GE Druck ADTS 405 F Mk2 Instruction Manual Download Page 138

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Appendix B. Errors and Warnings

120 | ADTS 405 R/F Mk2 Instruction Manual-English

309

CANNOT CONTROL

Failed pump test.

Check system limits.

310

PUMP TEST FAILED

Pump not achieving limits.

Set lower limits.

Table B-2: Warning Messages

Number

Message

Probable Cause

Action

Summary of Contents for Druck ADTS 405 F Mk2

Page 1: ...www gemeasurement com GE Data Classification Public Druck ADTS 405 R F Mk2 Air Data Test Set Instruction Manual ...

Page 2: ......

Page 3: ...ential operating and Safety instructions that must be followed to ensure safe operation Use suitably qualified Technicians and good engineering practice for all procedures in this publication Pressure Do not apply pressure greater than the maximum safe working pressure specified in this manual when using the ADTS 405 Mk2 series Toxic Materials There are no known toxic materials used in this equipm...

Page 4: ...ertissement qui indique que l utilisateur doit consulter le manuel d utilisation This symbol warns the user of the danger of electric shock Ce symbole alerte l utilisateur sur le danger de choc électrique Do not dispose of this product as household waste Use an approved organization that collects and or recycles waste electrical and electronic equipment For more information contact one of these Ou...

Page 5: ... CAS Calibrated airspeed dc Direct current e g For example EOC End of conversion EPR Engine pressure ratio EPROM Electrically programmable read only memory etc And so on ft Foot g Gauge Hg Mercury Hz Hertz IAS Indicated airspeed i e That is IEEE 488 Institute of Electrical and Electronic Engineers Standard 488 Data in inch kg Kilogram kts Knots LED Light emitting diode m Metre mA Milliampere max M...

Page 6: ...e adjustment correct relative position or coincidence Assemble To fit and secure together the several parts of to make or form by combining parts Calibrate To determine accuracy deviation or variation by special measurement or by comparison with a standard Check Make a comparison of a measure of time pressure temperature resistance dimension or other quality with a known figure for that measuremen...

Page 7: ...ticular state or condition especially in a state of efficiency or validity Operate Ensure that an item or system functions correctly as far as possible without the use of test equipment or reference to measurement Readjust To adjust again to move back to a specified condition to bring back to an in tolerance condition Reconnect To rejoin or refasten that which has been separated Refit Fit an item ...

Page 8: ... calculate as follows INFORMATION Service by unauthorized sources will affect the warranty and may not guarantee further performance Pressure Units Factor hPa Pressure Units Factor hPa mbar 1 0 cmH2O 20 C 0 978903642 bar 1000 0 mH2O 20 C 97 8903642 Pa N m2 0 01 kg m2 0 0980665 hPa 1 0 kg cm2 980 665 kPa 10 0 torr 1 333223684 MPa 10000 0 atm 1013 25 mmHg 0 C 1 333223874 psi 68 94757293 cmHg 0 C 13 ...

Page 9: ...3 ADTS 405R Mk2 Rack mounted Version 9 2 4 Positioning of the ADTS 10 2 4 1 ADTS 405R Mk2 Rack mounted Version 10 2 4 2 ADTS 405F Mk2 Flight line Version 11 2 5 Product Views 12 3 Getting Started 15 3 1 Preparation 15 3 2 Start up 15 3 2 1 Connections 15 3 2 2 Power up 16 3 2 3 Units of Measure 18 3 3 Keypad Display 19 3 4 Operation Quick Reference 19 3 5 Operating Mode Overview 22 3 5 1 Measure M...

Page 10: ...9 Engine Pressure Ratio EPR 37 4 9 1 Example EPR Test 37 4 10 Testing Aircraft Systems or UUT 38 4 10 1 Go To Ground and Shutdown 38 4 10 2 While Going to Ground 38 4 10 3 Resuming Testing after Going to Ground 38 4 11 Setup Options 39 4 11 1 Change Units in Full Setup Mode 39 4 11 2 Change Units in Minimum Setup Mode 40 4 12 Configuration Options 40 4 13 Communications Panel Options 40 4 13 1 Eth...

Page 11: ...59 6 6 Fault Diagnosis 60 6 7 Ventilating after Overpressure 62 6 8 Further Testing 63 6 8 1 Environmental and Preliminary Operations 63 6 8 2 Pressure Leak Check 63 6 8 3 Vacuum Leak Check 64 6 8 4 Range Check 64 6 8 5 Controller Stability 64 6 8 6 External Communication Ports 66 6 8 7 Altimeter Encoder 68 7 Reference 71 7 1 Introduction 71 7 2 Keypad Display 72 7 2 1 F1 F4 72 7 2 2 ALT Ps 72 7 2...

Page 12: ...OPEN OUTPUT VALVES 87 7 3 10 SETUP MORE SYSTEM SELF TEST 87 7 3 11 SETUP ALT 87 7 3 12 SETUP SPEED AUTO ZERO 87 7 3 13 SETUP SPEED CAS TAS 88 7 3 14 SETUP SPEED Pt TEMPERATURE 88 7 3 15 SETUP MACH 88 7 3 16 SETUP RATE TIMER 88 7 3 17 SETUP RATE 88 7 3 18 SETUP LEAK MEASURE CONTROL AUTO LEAK 89 7 3 19 SETUP LEAK MEASURE CONTROL AUTO LIMIT 89 7 3 20 SETUP GROUND 89 7 3 21 SETUP PORT 89 7 3 22 SETUP ...

Page 13: ...PTIONS DISPLAY TYPE 96 7 4 23 CONFIG MORE DISPLAY OPTIONS OPTIONS 96 7 4 24 CONFIG MORE DATE FORMAT 96 7 4 25 CONFIG MORE SETUP MODE 97 7 4 26 CONFIG SPEED AUTO ZERO 97 7 4 27 CONFIG SPEED CAS TAS 97 7 4 28 CONFIG SPEED Pt TEMPERATURE 97 7 4 29 CONFIG RATE TIMER 97 7 4 30 CONFIG RATE 97 7 4 31 CONFIG LEAK MEASURE AUTO LEAK ON OFF 97 7 4 32 CONFIG LEAK MEASURE AUTO LEAK LOCK 97 7 4 33 CONFIG LEAK M...

Page 14: ...Reserved 8 4 2 Rate Control 105 8 4 3 Control Response 106 8 4 4 Dynamic Testing 106 8 4 5 Control Offset 106 Appendix A Menus 107 A 1 Full Setup Menu 108 A 2 Minimum Setup Menu 111 A 3 Configuration Menu 112 Appendix B Errors and Warnings 117 B 1 Error Messages 117 B 2 Warning Messages 118 ...

Page 15: ...isplay 28 4 3 Triple Display 29 4 4 Rate Timer Display Aeronautical Units 29 4 5 Rate Timer Display Pressure Units 30 4 6 Pt Only Display 30 4 7 Configuring Windows For ADTS Subnet IP Address 41 4 8 Ping Test From Windows Command Prompt 42 4 9 PuTTY Configuration 43 4 10 Changing the Default Password 43 4 11 ADTS File System Directories Screen 45 5 1 Output Connector O ring Seal 51 5 2 ADTS 405F M...

Page 17: ...t 49 5 3 Tool and Test Equipment Requirements 50 5 4 AC Input Connector 56 5 5 DC Input Connector 56 6 1 Fault Advice and Action 61 6 2 Optional Cable AAU 32 Units 69 7 1 Rates in Aeronautical Units 75 7 2 Rates in Pressure Units 75 7 3 Aeronautical Units Dual Display 85 7 4 Pressure Units Dual Display 85 7 5 Aeronautical Units Triple Display 86 7 6 Pressure Units Triple Display 86 7 7 Setup Modes...

Page 19: ... operated as measure only channels with leak testing facility or each can be control channels producing true pressure conditions for altitude and airspeed To protect sensitive instruments and equipment a ground facility automatically and safely controls both channels to atmospheric pressure at the previously entered rates of change and then informs the operator when both channels are safely at gro...

Page 20: ...g limits are supplied with the ADTS 405 Mk2 Table 1 1 Operating Limits 850 kts Range Parameter Max Limits Standard Limits Civil Limits Min Alt 3 000 ft 2 000 ft 1 000 ft Max Alt 105 000 ft 80 000 ft 50 000 ft Min CAS 100 kts 0 0 kts 0 kts Max CAS 850 kts 850 kts 450 kts Min Ps 3 0 mbar 27 615 mbar 115 972 mbar Max Ps 1355 00 mbar 1088 657 mbar 1050 406 mbar Min Qc 1 352 00 mbar 0 0 mbar 0 0 mbar M...

Page 21: ...ax CAS 1 000 kts 1 000 kts 450 kts Min Ps 3 0 mbar 27 615 mbar 115 972 mbar Max Ps 1355 00 mbar 1 128 029 mbar 1050 406 mbar Min Qc 1 352 00 mbar 16 303 mbar 0 mbar Max Qc 2 500 00 mbar 2 490 50 mbar 368 01 mbar Max Mach 14 97 5 1 Max ROC 1000 000 ft min 15 000 ft min 6 000 ft min Max Rate CAS 2 000 kts min 700 kts min 600 kts min Max Rate Ps 10 000 00 mbar min 200 00 mbar min 100 00 mbar min Max ...

Page 23: ... supply cable 2 m or 10 m regional plug as per order iv Hand terminal optional v Hand terminal cable 2 m optional vi Hand terminal cable 18 m optional vii User Manual K0572 this publication viii O ring kit ix Safety and Installation Guide 124M8686 2 1 2 ADTS 405R Mk2 Standard Packaging List i Rack mount ADTS 405R Mk2 ii Power supply cable 2 5 m regional plug as per order iii User Manual K0572 this...

Page 24: ...t the hand terminal cable from the hand terminal When using packing materials other than the original proceed as follows 1 Wrap unit in polyethylene sheeting 2 Select a double wall cardboard container Inside dimensions must be at least 15 cm greater than the equipment The carton must meet test strength requirements of 125 kg 3 Protect all sides with shock absorbing material to prevent equipment mo...

Page 25: ...for Storage or Transportation 2017 General Electric Company All Rights Reserved ADTS 405 R F Mk2 Instruction Manual English 7 Figure 2 1 Equipment and Parts 3 1 2 A 9 12 11 14 5a h 6a p A 4 7a b 13a b 8a b 10a b ...

Page 26: ...Lead Japan 2 5 m 6a AA405F 1 AC Power Lead UK 2 m ADTS 405F 6b AA405F 2 AC Power Lead UK 10 m 6c AA405F 3 AC Power Lead USA Canada 2 m 6d AA405F 4 AC Power Lead USA Canada 10 m 6e AA405F 5 AC Power Lead Europe 2 m 6f AA405F 6 AC Power Lead Europe 10 m 6g AA405F 7 AC Power Lead Australia New Zealand 2 m 6h AA405F 8 AC Power Lead Australia New Zealand 10 m 6i AA405F 9 AC Power Lead India 2 m 6j AA40...

Page 27: ...m ADTS 405R 10d AS405 54 1729M0 Green Hose 15 m 11 AS405 60 1891M0 Altimeter Encoder Cable ADTS 405F R 12 AS405 82 1891M0 O ring Kit ADTS 405F R 13a AA500F 22 Hose Connector AN4 ADTS 405F R 13b AA500F 23 Hose Connector AN6 14 AS405 31 1891M0 DC Power Cable ADTS 405F RISK OF ELECTRIC SHOCK The power supply switch on the front panel is not classified as a disconnecting device To isolate the power su...

Page 28: ...icated on the mimic panel and the UUT See Section 7 3 11 SETUP ALT on page 87 for details of altitude correction Figure 2 2 ADTS 405R Mk2 Altitude Reference The corrected altitude output equals the true altitude output increased by height difference See equation below Note The Δh altitude correction value should be negative when the ADTS is positioned higher than the unit under test WARNING Observ...

Page 29: ...on page 87 for details of altitude correction Figure 2 3 ADTS 405F Mk2 Altitude Reference The corrected altitude output equals the true altitude output increased by height difference See equation below Note The Δh altitude correction value should be positive when the ADTS is positioned below the aircraft WARNING The ADTS should not be placed in contact with hazardous fuel vapor concentrations 1 Fl...

Page 30: ...y fuses optional 8 AC power supply fuses 9 DC power supply connector optional 10 Cross bonding connector 11 AC power supply connector 12 Vacuum input connector 13 Auxiliary vacuum output connector 14 Pressure input connector 15 Pump power supply switch 16 Calibration enable switch 17 Power supply switch 18 Altitude sensordatum height altitude reference level 19 Pitot output connector 20 Static out...

Page 31: ...cations connectors 2 Altitude sensordatum height altitude reference level 3 Solenoid valve status indicator 4 System status indicator 5 Hand terminal connector 6 Altitude encoder connector optional 7 Static output connector 8 Keypad and display 9 Pitot output connector 10 Power connection indicators 11 Power supply switch 12 Calibration enable switch 1 2 3 4 5 6 7 8 9 10 11 12 ...

Page 32: ...xpansion port 8 is not in use 1 AC power supply connector 2 DC power supply connector optional 3 AC fuses holder 4 Pressure regulator 5 Source vacuum input connector 6 Source pressure input connector 7 Cooling fan air intake 8 Expansion port used with GE PV103R pump unit 9 Pitot output connector optional 10 Static output connector optional 11 Communications connectors 12 Expansion port dongle 1 3 ...

Page 33: ...p 3 2 1 Connections a Connect the hoses for the test procedures to the air data test system i Red hose to the STATIC output Ps ii Blue hose to the PITOT output Pt b Temporarily seal the free ends of the hoses Note When connected take care not to restrict air flow to the hoses c Connect the hand terminal to the air data test system through the hand terminal connector on the front panel If necessary...

Page 34: ...rmal Note Vxx xx will display the current software version number 2 Controller power up screen After a short time the display shows the following The system status indicator LED changes to orange in color 3 Date of the last calibration and type of main transducer fitted Note Date format can be set to a leading value of day or month in SETUP 4 Self test message and front panel LED status The system...

Page 35: ...ote 1 The ADTS 405 Mk2 is a continuous self monitoring system If the system detects an error the display shows an error message Lists of errors are detailed in Section 6 2 Error Messages on page 57 Note 2 The display at power up can be changed see Section 7 3 6 SETUP MORE DISPLAYS OPTIONS DISPLAY TYPE on page 85 INFORMATION The ADTS 405 Mk2 system may now be used But for full specification accurac...

Page 36: ...Calibrated and True Airspeed CAS TAS kts km h mph Mach MACH Rate of Climb ROC ft m m m m s hm m Rate of Airspeed Rt CAS kts m km h m mph m Rate of Mach RtMCH Mach m Table 3 2 Pressure Units of Measure Pressure Function Display Abbreviation Displayed Unitsa a Where P is the currently selected pressure units from the following list mbar inHg mmHg inH2O 4 C inH2O 20 C psi hPa kPa inH2O 60 F kg cm2 or...

Page 37: ...nctions See Chapter 7 on page 71 for full details Table 3 3 Keypad Key Functions Key Function Function keys soft keys for menus Altitude Aeronautical units or Ps Pressure units ALT Ps ROC Ps RATE MEASURE LEAK CONTROL PRINT SPEED Qc TIMER RATE GROUND TEST EXECUTE PROGRAM MACH Pt HOLD PORT HELP EPR RATE REMOTE LOCAL SETUP 000 CLEAR QUIT ENTER 1 2 3 0 4 5 6 7 8 9 STATIC PITOT F1 F2 F3 F4 Alt 0 ft Lea...

Page 38: ...nt value Press again to release Rate of change of pitot parameter Press SPEED QC or MACH Pt then press RATE Switches between measure mode for leak testing and control mode Controls Ps to atmospheric pressure and Qc to zero at current rates of change See Line Switching Unit user manual Switches toggles between remote and local operation Prints current parameter values Execute downloaded test progra...

Page 39: ... The settings in configuration menu are permanent They are not lost after a power down For more details see Appendix A 3 Configuration Menu on page 112 Increases the aim value Decreases the aim value Number entry Minus sign for first number entry 000 thousand if not the first number of entry Clear number entry or quit from menu or clear warning message Complete number entry This combination of key...

Page 40: ...l ground pressure The ADTS 405 Mk2 always powers up in Measure mode with the pressure controllers off When changing to Control Mode the pump unit must be switched on and producing the correct pressure and vacuum Each operating function shows the required key presses to set displays and selections INFORMATION Once initialized wait 15 minutes to allow the pressure measurement system to reach a stabl...

Page 41: ...ruction Manual English 23 3 5 1 Measure Mode Pressure Measurement Mode Measured value To select the measured parameter press or or Units of measurement Measured parameter Leak Measure when measure mode selected Change display single dual or triple press Change units from aeronautical to pressure ...

Page 42: ...struction Manual English 2017 General Electric Company All Rights Reserved 3 5 2 Control Mode Pressure Control Mode From leak measure press For ADTS 405F Mk2 set the pump switch to PUMP ON Aim of 5 000 ft press Return to leak measure at new altitude ...

Page 43: ... for the heated gas to cool and the pressure to stabilize When setting the rate timer consider three factors 1 The volume of the system to be tested large volumes take longer to stabilize 2 The pressure change the higher the change the greater heat generated 3 The ambient air temperature Static channel altitude 5 000 ft measure leak Rate timer setup 1 Wait 05 00 minutes 2 Test 01 00 minutes Displa...

Page 44: ...Local Ground Pressure Dual parameter display Single parameter display Note In Leak Measure use F2 and F3 for QFE and QNH information F1 is only valid in Control mode Note This ground value will not be zero and depends on local atmospheric pressures erh emvƉiph epxmxyhi Note Safe to disconnect pipes and adaptors from the aircraft or component under test ...

Page 45: ...or that channel e g display airspeed rate press SPEED Qc then RATE ROC Ps Rate may be directly pressed without first pressing ALT Ps Note The displayed parameters depend on the last keys pressed To display two parameters a Press each value parameter in turn e g display altitude and airspeed together press ALT Ps then SPEED Qc b In control mode an arrow at the right hand end of the aim value indica...

Page 46: ...nute Figure 4 1 Single Display Figure 4 2 Dual Display 1 Controlled or measured parameter 2 Measured value 3 T for timed rate of change 4 Units of measurement 5 Pointer for parameter i e aim that changes on data entry 6 Special messages e g warm up period 7 Aim set point or target in control mode or Leak Measure when the pressure controller is off 1 Controlled or measured parameter 2 Measured valu...

Page 47: ...key ALT ROC etc or CLEAR QUIT exits the rate timer displays Figure 4 4 Rate Timer Display Aeronautical Units 1 Constant indication of values 2 Measured value 3 T for timed rate of change 4 Units of measurement 5 Special messages e g warm up period 6 Pointer for parameter i e aim that changes on data entry 7 Aim set point or target in control mode or Leak Measure when the pressure controller is off...

Page 48: ...ETUP switched off or in minimum mode 1 Measured parameter 2 Measured value 3 T for timed rate of change 4 Units of measurement 5 Special messages e g warm up period 1 Always displays Alt for altitude 2 Measured altitude 3 T for timed rate of change 4 Units of measurement 5 Special messages e g warm up period 6 Pointer for parameter i e aim that changes on data entry 7 Aim set point or target in co...

Page 49: ...er display 4 3 Changing the Units In Full Setup Mode any set of aeronautical or pressure units can be selected 4 3 1 Changing the Measurement Units a Press the SETUP key b Select UNITS c Use NEXT and PREV keys to select the required units d Select SAVE to accept e Press CLEAR QUIT repeatedly to return to the main pressure display Note 1 In Minimum Setup Mode only the default aeronautical and press...

Page 50: ...turn to Leak Measure mode b Press RATE TIMER F3 Wait 05 00 Time 01 00 c Different wait and time periods can be selected by pressing F1 or F2 d Wait until rate timer has completed and the results displayed e Check rate of climb is less than 100 ft min and rate of airspeed CAS is less than 1 kts f Press LEAK MEASURE CONTROL to return to Control mode g Press GROUND F1 Go to Ground h Wait until for th...

Page 51: ...nge of speed ii 6 0 0 ENTER to set the rate iii SPEED Qc to select airspeed iv 3 0 0 ENTER to set an airspeed of 300 kts airspeed CAS now starts increasing v ROC Ps RATE to select rate of climb vi 6 000 ENTER to set the rate of climb vii ALT Ps to select the altitude viii 5 000 ENTER to set altitude Alt altitude now starts increasing ix SPEED Qc to view altitude and airspeed together Note When alt...

Page 52: ...another unsuccessful leak test i Disconnect both hoses check the condition of the o rings on the Ps and Pt connectors Replace if necessary as detailed in the Section 5 4 2 Replacing the Output Connector O ring on page 51 Then firmly replace the blanking caps ii Press CLEAR QUIT and repeat the leak test procedure iii After a successful leak test without hoses connected iv Replace or repair the faul...

Page 53: ...he display shows the name of the associated parameter e g If a Mach limit is exceeded when entering an airspeed value the display shows Mach and the equivalent maximum and minimum limits as airspeed values Similarly if an ARINC 565 limit is exceeded when entering a value and ARINC limits are enabled the display shows ARINC Select the limits in use a Press SETUP b Select LIMITS c Use NEXT or PREV t...

Page 54: ...alent to IAS for testing purposes The airspeed parameter may be changed to True Airspeed TAS as follows a Press SETUP then SPEED b Select CAS TAS c Select TAS d Press QUIT CLEAR repeatedly to exit setup e Press SPEED The display now shows the airspeed parameter as TAS Note Airspeed parameter type can only be changed in Full Setup mode Rate of change of airspeed will still be shown as Rate CAS Pito...

Page 55: ...ailed in Full Setup see Section 7 3 4 SETUP OSC on page 84 The above method steps a to g can be applied for the other parameters 4 9 Engine Pressure Ratio EPR The ADTS 405 Mk2 may be used to check EPR sensors and indicators Use Ps for INLET pressure and Pt for OUTLET pressure To carry out an EPR check the display must be showing pressure units e g mbar or in Hg 4 9 1 Example EPR Test To enter an E...

Page 56: ...hile Going to Ground If required new rates of change can be entered while going to ground a To change the ROC or static rate press ROC Ps RATE and enter the new value b To change the airspeed or Qc rate press SPEED Qc then RATE and enter the new value 4 10 3 Resuming Testing after Going to Ground When the airspeed reaches zero and the Ps channel pressure nears ground the system re measures atmosph...

Page 57: ...ry and will be lost when the system is switched off The range of options allowed in setup is determined by the setup mode See Appendix A 1 and Appendix A 2 for the SETUP menu hierarchy Example a Press SETUP and the display shows b Pressing a function key F1 to F4 enters the setup menu c When in setup pressing a key ALT Ps in this example enters a menu or setting that applies to the parameter 4 11 ...

Page 58: ...N in turn ENTER is not required as each digit is entered an asterisk appears If an incorrect PIN is entered the complete PIN is requested again b When the correct PIN is entered the CONFIG menu appears Note The PIN may be changed using CONFIG 000 c To use the configuration menu press the appropriate function key to select the required menu item To configure a parameter key enter configuration menu...

Page 59: ... with a network interface using a UTP network cable The network interface should be configured with an IP address on the same subnet Example If the ADTS has the default IP addresses then the host network address should be configured as 192 168 2 1 255 255 255 The method for doing this may vary but the following example screens show the method under Windows 7 It is suggested to take careful note of...

Page 60: ...d in Section 4 11 and Section 4 12 An SSH server is available on each IP address for general purpose file access The factory default user name and password for accessing the server is It is strongly advised that the default password be changed as part of the initial end user customization 4 13 2 Changing the Default Access Password Configure the network interface with an IP address on the same sub...

Page 61: ...d passwd followed by the RETURN key f Follow the screen prompts by Enter the existing password followed by the new password and further confirmation entry The results of a successful change should look like the PuTTY window in Figure 4 10 Figure 4 10 Changing the Default Password Close the PuTTY window and confirm that a new connection can still be gained using the new password 4 13 3 Access ADTS ...

Page 62: ...ogin using the following credentials and save under a suitable name for future connections b Connect to the unit by pressing Login Table 4 3 Win SCP Client Credentials Parameter Value Notes Host Name 192 168 2 2 The IP address of the ADTS supervisor Ethernet adaptor Port 22 User name adts Password druk Or new password if changed Private key leave blank ...

Page 63: ... the PC left panes by drag and drop to the ETP directory They will then become available for stand alone use under the front panel ETP key Unwanted programs may be deleted from the ETP directory as required Similarly any reports previously generated using the PRINT key will be available under the SPOOL directory This may be transfer to the PC window for archive or hard copy print as required d The...

Page 64: ...EEE 488 facility will be available from power up of the ADTS 405 Mk2 The setting is held in non volatile memory 4 14 2 IEEE 488 Connector The IEEE 488 connector is located behind the optional communications module cover plate The connector s pin out is detailed in Table 4 4 INFORMATION The cover plate for communications option must always be fitted when the equipment is used outdoors or in an envi...

Page 65: ...n incorrect bit combination such as all zeros the display shows ENCODER ERROR in the place of the decoded value 20 GNDb 21 GNDb 22 GNDb 23 GNDb 24 GNDb a Chassis connection b 0V return for signals not chassis 1 Controlled or measured parameter 2 Aim set point or target in control mode or Leak Measure when the pressure controller is off 3 Measured value 4 Pointer for parameter i e aim that changes ...

Page 67: ...urther information required to identify the item Note Equivalent substitutes can be used Table 5 1 Maintenance Chart Task Code Period Inspect A Daily before use Inspect B Weekly Test C Before use Test D Daily before use Calibrate E Every 12 monthsa a Periodicity may change depending on usage and environment refer to the Engineering Authority Replace F As detailed in fault finding or when detailed ...

Page 68: ...ilityTest detailed in Section 6 4 Standard Serviceability Test on page 58 e Normal calibration period is 12 months When calibration is due the unit should be withdrawn from service and returned to depot or calibration facility 1 The date of calibration is stored in the unit and displayed in the power up sequence and on a label on the front panel 2 Do not use a unit with out of date calibration 3 E...

Page 69: ... small groove at the top of the connector b Fit a new o ring in the small groove at the top of the connector c Check the o ring is located in the groove and not damaged after fitting Note Damage to this o ring causes leaks Figure 5 1 Output Connector O ring Seal 5 4 3 Fuse Replacement Replace the fuse when detailed in Section 6 6 Fault Diagnosis on page 60 INFORMATION Absolute cleanliness of the w...

Page 70: ...cuit For fuse specification see Table 8 2 on page 102 Figure 5 2 ADTS 405F Mk2 AC Fuse Positioning a Set the power switch to OFF b Isolate the power supply to the instrument and disconnect the power supply connector 1 c Remove the fuse holders 2 from the front panel and replace the fuse cartridges 3 d Refit the fuse holders 2 in the front panel e Connect the power supply connector and switch on th...

Page 71: ... fuse specification see Table 8 2 on page 102 Figure 5 3 ADTS 405F Mk2 DC Fuse Positioning a Set the power switch to OFF b Isolate the power supply to the instrument and disconnect the power supply connector 1 c Remove the fuse holders 2 from the front panel and replace the fuse cartridges 3 d Refit the fuse holders 2 in the front panel e Connect the power supply connector and switch on the power ...

Page 72: ...ning a Set the power switch to OFF b Isolate the power supply to the instrument and disconnect the IEC power supply connector c Pull the capped lid of the fuse carrier 2 on the power supply input socket assembly d Replace the fuse cartridges 3 e Refit the fuse carrier 2 flush in the power supply inlet socket assembly f Refit and reconnect rack mounted units g Switch on the power supply and set the...

Page 73: ...urn g Measure also the resistance between individual pairs of pins i e 1 2 1 3 1 4 1 5 1 6 2 3 2 4 2 5 2 6 3 4 3 5 3 6 4 5 4 6 and 5 6 In all cases the resistance must exceed 10 MΩ 5 5 2 AC Power Regional Line Plug Cables Note For parts AA405F 1 to AA405F 16 a Prepare to measure continuity using the DMM item 1 Table 5 3 set to the applicable resistance range b Measure the continuity between corres...

Page 74: ...value is the expected maximum value for the 5 m 16 ft cable length supplied c Prepare to measure insulation using the Insulation tester item 2 Table 5 3 set to the 500 V range This test will be most practically performed at the open end of the cable d Measure the insulation resistance between Gray 28 V and Green Protective Ground e Measure the insulation resistance between White 0 V and Green Prot...

Page 75: ...aining additional information record the whole error code check that the error code is complete and listed in the table before returning the unit to the repair depot In the event of a fault the built in self test and diagnostic system displays an error message and error code A unit displaying an error should be returned to the repair depot See Appendix B 1 Error Messages on page 117 for a list of ...

Page 76: ...nit and if necessary connect the hand terminal b Make sure that the blanking caps are fitted to the Ps and Pt front panel outputs c Check power indicator is on d Set the front panel switch to OPERATE e Set the front panel switch for the pump unit to PUMP ON and check that the pump power indicator lights f Check the display shows the first stage power up message as below where xx xx is the version ...

Page 77: ...es place regularly The display shows ZERO and the state of the valves on the mimic panel change for approximately 6 seconds Commands may still be entered while auto zero takes place 6 4 2 Pump Unit ADTS 405F Mk2 a Set the front panel switch for the pump unit to PUMP ON and check that the pump power indicator lights b Press LEAK MEASURE CONTROL to go to control mode c Enter an altitude aim of 5000 ...

Page 78: ...ASHING RED ORANGE GREEN OFF RED FLASHING RED ORANGE STATUS LIGHT HAND TERMINAL FITTED HAND TERMINAL DISPLAY POWER UP MESSAGE POWER UP MESSAGE HAND TERMINAL BACKLIGHT ON FRONT PANEL DISPLAY POWER UP MESSAGE OFF RED FLASHING RED ORANGE HAND TERMINAL FITTED STATUS LIGHT GREEN OFF RED FLASHING RED ORANGE FROM NOW ON IF ANY ERROR OCCURS THE SYSTEM LOGS THE OCCURRENCE AND DISPLAYS AN ERROR MESSAGE REFER...

Page 79: ...y fault Use an available hand terminal Record fault and return ADTS 405 Mk2 to depot for repair F5 No hand terminal display status light green Hand terminal key illumination on Hand terminal fault cable OK Replace hand terminal Record fault and return hand terminal to depot for repair F6 No hand terminal display status light green Hand terminal key illumination not on Hand terminal Replace hand te...

Page 80: ...Remove the source of pressure and vent Ps and Pt to atmosphere caps off b Re power the ADTS 405 Mk2 During the power up screen c Press F1 and F4 simultaneously The ADTS 405 Mk2 enters maintenance mode Note The system may prompt for a PIN This is not the CONFIG PIN but the Calibration PIN If this Calibration PIN is enabled and not entered the system will not execute the following procedure d In mai...

Page 81: ...nge the units to mbar as follows a Press SETUP then select UNITS b Repeatedly select NEXT until the display shows mbar c Select SAVE and then press CLEAR QUIT twice and the display now shows Ps and Pt in units of mbar 6 8 2 Pressure Leak Check This check confirms that the unit does not leak under positive pressure conditions a Press LEAK MEASURE CONTROL to enter control mode The display shows Aim ...

Page 82: ...wn followed by the Timing time g At the end of the Timing period press ROC Ps RATE to display the measured rate of change of Ps T is shown after the value indicating a timed average h Check that the Ps Qc and Pt rates are less than or equal to 0 5 mbar min If the leak rate is not achieved allow further thermal stabilization time and re test by pressing RATE TIMER and selecting WAIT 05 00 TIME 01 0...

Page 83: ...y shows Zero in place of the airspeed aim value The time to auto zero should be less than 1 minute from achieving the aim value f Wait for a minimum of 20 seconds after auto zero before proceeding g Observe the measured values of Ps and Qc on the display for 1 minute h Check that the displayed value of Ps remains within 0 068 mbar i Check that the displayed value of Qc remains within 0 068 mbar No...

Page 84: ...he following tests should only be done if the serviceability of an option facility is suspected or when an error occurs Figure 6 2 External Communication Ports 1 Loosen the eight captive screws to remove the cover plate from the communications connector panel 2 ADTS 405 Mk2 front panel 3 Details of communications connector panel that is behind the cover plate 1 1 8 2 3 ...

Page 85: ...el should use this facility the test procedure must be authorized by the appropriate engineering authority If the display does not show that SCPI is selected follow the procedure in Section 4 14 1 Enabling the IEEE 488 Option on page 45 then carry out the following procedure a Press SCPI b Press CLEAR QUIT DEVICE ADDRESS c Check the address displayed is 1 d If not press 1 on the numeric keypad and...

Page 86: ...the IEEE 488 cable if unserviceable replace the cable ii Do steps a to g again If the test fails again return the ADTS 405 Mk2 to the repair depot 6 8 7 Altimeter Encoder To enable and disable this Altimeter Encoder facility access the configuration menu When enabled this facility will be available from power up of the ADTS 405 Mk2 with the settings held in non volatile memory If the altimeter enc...

Page 87: ...in Function Cable Color AAU 32 Connector Pin 1 C4 LSB Brown B 3 C2 Red C 5 C1 Orange D 7 B4 Yellow E 9 B2 Green F 11 B1 Blue G 13 A4 Violet H 22 A2 White J 2 A1 Gray K 4 D4 Black L n c D2 MSB Turquoisea a The D2 data line turquoise cable is not defined for the AAU 32 it is for above 62 000 ft and not connected n c 8 Common 0V signal Pink A 10 Common 0V power Yellow Red b M 14 Vibrator 24 V Red Blu...

Page 89: ...escription of each key function including references to associated functions The available keys are F1 F4 ALT Ps SPEED Qc MACH Pt EPR ROC Ps RATE RATE TIMER HOLD RATE LEAK MEASURE CONTROL GROUND PORT REMOTE PRINT EXECUTE TEST PROGRAM HELP SETUP nudge up nudge down 0 to 9 000 CLEAR QUIT ENTER decimal point Double key presses give ABORT CLEAR ENTER CONFIGURATION F1 SETUP ...

Page 90: ...d measure mode 7 2 3 SPEED Qc 1 In aeronautical units kts km h this key selects an airspeed CAS or TAS display In pressure units mbar inHg etc this key selects dynamic pressure and the display shows Qc 2 The airspeed can be displayed and entered as either Calibrated Airspeed CAS Vc or True Airspeed TAS Vt Note For testing purposes Calibrated Airspeed equates to Indicated Airspeed IAS 3 The Pt temp...

Page 91: ...while the TAS and Mach values remain unchanged 4 If the Ps aim is changed after the entry of Qc then the Pt aim value changes while the Qc remains unchanged 5 If the Ps aim is changed after the entry of Pt then the Qc aim value changes while the Pt remains unchanged 6 Before entering a new Mach or Pt aim set the rate of change of speed using the SPEED Qc key 7 Press the RATE key 8 In Control Mode ...

Page 92: ...the WAIT or TIME period counting down After timing the timed average value identified by a T directly to the right of the value replaces the instantaneous rate value In measure mode the display changes to show the timed rate of all associated parameters on the same screen Pressing one of the set point keys e g ALT ROC SPEED etc or CLEAR QUIT exits from this screen 3 At any time during rate timing ...

Page 93: ... required rates e Press HOLD again to release hold f HOLD is automatically released when entering Measure Mode 7 2 9 RATE 1 In aeronautical units kts km h this key selects a rate of change of airspeed Rate CAS display The following rates are available in aeronautical units 2 In pressure units mbar inHg etc this key selects a rate of change of pressure Rate Qc Rate Pt or Rate EPR display The actual...

Page 94: ...ressure No significant pressure transients are produced when regaining control 4 In CONTROL mode the display shows Aim value 5 Two safety systems are built in to protect the aircraft systems during leak testing These are Auto Leak recovery and Auto Limit recovery Auto Leak recovery automatically regains control if the leak rate exceeds the currently set limits on either channel 6 Auto Leak recover...

Page 95: ...The display shows the message Safe At Ground the ground and zero valves remain open so that the aircraft system permanently vents to atmosphere No commands can be entered when these two messages are displayed 5 Press CLEAR QUIT to continue with normal operation The ground and zero valves then automatically close 7 2 13 DISPLAY QFE 1 When DISPLAY QFE is selected the local atmospheric pressure recor...

Page 96: ... character A to Z press the ALPHA key and use the or nudge keys to change to the required character To enter another alphabetic character press the ALPHA key again Press BACK to delete the last character 2 Up to nine user readings can be entered sequentially The display prompts for the next user reading each time one is entered When no further readings are required press CLEAR QUIT Example print o...

Page 97: ...re described in Section 4 13 3 Access ADTS Files on page 43 7 2 18 3 Deleting Program Files If a test program within an ADTS 405 Mk2 is no longer required then it may be deleted To delete a test program proceed as follows a Enter configuration CONFIG by pressing and holding F1 and pressing SETUP b At the first menu level of configuration press the EXECUTE TEST PROGRAM key then F2 The display then ...

Page 98: ...this procedure using the until the switch returns to its original condition refer to Section 4 8 Airspeed Switch Test on page 36 for an example Holding the nudge function automatically repeats the function e Record the pressure reading shown on the display Note 1 Holding down one of the keys automatically repeats the function Note 2 The nudge value can be used for large increments e g 100 kts or 5...

Page 99: ...generally to the previous display 3 For those displays containing a SAVE option changes made before pressing CLEAR QUIT are ignored For all other displays changes are saved when CLEAR QUIT is pressed 4 When warning messages are displayed pressing CLEAR QUIT removes the message 7 2 24 ENTER The ENTER key completes numeric entry 7 2 25 CLEAR ENTER ABORT Pressing CLEAR QUIT and ENTER together restart...

Page 100: ...its at power up with a particular set of limits that must not be changed Attempting to change a locked parameter causes the display to show a warning message 2 Pressing the SETUP key makes the setup functions available Pressing the function keys selects the setup menus using the appropriate function key selects the required menu choice To setup a parameter key press SETUP then press the required p...

Page 101: ...h set of limits is identified by its aircraft name Note The ADTS 405 Mk2 when delivered contains Standard and Civil limits to set and store Max limits for the first time enter configuration The Max limits depend on the range of the pitot channel either 850 or 1000 kts see Section 1 3 Operating Limits on page 2 1 Use NEXT or PREV to step through the aircraft names select SEL and press QUIT when the...

Page 102: ...AMPL FREQ and enter the required amplitude and frequency c Select START to start oscillation d Select STOP to stop oscillation at the end of a half cycle e Select FREEZE to stop oscillation immediately 7 3 5 SETUP MORE CONTROL Ps Pt DUAL 1 Dual channel is the normal mode of operation where both Ps static and Pt pitot channels are connected to the unit or aircraft system under test 2 To test instru...

Page 103: ... sequence Table 7 3 Aeronautical Units Dual Display 1st Key Press 2nd Key Press Upper Display Lower Display ALT SPEED ALT CAS or TAS ALT MACH ALT MACH Any key ROC ALT ROC SPEED RATE CAS or TAS RATE CAS MACHa a The Mach parameter changes on numeric entry RATE MACH RATE MACH SPEED MACH MACH CAS TAS SPEED ALT ALT SPEED MACH ALT ALT MACH MACH SPEED MACH SPEED Table 7 4 Pressure Units Dual Display 1st ...

Page 104: ...r further details If an option that is not fitted is selected the display shows the error message Option Hardware not fitted Refer to the option user manual 7 3 8 SETUP MORE CLOSE OUTPUT VALVES This function closes the Ps and Pt valves to enable leak checking of the internal pneumatics of the ADTS 405 Mk2 with the aircraft system isolated but still connected All the normal functions of the ADTS 40...

Page 105: ...ust to the left of the Status LED assumes front panel is vertical The ADTS 405F Mk2 altitude reference level is marked on the side product label of the flight line case assumes front panel is horizontal If the ADTS is below the aircraft system enter the correction value as a positive number See Section 2 4 Positioning of the ADTS on page 10 a Enter the height difference between the aircraft system...

Page 106: ...its To change the limit enter a numeric value or select as follows a Select OFF to disable the Mach limit b Select ON to enable the Mach limit c Select DEFAULT to restore the Mach limit from the aircraft limits in use 7 3 16 SETUP RATE TIMER This function allows the Wait Time values to be set for F1 F2 and F3 of the RATE TIMER function To change the times a Select the function to be changed F1 F2 ...

Page 107: ...up the port option If an option that is not fitted is selected the display shows the error message Option Hardware not fitted Refer to the Line Switching Unit User Manual 7 3 22 SETUP PRINT DATE TIME This function allows the system time and date to be set The time and date is maintained by a battery backed clock when the ADTS 405 Mk2 is switched off a Use TIME or DATE to select between time or dat...

Page 108: ... Pt Qc RATE Qc EPR RATE EPR 5 The nudge value can be used for large increments e g 100 kts or 5 000 ft to step through the cardinal points of a test 7 3 26 MINIMUM SETUP Minimum setup allows access to a limited number of setup functions Any parameter changed under setup returns to the default settings at power down The CONFIG mode may be used to change the default settings so that the ADTS 405 Mk2...

Page 109: ...ax Qc Min Qc Max Rate Ps Max Rate Qc ARINC limits on or off Altitude correction value The set of limits used at power up default can be selected using CONFIG LIMITS DEFAULT AIRCRAFT The default aircraft set of limits can be locked using CONFIG LIMITS LOCK AIRCRAFT so that an operator cannot change the limits If the selected set of limits result in the measured pressure values being outside the lim...

Page 110: ...he correct PIN is entered the CONFIG menu appears c The PIN may be changed using CONFIG 000 d To use the configuration menu press the appropriate function key to select the required menu item To configure a parameter key enter configuration menu then press the required parameter key Each parameter key configuration provides changes to the normal user mode function and to the settings available in ...

Page 111: ... when all required changes have been made and select YES to save changes The ADTS 405 Mk2 when delivered contains Standard and Civil limits to set and store Max limits for the first time enter configuration The Max limits depend on the range of the pitot channel either 850 or 1000 kts see Section 1 3 Operating Limits on page 2 The system s defined STANDARD CIVIL and MAX limit sets cannot be redefi...

Page 112: ...are the maximum rate of change for altitude and airspeed and only apply in aeronautical units 7 4 9 MIN Ps MAX Ps MIN Qc MAX Qc These are the fundamental pressure unit limits 7 4 10 MAX RATE Ps MAX RATE Qc These limits are the maximum rate of change for Ps and Qc and only apply in pressure units 7 4 11 ALTITUDE CORRECTION The altitude correction value for a specific aircraft may be entered as well...

Page 113: ... screen If changes have been made the display shows a request for confirmation before saving the changes If the system detects any errors e g duplicate aircraft names values out of range or editing system defined limits the display changes to the edit screen for the error to be corrected 7 4 14 CONFIG LIMITS EDIT LIMITS MAX LIMITS This function makes a set of maximum limits a set of MAX limits can...

Page 114: ...ges to the default limits If lock is ON no changes to the power up default aircraft limits can be made from setup 7 4 18 CONFIG LIMITS DEFAULT AIRCRAFT This function selects the set of limits used at power up Use NEXT or PREV to display the name of the required limits Select SEL 7 4 19 CONFIG MORE CONTROL CONTROL MODE CONFIG equivalent of SETUP function 7 4 20 CONFIG MORE DISPLAY OPTIONS DISPLAY T...

Page 115: ...10 LEAK MEASURE CONTROL on page 76 for details 7 4 32 CONFIG LEAK MEASURE AUTO LEAK LOCK Prevents changes to AUTO LEAK setting in SETUP 7 4 33 CONFIG LEAK MEASURE AUTO LIMIT ON OFF CONFIG equivalent of SETUP function see Section 7 2 10 LEAK MEASURE CONTROL on page 76 for details 7 4 34 CONFIG LEAK MEASURE AUTO LIMIT LOCK Prevents changes to AUTO LIMIT setting in SETUP Table 7 7 Setup Modes Mode De...

Page 116: ...ram on power up See the Test Program Manager User Manual for further details 7 4 39 CONFIG ETP ERASE PROGRAMS Removes a down loaded test program from non volatile memory See the Test Program Manager User Manual for further details 7 4 40 CONFIG ETP RESULT 1 Configures the PRINT SAVE mode as in setup mode 2 Selects and deletes a result file stored in the ADTS 405 Mk2 7 4 41 CONFIG NUDGE CONFIG equi...

Page 117: ...ON 2017 General Electric Company All Rights Reserved ADTS 405 R F Mk2 Instruction Manual English 99 Note Access to maintenance functions may also be PIN protected This PIN number is not the same as the CONFIG PIN ...

Page 119: ...50 60 Hz 115 V 400 Hz Power 400 VA Installation Category II Fuse T5AH250V DC Power Supply Supply range 16 to 30 V Power 400 VA Fuse Not user serviceable Operating Environment Indoor use Operating Altitude Up to 4 570 metres 15 000 ft Operating Temperature 20 C to 50 C 4 F to 122 F Storage and Shipping Temperature 51 C to 70 C 60 F to 158 F Ingress Protection IP23 Operating Humidity 0 to 95 RH non ...

Page 120: ...115 V 400 Hz Power 500 VA Installation Category II Fuse T5AH250V DC Power Supply Supply range 16 to 30 V Power 500 VA Fuse T20AH250V left T32AH250V right Operating Environment Indoor and outdoor use Operating Altitude Up to 4 570 metres 15 000 ft Operating Temperature Standard Range 20 C to 50 C 4 F to 122 F Extended Range 40 C to 55 C 40 F to 131 F Storage and Shipping Temperature 51 C to 70 C 60...

Page 121: ... Mk2 is supplied in one of two full scale ranges 850 or 1000 kts for measurement and control of the pitot pressure channel The following operating parameters are based on a 1000 kts capability test systems Variations for 850 kts test systems are shown where appropriate in brackets For both full scale ranges limits are set predefined tabular limits known as STANDARD CIVIL and MAX these can be selec...

Page 122: ...non linearity hysteresis and repeatability over full temperature range 12 months drift and calibration standard uncertainty 3 at 0 7 at 30 000 29 at 60 000 1 of value 0 5 at 50c 0 07 at 550 0 05 at 1000 c The accuracy figures stated assume that the auto zero function is enabled Better than 0 005 5 of value Resolution 1 1 0 1 0 001 0 1 Table 8 4 Static and Pitot Performance Expressed in Pressure Un...

Page 123: ...ers in either aeronautical or pressure units Table 8 5 Qc Rate Qc and EPR Performance Expressed in Pressure Units Parameter Differential Qc 1000 kts Differential Qc 850 kts Rate Qc EPR Units mbar diff mbar diff mbar min Maximum Rangea a Pressures below 35 mbar absolute and the peak rates of change are available but subject to the use of a suitable vacuum pump 1352 to 3377 1352 to 2700 10 000 0 1 t...

Page 124: ...lace within a 400 millisecond period 8 4 4 Dynamic Testing The ADTS 405 Mk2 can generate sinusoidal variations of either the Ps or Pt or both channels Frequency and amplitude of the required oscillation can be programmed external volumes limit the achievable results Maximum drift from the mean value during dynamic testing should be no more than twice that specified for steady state testing 8 4 5 C...

Page 125: ...ple key press on keypad display Simultaneous key press on keypad display In this example press and hold the F1 key and press the SETUP key to enter the CONFIG menu NEXT Item in soft menu keys labeled F1 to F4 SINGLE DOUBLE Sequence of parameters selected by NEXT key aircraft1 aircraft2 Sequence of names selected by NEXT key data entry Enter number from keypad SETUP F1 SETUP ...

Page 126: ...VE I O Setup ENET SUPER Fixed IP ADDR MASK BCST Show active ENET COMMS Show active Options Close O P Valves System Self Test Select single dual or triple display SINGLE DUAL TRIPLE ENCODER As NEXT but in reverse order Save display type MsrƉkyvi Oxlivrix Supervisor node Ethernet parameters DHCP option not available see CONFIG menu ixyt Ɖ ih SZ ehhviww IP address Subnet mask Broadcast address MsrƉvq...

Page 127: ...ing Unit user manual data entry ON OFF CAS TAS Pt Temperature data entry DEFAULT OFF ON data entry Wait Time on F1 TIME data entry WAIT data entry Wait Time on F2 Wait Time on F3 ON OFF Auto Leak Auto Limit ON OFF ON OFF data entry Enter pitot temperature Mach limit from current limits Removes Mach limit Enables Mach limit Enter new Mach limit Leak test WAIT and TIME for F1 preset See Wait Time on...

Page 128: ...he nudge value for When in aeronautical units Altitude CAS TAS Mach ROC Rate CAS Rt Mach When in pressure units Ps Pt Qc EPR Rate Ps Rate Pt Rate Qc Rate EPR As NEXT but in reverse order See SETUP S for menu hierarchy EXECUTE TEST PROGRAM 4Zvmrx Ɖpi5 Print Save PRN SAV Print results data ezi viwypxw hexe xs Ɖpi PRN PREV NEXT Choose destination for results data Set the ADTS date and time Zvmrx viwy...

Page 129: ... PREV SEL More Select units type Select aeronautical units Select pressure units Select set of limits aircraft 1 aircraft 2 As NEXT but in reverse order Select displayed limit set Control Ps Selects Ps only Pt only or dual channel control Pt DUAL SETUP Altitude correction value data entry SETUP ALT Ps See Line Switching Unit user manual PORT HELP Help on SETUP menu Enters the SETUP menu Enters the...

Page 130: ...xli hijeypx xiqtivexyvi yrmxw Clear Limits NEXT PREV SEL aircraft 1 aircraft 2 As NEXT but in reverse order Mpiev xli wipigxih pmqmxw YES NO MsrƉvq hipixi NEXT PREV SEL Edit existing Mlerki pmqmx zepyiw Mlerki i mwxmrk pmqmx zepyiw NEXT xit xlvsykl ezempefpi pmqmx mxiqw Xeqi We Kpxmxyhi Wmr Kpxmxyhi We MK Wmr MK We Wegl We YM We exi MK We Zw Wmr Zw We g Wmr g We exi Zw We exi g K SXM pmqmxw Kpx Ms...

Page 131: ... ixyt Ɖ ih SZ ehhviww SZ ehhviww yfrix qewo Lvsehgewx ehhviww MsrƉvq egxmzi SZ wixxmrkw Msqqyrmgexmsrw rshi Oxlivrix teveqixivw ii 4OXO _ZO 5 jsv qiry lmivevgl ii stxmsr qeryep Pt DUAL Lock aircraft ON OFF Zvizirxw glerkiw xs emvgvejx pmqmxw yvr sr xs qeoi O _Z qiry pmqmxw viehsrp Default aircraft Zvizirxw glerkiw xs emvgvejx pmqmxw NEXT PREV SEL 0emvgvejx emvgvejx 1 Kw 4XOb 5 fyx mr vizivwi svhiv...

Page 132: ...anual ON OFF CAS TAS Pt temperature data entry Wait time on F1 TIME data entry WAIT data entry Wait time on F2 Wait time on F3 ON OFF 4Kyxs pieo sr sƇ5 4Kyxs pmqmx sr sƇ5 ON OFF ON OFF data entry Enter pitot temperature Leak test WAIT and TIME for F1 preset See Wait Time on F1 for menu hierachy Change duration time entry Change wait time entry Select between calibrated or true airspeed Station alt...

Page 133: ... SEL Select no test program at power up Select the desired test program Results 4Zvmrx Ɖpi5 Print Save PRN SAV Print results data ezi viwypxw hexe xs Ɖpi PRN PREV NEXT Choose destination for results data Zvmrx viwypxw Ɖpi stxmsrw xit xlvsykl ezempefpi viwypxw Ɖpiw As NEXT but in reverse order Zvmrx xli wipigxih viwypxw Ɖpi HELP Help on CONFIG menu NEXT data entry PREV Enter nudge increment e g 2 f...

Page 135: ...INTERNAL RAM ERROR 603 ERROR WRITING TO EEPROM 701 Ps SELF TEST ERROR 702 Pt SELF TEST ERROR 703 Ps SELF TEST TIME OUT ERROR 704 Pt SELF TEST TIME OUT ERROR 710 Ps CONTROLLER ERROR 711 Ps CONTROLLER ERROR 712 Ps CONTROLLER ERROR 713 Ps CONTROLLER ERROR 714 Ps CONTROLLER ERROR 717 Ps CONTROLLER ERROR 720 Pt CONTROLLER ERROR 721 Pt CONTROLLER ERROR 722 Pt CONTROLLER ERROR 723 Pt CONTROLLER ERROR 724...

Page 136: ...t CONTROL again If fails again refer to main fault finding chart in the service manual 212 Ps PRESSURE FAIL The Ps controller has detected loss of supply pressure and automatically switched all channels to measure mode This can occur at very high rates of pressure change in large volume systems if the pumps cannot produce enough pressure Restore pressure supply BEFORE going to control mode again R...

Page 137: ...for aircraft safety as leak rates too high Correct leak and retest 302 OUTSIDE LIMITS REGAINING CONTROL Controlmodeautomatically regained for aircraft safety as the measures values have drifted outside the operating limits due to leaks Correct leak and retest If leak Ps ensure that normal Qc pressure is applied e g 200 kts to avoid negative airspeed 303 ZERO OFFSET TOO LARGE The zero offset measur...

Page 138: ...truction Manual English 2017 General Electric Company All Rights Reserved 309 CANNOT CONTROL Failed pump test Check system limits 310 PUMP TEST FAILED Pump not achieving limits Set lower limits Table B 2 Warning Messages Number Message Probable Cause Action ...

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