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Operators and Maintenance Manual 

 

Measuring module

 

EMS DAQ R02.01

 

Page 

5/18

 

 

Copyright: 

Auto & Aero Technologies Sp. z o.o. 

Mazowiecka 10/5, 20-723 Lublin, Poland  

 email: info@aatech.pl 

  

www.aatech.pl 

 

 

 

Fig. 1. EMS DAQ R02.01 module (complete casing and casing with lid removed)

 

 

1.  General information 

This manual contains binding information, guidelines and warnings for safe 
handling and maintenance of this particular instrument before installation, 
during  installation  and  in  its  operating  phase.  This  document  does  not 
contain rules and guidelines on operation of aircraft instruments at large. 

Read  the  manual  thoroughly  before  turning  on  the  instrument  and 
precisely  follow  the  instructions  to  install  and  configure  it.  This  manual 
does  not  replace  instructions  on  installation,  maintenance  and  operation 
of  this  device  in  a  particular  airframe  -  these  are  to  be  prepared  by  the 
user. Instructing the pilots and maintenance personnel on operation of the 
instrument is also the responsibility of the user. 

Operation of this device is the sole responsibility of the pilot in command 
(PIC)  of  the  aircraft.  This  person  must  be  proficient  and  carry  a valid  and 

relevant  pilot’s license.  This  person has to  make themselv

es familiar  with 

the  operation  of  this  module  and  the  effect  of  any  possible  failure  or 
malfunction.  Under  no  circumstances  does  the  manufacturer  condone 
usage of this instrument for IFR flights. 

This  manual  defines  the  scope  of  maintenance  measures  the  user  is 
authorised  to conduct on their own. Any repairs or  modifications outside 
this scope conducted by the user or contracted to a third party, as well as 

Summary of Contents for EMS DAQ R02.01

Page 1: ...asuring module EMS DAQ R02 01 Page 1 18 Copyright Auto Aero Technologies Sp z o o Mazowiecka 10 5 20 723 Lublin Poland email info aatech pl www aatech pl Operators and Maintenance Manual Measuring mod...

Page 2: ...ort and storage 6 3 Installation 6 3 1 Environmental specifications 6 3 2 Dimensions 7 3 3 Mounting 7 3 4 Power and wiring 7 4 Operation and maintenance 10 4 1 Measured signals 10 4 2 Signal analysis...

Page 3: ...an element of the Integrated Avionics System that measures the following engine operation parameters a Engine speed b Rotor speed c Inlet air pressure d Inlet air temperature e Oil pressure f Oil temp...

Page 4: ...3 Inlet air pressure Bosch 0 281 002 976 4 Oil pressure BRP 456180 1 5 Oil temperature BRP TEMPERATURE SENSOR 965531 1 6 Cylinder head temperature BRP TEMPERATURE SENSOR 965531 1 2 sensors 7 Exhaust g...

Page 5: ...e it This manual does not replace instructions on installation maintenance and operation of this device in a particular airframe these are to be prepared by the user Instructing the pilots and mainten...

Page 6: ...e and packed in a cardboard box together with the warranty card 2 The display must be stored and transported assuring that o the ambient temperature stays in the range of 10 40 C o the ambient relativ...

Page 7: ...EMS DAQ R02 01 module outline drawing 3 3 Mounting The EMS DAQ R02 01 Module should be installed vertically using mounting holes shown in Figure 2 The module should be located in a part of the engine...

Page 8: ...n Figure 3 The power supply requires 0 75 mm2 wires Sensor connection requires 0 5 mm2 wires Thermocouple wires should be attached directly to the module s connector Data bus RS0 RS1 RS2 requires twis...

Page 9: ...Maintenance Manual Measuring module EMS DAQ R02 01 Page 9 18 Copyright Auto Aero Technologies Sp z o o Mazowiecka 10 5 20 723 Lublin Poland email info aatech pl www aatech pl Fig 1 EMS DAQ R02 01 Modu...

Page 10: ...b 2 Signals processed by EMS DAQ R02 01 Module No Parameter Measurement range Accuracy 1 Engine speed 0 6500 rpm 10 rpm 2 Rotor speed 0 500 rpm 1 rpm 3 Inlet air temperature 0 3 4 bar abs 0 1 bar 4 Oi...

Page 11: ...hold crossings recorded by EMS DAQ R02 01 Module No Signal Threshold levels 1 Engine speed 5500 rpm if present for more than 5 min 2 Engine speed 5800 rpm 3 Rotor speed 450 rpm 4 Inlet air pressure 46...

Page 12: ...on of a parameter assuming values from a specific range The data are recorded separately for each parameter and for each of four value ranges Information on the statistics is downloadable by means of...

Page 13: ...from 900 to 925 above 925 11 Cylinder head temperature sensor 2 C from 850 to 875 from 875 to 900 from 900 to 925 above 925 12 Linear acceleration g 1 from 2 to 4 from 4 to 8 from 8 to 12 above 12 1 i...

Page 14: ...display data 2 After 100 hours of flight a Check the instrument s electric connections Remove the lid of the monitor casing Check if wires sit firmly in screw connection terminal blocks Check for wire...

Page 15: ...onnection ensure that your power supply is capable of supplying at least 8 volts and no more than 30 V data bus connection RS0 Fig 3 Indication of no connection to measurement module a If the system d...

Page 16: ...the bulletins published by the Manufacturer The updates can be introduced by means of service software provided by the Manufacturer and the dedicated diagnostic interface 5 7 Spare parts The module do...

Page 17: ...is lodged within months 7 to 12 after date of purchase the warranty extends for a further 6 months after completion of the warranty repair 7 This warranty does not cover failures due to a mechanical...

Page 18: ...o Aero Technologies Sp z o o and shall not without prior written permission of Auto Aero Technologies Sp z o o be disclosed in whole or in part to third parties This statement shall be included on any...

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