.
  • Page 82 O TO GROUND Figure 3-21: Start go to ground action The aircraft colour changes to orange while it is being controlled to ground pressure. : Once the green “tick” has been ticked, the Go to Ground process cannot be stopped. NOTE The “cross”...
  • Page 83 O TO GROUND Figure 3-23: Aircraft Going to Ground - Multiple Channel To request all channels to temporarily hold at the current controlled pressure, touch the green "hand" icon (5). The controller status bar will change from CONTROL to HOLD and the “Hand”...
  • Page 84 O TO GROUND Figure 3-24: Hold status during go to ground ramp When at ground pressure, the aircraft colour changes to green. Figure 3-25: Aircraft at ground Tap the “cross” icon (6) to close the Go to ground screen. [EN] English K0553 Revision D...
  • Page 85 O TO GROUND Figure 3-26: Aircraft Going to Ground - Single Channel The display shows “AT GROUND”. The ADTS will remain in this aircraft safe condition for as long as required so that Ps or Pt port pipe connections may be added or removed without creating pressure transients to connected systems.
  • Page 86: Manual Venting Of The Aircraft Pitot And Static Systems

    ANUAL ENTING OF THE IRCRAFT ITOT AND TATIC YSTEMS Manual Venting of the Aircraft Pitot and Static Systems ADTS status on power failure On removal of power, the main output valve linking external ports Pt and Ps to the internal pres- sure controllers will automatically close.
  • Page 87 ANUAL ENTING OF THE IRCRAFT ITOT AND TATIC YSTEMS The order the manual let-down valves are opened is: Figure 3-27: Manual let-down ADTS542F and ADTS552F Number of Channels Application 1st Valve open 2nd Valve open 3rd Valve open 4th Valve open Pitot &...
  • Page 88 ANUAL ENTING OF THE IRCRAFT ITOT AND TATIC YSTEMS Figure 3-29: Manual let-down ADTS554F Number of Channels Application 1st Valve open 2nd Valve open 3rd Valve open 4th Valve open Pitot & Static Pt2 to Ps2 (B) Pt1 to Ps1 (C) Ps2 to Ps1 (A) Ps1 to Atm (D) Pilot &...
  • Page 89: Multi-Channel Advanced Features

    The ADTS553F can function as an ADTS552F by disabling the second static channel. The four channel ADTS554F can function as a three channel ADTS553F by disabling the second pitot channel. It can also function as an ADTS552F by disabling the second pitot channel. Figure 3-30: Settings menu to disable static channel Similarly, the ADTS553 can function as an ADTS552 by disabling the second static channel.
  • Page 90 ULTI HANNEL DVANCED EATURES Aims for the 3 channels can be entered manually in the normal method but it is recommended that the test script is used to reduce operator entry error. Before using the test set the limits must be correctly set for the aircraft under test including the Ps1 Ps2 differential limit.
  • Page 91: Example Basic Aircraft Test Operation Using The Adts542F

    ADTS542F XAMPLE ASIC IRCRAFT PERATION USING THE Example Basic Aircraft Test Operation using the ADTS542F Preparation for Testing If unfamiliar with the features and functions of the ADTS5XXF then it is important for operators to read and understand the following documents before use: •...
  • Page 92 ADTS542F XAMPLE ASIC IRCRAFT PERATION USING THE The direct connections to the aircraft Pitot and Static ports should be made using the adaptor set approved in the AMM, or using equivalents supplied by a specialist port adaptor manufac- turer. We do not recommend the use of improvised connections since this can lead to excessive leakage and potential damage to the aircraft avionics systems.
  • Page 93 ADTS542F XAMPLE ASIC IRCRAFT PERATION USING THE Consult the ADTS limits values for the three predefined tables, HELICOPTER, FIXED WING and MAX AERO in the SETTINGS menu (see section Settings). If a suitable protective limits match cannot be found in one of the three predefined tables then choose CREATE NEW LIMITS and edit your own custom limits table name and preferred values from the offered starting values.
  • Page 94 ADTS542F XAMPLE ASIC IRCRAFT PERATION USING THE to approach and stabilise the aims until the ADTS Touch shows each measurement in green record the difference between the ADTS and the Aircraft instrument under test. Ps Pressure Pt Pressure Qc Diff. Press. Test Point Altitude (feet) (mbar Abs.)
  • Page 95: Engine Pressure Ratio (Epr)

    ATIO Engine Pressure Ratio (EPR) Engine Pressure Ratio (EPR) is sold as a software product option. Contact GE for more details. The ADTS may be used to check EPR sensors and indicators. Use Ps (static) for INLET pressure and Pt (Pitot) for OUTLET pressure.
  • Page 96 (EPR) NGINE RESSURE ATIO Figure 3-31: EPR Control Screen (Method1) Touch the “Aim” value (2). A numbered keypad opens. Enter the desired “Aim” value and touch the “tick” icon. The numbered keypad closes and the previously entered value appears in the “IN” display. Touch the “Aim”...
  • Page 97 (EPR) NGINE RESSURE ATIO Figure 3- 32: EPR Control Screen (Method2) Touch the “Aim” value (2). A numbered keypad opens. Enter the desired “Aim” value and touch the “tick” icon. The numbered keypad closes and the previously entered value appears in the “IN” display. Touch the “Aim”...
  • Page 98 (EPR) NGINE RESSURE ATIO Max (Ratio) 10.0 Min Inlet Rate Max Inlet Rate 1000 mbar/min Min EPR Rate Max EPR Rate 60 mbar/min [EN] English K0553 Revision D...
  • Page 99: Test Sequence

    EST SEQUENCE Test sequence The test sequence mode allows you to run tests, using the ADTS, based on previously defined and stored test sequence data. On the Dashboard, swipe across to select TEST SEQUENCE. The “Test sequence” screen appears showing the last used test sequence title (1). Figure 3-33: Test Sequence screen Touch the test file browse icon (2).
  • Page 100 EST SEQUENCE Figure 3-34: Test Sequences Menu Touch the desired test file radio button. A list of test procedures in that file is displayed. Figure 3-35: Test procedure selection screen [EN] English K0553 Revision D...
  • Page 101 EST SEQUENCE Select the desired test procedure from the list and touch the “tick” icon to select the proce- dure. Touching the “cross” icon closes the procedures menu without selecting a test proce- dure. When the file has loaded, a list of steps, e.g. 1..4, for that procedure is displayed (4). The first step in the list is highlighted.
  • Page 102 EST SEQUENCE The example below identifies the areas or ‘fields’ of the screen where user entries from the CSV file are used to format the screen layout and specific test information. Figure 3-37: Test sequence screen based on Data Field input Test table title, e.g.
  • Page 103 EST SEQUENCE An example of how the data fields of the file may be populated for use in creating the test screen is shown below. Figure 3-38: Test Sequence Data Fields K0553 Revision D [EN] English...
  • Page 104 EST SEQUENCE Saving Finished Test Sequences as CSV Format When the test sequence data sheet has been completed, click “File”, “Save As”. The following screen is displayed: Figure 3-39: Saving the test sequence file Select the file folder destination in the explorer window. Give the file an appropriate “File name”...
  • Page 105 EST SEQUENCE Either, copy and paste the CSV file from the PC file explorer, or drag-and-drop the CSV file from the PC file explorer into the already created “TestSequences” folder of the ADTS Touch. K0553 Revision D [EN] English...
  • Page 106: Pt Only Or Ps Only Control Modes

    NLY OR ONTROL MODES Pt Only or Ps Only Control modes This mode can be used as an alternative to test airspeed indicators (ASI) using just the ADTS Pt or Ps port connected to the ASI. An altitude correction may need entering into the ADTS if there is a height difference and environmental draughts can cause airspeed errors.
  • Page 107 NLY OR ONTROL MODES 11) Tap Home icon to return to the Dashboard. 12) On the Dashboard screen >> Pitot Static. The Measure screen is displayed. 13) Tap the Control (1) icon to toggle the controller on. The following screen is displayed: Figure 3-42: Pt Only control mode The figure above shows that the Ps channel is in Measure mode and the Pt channel is in Control mode, as shown by the indication (2).
  • Page 108: Bluetooth

    An up-to-date list of countries that the ADTS with Bluetooth® wireless technology is licensed to be used in is available upon the request from GE. Bluetooth® operations is normally enabled at point of manufacture, but can also be enabled after sale (product option code ASTOUCH-36).
  • Page 109 ® LUETOOTH Figure 3-43: Bluetooth® Reliable Coverage Area Optimum pairing procedure The following procedure is used to “Pair” the base unit and ADTS Touch: Place the ADTS Touch on (but not docked) or close to the base unit. Power cycle the base unit and ADTS Touch. On the ADTS Touch, select TOOLS.
  • Page 110 ® LUETOOTH Touching the “cross” icon closes the list of devices without making any changes. If the Bluetooth® link drops and does not automatically reconnect, then repeat the procedure above rather than pairing the devices from within the cockpit. K0553 Revision D [EN] English...
  • Page 111: Adts Touch-Er (Extended Range) Bluetooth

    ADTS TOUCH-ER (E ® XTENDED ANGE LUETOOTH ADTS TOUCH-ER (Extended Range) Bluetooth® On large aircraft, particularly if situated out in the open away from buildings or other reflective surfaces, Bluetooth® link performance can be impaired. The ADTS TOUCH-ER has been devel- oped for these instances.
  • Page 112 ADTS TOUCH-ER (E ® XTENDED ANGE LUETOOTH WARNING AT LEAST 20cm OF SEPARATION DISTANCE BETWEEN THE TOUCH-ER ANTENNA AND THE USER’S BODY MUST BE MAINTAINED AT ALL TIMES WHEN BEING USED WITH THE ANTENNA EXTENSION KIT. ENSURE ANTENNA SUCTION CUP IS ATTACHED TO THE COCKPIT WINDOW BEFORE CONNECTING EXTENSION KIT TO THE TOUCH-ER TO PREVENT THE 20cm SEPARA- TION FROM BEING INFRINGED UPON.
  • Page 113 ADTS TOUCH-ER (E ® XTENDED ANGE LUETOOTH In general terms, the Bluetooth® performance with the different options can be described as follows, although this is very dependant upon aircraft type, and its immediate environment (in terms of RF reflecting surfaces). Performance inside a hangar environment is generally better than when the aircraft is out in the open on an airfield.
  • Page 114 Chapter - 4 Calibration...
  • Page 115 NTRODUCTION Introduction For the system to remain accurate, a calibration check should be carried out at regular intervals. The recommended calibration period is 12 months. If the accuracy of the system is not within the specification, carry out a calibration adjustment. K0553 Revision D [EN] English...
  • Page 116: Pin Codes And Pin Protection

    CODES AND PROTECTION PIN codes and PIN protection The ADTS contains some PIN protected menus. The following table lists the factory set default PIN numbers: Settings ADTS settings Edit limits 0268 Create new limits 0268 Delete limits 0268 Change supervisor PIN 0268 Tools Calibration (Calibrate sensors)
  • Page 117: Calibration Process

    ALIBRATION PROCESS Calibration process The calibration process is PIN protected. This chapter describes the Ps and Pt sensor calibration. The Tools, Calibration Sensor menu contains the calibration adjustment as part of the function Calibration check. : Calibration checks must be performed within the calibration check menu because the main NOTE Ps/Pt measure display screen Pt reading includes an “Auto Zero”...
  • Page 118 ALIBRATION PROCESS Accuracy specifications(k = 2, 95% uncertainty)Includes: NL, H and R over the ADTS operating temperature range and calibration stability over 12 months and calibration equipment uncertainty stated in ADTS552/553/554F Table 4-3 Test method Pneumatic pressure Ps Range: Compared against calibration 72 mbar to 1130 mbar absolute standard (EALT option 57 mbar)
  • Page 119 ALIBRATION PROCESS Suggested calibration check points Ps (Calibration check points) Pt (Calibration check points) 56.39 mbar (~65,000 ft)** 56.39 mbar** 71.71 mbar (~60,000 ft)* 71.71 mbar* 92.00 mbar (~55,000ft) 92.00mbar 178.74 mbar (~41,000ft) 178.74mbar 314.85 mbar (~29,000ft) 314.85mbar 465.63 mbar (~20,000ft) 465.63mbar 696.82 mbar...
  • Page 120: Calibration Description

    ALIBRATION DESCRIPTION Calibration description The date of calibration adjustment is logged and stored during this procedure. It is important that the ADTS Touch clock date is checked before starting a calibration adjustment or an incor- rect date may be recorded. Instructions for checking and setting the time and date can be found in section Settings.
  • Page 121 ALIBRATION DESCRIPTION If the recorded difference exceeds the allowable tolerance, carry out the “Calibration adjustment” procedure detailed below. Repeat this procedure for the other channel. Calibration adjustment The procedure applies known pressures to the ADTS and then entering the exact applied pres- sure using the ADTS Touch.
  • Page 122: Completion Of Sensor Calibration

    OMPLETION OF SENSOR CALIBRATION Completion of sensor calibration After completion of all calibration adjustment procedures, carry out the following: Make sure the calibration standard and the ADTS are at atmospheric pressure. Disconnect the calibration standard from the ADTS. If there is no further calibration or testing required, exit menus, select standby or switch off the ADTS.
  • Page 123 Chapter - 5 Maintenance...
  • Page 124 NTRODUCTION Introduction This section details the before-use tasks and the weekly inspection to be carried out by the oper- ator. The maintenance chart shows the maintenance tasks, the periodicity of each task and a code referenced to the tasks detailed in Table 5.1. Task Code Period...
  • Page 125: Battery Care And Maintenance

    ATTERY CARE AND MAINTENANCE Battery care and maintenance ADTS Touch battery pack The battery unit contains a Lithium Ion battery which requires no user maintenance. Prolonged exposure to temperature extremes may significantly reduce battery lifetime. For maximum lifetime, avoid prolonged periods where the battery is exposed to temperatures outside the range -30°C to +45°C.
  • Page 126: Maintenance Tasks

    AINTENANCE ASKS Maintenance Tasks Code Task Check that all the equipment is present, record any deficiencies. Visually inspect the exterior of the ADTS and its associated equipment for obvious signs of damage, dirt and the ingress of moisture. If necessary, use mild liquid detergent and a lint-free cloth to clean the external surfaces, see the “Safety and Installation”...
  • Page 127: Routine Maintenance

    OUTINE AINTENANCE Routine Maintenance Absolute cleanliness of the work area, tools and equipment are essential. Replacing the output connector o-ring After inspection as detailed in maintenance task B, carry out the following if the o-ring is worn or damaged: Figure 5-1: Replacing the o-ring Carefully remove the o-ring from the small groove at the top of the connector.
  • Page 128: Software Updates

    OFTWARE UPDATES Software updates When software updates are available, they can be downloaded from the GE website to a USB memory stick and used to update the applications on the ADTS and ADTS Touch. Context sensitive help pages are updated with software version increments. ADTS (PDF) manuals are updated without prompt when a newer version of the manual is available via the software update procedure.
  • Page 129 OFTWARE UPDATES Figure 5-2: Software update folders 13) Copy these five folders to the root directory of the USB memory stick ready for transfer to the ADTS Touch. 14) Once the files have been downloaded to the USB memory stick, safely remove the USB memory stick from the computer.
  • Page 130 Selecting “No” closes the dialog without making any changes. Downloading ADTS manuals Go to www.gemeasurement.com. The “GE Measurement & Control” page is displayed. On the top level menu bar, click Support. Menu items under that header are shown. Click Download Center. The “Download Center” page is displayed showing the search panels.
  • Page 131 OFTWARE UPDATES Using the Search by Product drop-down search boxes, select: - “Test & Calibration”. - “Pitot Static Testers”. A list of available downloads is displayed containing all available software updates, user manuals and data sheets. Select the appropriate manual from the list. The file is displayed as a PDF with a set of func- tion buttons in the top right corner.
  • Page 132 Chapter - 6 Testing and Fault Finding...
  • Page 133 Introduction Limited testing and fault finding can be carried out by the operator. Units can be returned to the nearest GE (www.gemeasurement.com) or approved service centre for fault finding and rectifi- cation. At power-up, the ADTS indicates if there is a fault by flashing an error code and/or displaying a message.
  • Page 134: Standard Serviceability Test

    TANDARD SERVICEABILITY TEST Standard serviceability test The following procedure shows if the ADTS is serviceable and checks functions and facilities: Connect power to the unit. Make sure the blanking caps are fitted to the front panel outputs. Set the power supply switch to ON. Check that the power indicator is on and flashing green.
  • Page 135: Adts Leak Check

    ADTS LEAK CHECK ADTS leak check Before carrying out a leak check, allow at least 15 minutes for the ADTS to warm-up. Set-up From Dashboard >> Settings. In the Settings >> ADTS Settings. Select ADTS LIMITS >> then SELECT LIMITS" >> select MAX AERO. Return to ADTS Settings.
  • Page 136 ±0.6 mbar/min. If the rates are greater than this value, allow further thermal stabilization time and re-test. If repeated failures occur, return the unit to GE or a GE authorised repair depot. [EN] English...
  • Page 137: Fault Codes And Error Messages

    If the display shows an error message, the unit should be switched off and then on again. If the display still shows an error message after switching on again. the unit should be returned to GE or a GE authorised repair depot.
  • Page 138: Error Codes

    RROR ODES Error Codes Error Number Description Boot database queue has failed Memory Allocation for Bootloader task has failed Memory Allocation for Bootloader environment has failed Bootloader task registration has failed Failed to warm up Ps sensor failed or disconnected Autoleak recovery activated Bias Channel Pressure Ps Failed Bias Channel Pressure Pt Failed...
  • Page 139 RROR ODES Error Number Description Demand NULL EXP out of range LOG out of range Measured NULL Controller Pool Control Memory Invalid Next State Test set must be at ground Pressure Leak in Ps. Leak rate = Pressure Leak in Pt. Leak rate = Invalid Ps Demand Ps pressure not settling Ps Aim Overshoot...
  • Page 140 RROR ODES Error Number Description Ps vacuum control valve cannot be calibrated Pt vacuum control valve cannot be calibrated Invalid Curve Records Invalid Curve State Valve Bias Select Fail Valve Bias Values Qc Negative so Clamped to Zero Current pressure limits exceeded Database Change Failed Database Clear Failed Database Copy...
  • Page 141 RROR ODES Error Number Description Abort Detected ABORT INSTIGATED ADC7822 Invalid Input Calibration switch in ON position when commanded OFF Calibration switch in OFF position when commanded ON Calibration Latch indicates invalid inputs ALTERA Event ALTERA HISR Failed ALTERA LISR Failed ALTERA is not present or not responding Application code FLASH is not blank BIT Clear Byte...
  • Page 142 RROR ODES Error Number Description CAN Loopback using test remote device has failed CAN test transmission has failed No CAN Response from remote board CAN Task Buffer Full CAN Task HISR Fail CAN Task LISR Fail CAN Task Memory fail CAN Task Queue Fail CAN Task task Fail Data FLASH is not blank...
  • Page 143 RROR ODES Error Number Description Flash has failed operation Invalid Flash Invalid FLASH device selected Invalid sector FLASH device is not present Sector is protected Invalid I2C Board Solenoid Null Pointer Driver Initialisation Fail Invalid FLASH device Keypad Timer Failed Device Length Ps sensor failed Pt sensor failed...
  • Page 144 RROR ODES Error Number Description Pump monitoring has failed when pumps commanded ON Pump monitoring has failed when pumps commanded OFF Pump monitoring has failed when pressure pump commanded ON Pump monitoring has failed when vacuum pump commanded ON Pump monitoring has failed when heater commanded ON Pump Timer Failed Invalid PWM Channel QSPI LISR Failed...
  • Page 145 RROR ODES Error Number Description PT apply valve failed - short PT apply valve failed - open PT release valve failed - short PT release valve failed - open Solenoid valves have failed when all commanded OFF Solenoid Timer Failed Invalid Solenoid ID SPI Entry parameters are invalid EEPROM Block is null...
  • Page 146 RROR ODES Error Number Description Restext Text Size Screen Screen Overflow Screen has failed to initialise Screen Failure Invalid base screen Screen Stack Default Handler Screen Stack Overflow Invalid screen selected Screen Stack Softkey overflow Status Line Internal Software Fault Abort sequence started by user Cannot Modify Altitude Correction in Pressure Units Changed Aim to ARINC Limit...
  • Page 147 RROR ODES Error Number Description LDK Task Failed Read only Limits Hourscreen timer failed Workstation event has failed to initialise Workstation memory pool has failed Workstation serial HISR failed to initialise Workstation task has failed to initialise SPI Parameter Error Test Message Ground Request in Leak Mode.
  • Page 148 RROR ODES Error Number Description Watchdog Interrupt handler has failed to initialise Hand terminal timer handler has failed to initialise Connected hand term has failed to respond. Disconnecting power Out of working temperature range Valve characterisation data is invalid. Restoring from FLASH Valve constant a1 is out of range Valve constant b1 is out of range Valve constant Vb1 is out of range...
  • Page 149 RROR ODES Error Number Description Valve constant a4 is out of range Valve constant b4 is out of range Valve constant Vb4 is out of range Valve constant Vl4 is out of range Valve constant Fl4 is out of range Valve constant G4 is out of range Valve constant Fmax4 is out of range Controller limits corrupted...
  • Page 150 RROR ODES Error Number Description Reserved Cannot connect Hand Term while safe at ground for this version of ADTS505 RtCAS is fixed and cannot be altered Calibration date not entered. Enter the calibration date No Handset code in LDK flash Invalid Pt/Pt rate aim entry whilst in aero units Invalid Qc/Qc rate aim entry whilst in Pt ramp mode Invalid Pt/Pt rate aim entry whilst in Qc ramp mode...
  • Page 151 RROR ODES Error Number Description PT control sensor EEPROM write error PS control sensor checksum error PS control sensor diode ADC acquisition error PS control sensor frequency acquisition error PS control sensor EEPROM write error LED IO expander initialisation error Valve IO expander initialisation error Power check initialisation error in external ready Power check initialisation error in internal ready...
  • Page 152 Chapter - 7 Specification...
  • Page 153 PECIFICATION Specification For the most up to date equipment specification, refer to the current data sheet, as follows. • ADTS542F, 920-648x • ADTS552/553/554F, 920-659x In addition to the information contained in the latest data sheet, note the following: ADTS542F - Above 9,144 m (30,000 ft) the rate of climb (ROC/Rt Ps/Pt) into a 3L total volume (Ps 2L + Pt 1L) performance is limited by pump capability (that may vary higher or lower depending on pump running hours, equipment under test volume, ambient temperature and barometric pressure of the day).

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