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Operators and Maintenance Manual 

 

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EEM MOT 01 FE03.02

 

Page 

4/16

 

 

Copyright: 

Auto & Aero Technologies Sp. z o.o. 

Mazowiecka 10/5, 20-723 Lublin, Poland  

 email: [email protected] 

  

www.aatech.pl 

 

 

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  instrument  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  themselves 

familiar  with  the  operation  of  this  instrument  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 
using non-original parts and subassemblies voids the warranty, relieves the 
supplier  from  any  liability,  making  the  instrument  lose  the  status  of  the 
product  of  Auto  &  Aero  Technologies  Sp.  z  o.o.  with  all  the  resulting 
consequences. 

2.  Handling in transport and storage 

1.

 

The EEM MOT 01 monitor is bubble-wrapped to protect it against 
vibration  and  other  physical  damage,  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 relative humidity stays in the range of 10

90 %, 

safe from condensation. 

3.

 

The display should be protected from water.  

Summary of Contents for EEM MOT 01 FE03.02

Page 1: ...Display EEM MOT 01 FE03 02 Page 1 16 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 Display EEM MOT...

Page 2: ...oduction 3 1 General information 3 2 Handling in transport and storage 4 3 Installation 5 3 1 Environmental specifications 5 3 2 Dimensions 5 3 3 Mounting 6 3 4 Power and wiring 6 4 Operation and main...

Page 3: ...ce is equipped with an in built colour display protected by anti reflective coated glass The encoder knob push button located in the front provides user interaction with the device The electric connec...

Page 4: ...This person has to make themselves familiar with the operation of this instrument and the effect of any possible failure or malfunction Under no circumstances does the manufacturer condone usage of t...

Page 5: ...ed in non hermetic cockpits of ultralight aircrafts of ceiling not exceeding 3 000 m 10 000 ft Acceptable range of operating parameters is listed below Operating temperature 20 o C 50 o C Short term o...

Page 6: ...e to be cut in the panel is 80mm It is recommended that the display is installed from the rear side the control panel The display is to be fastened to the panel by means of four M3 screws that are loc...

Page 7: ...A schematic diagram of the connection is shown in Figure 4 and in Table 1 The power supply pins no 5 and 6 requires 0 5 mm2 wires Data bus pins no 3 and 4 requires twisted pair wires 2 x 0 5mm2 accord...

Page 8: ...lay The EEM MOT 01 display displays values of flight parameters that are either directly measured or calculated by the system The display starts automatically as the power is turned on As shown in Fig...

Page 9: ...some of the above parameters according to the specification provided by the aircraft supplier Default threshold values are listed in Table 2 Tab 2 Parameters displayed by EEM MOT 01 FE03 01 display L...

Page 10: ...the diodes flashing red The pilot can switch off flashing by pushing the encoder knob Figure 7 presents the idea of colour codes and warning alarm indication Thus information on the status of a flight...

Page 11: ...ght Auto Aero Technologies Sp z o o Mazowiecka 10 5 20 723 Lublin Poland email info aatech pl www aatech pl Fig 7 The idea of flight parameter status information Both diodes are always of the same col...

Page 12: ...check if operational 2 After 100 hours of flight a Check the instrument s electric connections b Turn on the power on to check if operational 5 3 Cleaning and conservation The screen is to be buffed...

Page 13: ...needs to be replaced e A defective instrument must not be used 5 5 Repairs Repairs and inspections of the instrument can be conducted only by its manufacturer The display does not contain any user se...

Page 14: ...operation of the product if it is used in accordance with its intended purpose and in accordance with the Operators and Maintenance Manual 3 Auto Aero Technologies Sp z o o warrants this product for...

Page 15: ...airs c damage caused by abuse or misuse d unauthorised alterations to hardware or software 8 The warranty does not cover claims that arise from the product parameters unless they are different from va...

Page 16: ...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 reprod...

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