A&A Tech EEM MOT 01 FE03.02 Operator And Maintenance Manual

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Operators and Maintenance Manual
Page
1/16
Display EEM MOT 01 FE03.02
Operators and Maintenance Manual
Display
EEM MOT 01
FE03.02
Rev. 01 – December 2017
Copyright:
Auto & Aero Technologies Sp. z o.o.
Mazowiecka 10/5, 20-723 Lublin, Poland
■ email: info@aatech.pl ■ www.aatech.pl

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Summary of Contents for A&A Tech EEM MOT 01 FE03.02

  • Page 1 Operators and Maintenance Manual Page 1/16 Display EEM MOT 01 FE03.02 Operators and Maintenance Manual Display EEM MOT 01 FE03.02 Rev. 01 – December 2017 Copyright: Auto & Aero Technologies Sp. z o.o. Mazowiecka 10/5, 20-723 Lublin, Poland ■ email: info@aatech.pl ■ www.aatech.pl...
  • Page 2: Table Of Contents

    Operators and Maintenance Manual Page 2/16 Display EEM MOT 01 FE03.02 Table of Contents Introduction ....................3 General information ................3 Handling in transport and storage ............4 Installation ..................... 5 3.1. Environmental specifications ............5 3.2. Dimensions .................. 5 3.3.
  • Page 3: Introduction

    Operators and Maintenance Manual Page 3/16 Display EEM MOT 01 FE03.02 Introduction This instrument is intended for ultralight, microlight, homebuilt and experimental aircraft. The purpose of EEM MOT 01 type display is to present key engine status information to the pilot. Version FE03.02 displays fuel level, pitch and roll trim position, voltage, flight time, hobbs and number of recorded threshold crossings.
  • Page 4: Handling In Transport And Storage

    Operators and Maintenance Manual Page 4/16 Display EEM MOT 01 FE03.02 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.
  • Page 5: Installation

    Operators and Maintenance Manual Page 5/16 Display EEM MOT 01 FE03.02 3. Installation 3.1. Environmental specifications The EEM MOT 01 display has been designed to be installed in non- hermetic cockpits of ultralight aircrafts of ceiling not exceeding 3 000 m (10 000 ft).
  • Page 6: Mounting

    Operators and Maintenance Manual Page 6/16 Display EEM MOT 01 FE03.02 3.3. Mounting The display should be located conveniently within the pilot’s view in the control panel in the cockpit. The diameter of the mounting hole to be cut in the panel is 80mm. It is recommended that the display is installed from the rear side the control panel.
  • Page 7 Operators and Maintenance Manual Page 7/16 Display EEM MOT 01 FE03.02 The EEM MOT 01 display is connected to the system by in-built MOLEX Ultra-Fit 3.5 mm 6 pin male connector located at the back of the instrument. A schematic diagram of the connection is shown in Figure 4 and in Table 1.
  • Page 8: Operation And Maintenance

    Operators and Maintenance Manual Page 8/16 Display EEM MOT 01 FE03.02 4. Operation and maintenance The display is to be connected to EMS DAQ R2. The front panel of EEM MOT 01 is composed of three elements: the display, two status diodes (alert indication), and the encoder knob & push- button for setting parameters (Fig.
  • Page 9 Operators and Maintenance Manual Page 9/16 Display EEM MOT 01 FE03.02 g) Number of recorded threshold crossings – the upper centre of the display (e00); Fig. 6. Display of the FE03.02 software version On client’s request, warning and alarm threshold values may be set for some of the above parameters according to the specification provided by the aircraft supplier.
  • Page 10 Operators and Maintenance Manual Page 10/16 Display EEM MOT 01 FE03.02 As the aircraft operates within “normal” range of the parameter in question, the instrument displays values in green, and status diodes are green. If the threshold level is being exceeded, the instrument informs the pilot by changing both the colour of displayed figures and the colour of status diodes.
  • Page 11 Operators and Maintenance Manual Page 11/16 Display EEM MOT 01 FE03.02 Fig. 7. The idea of flight parameter status information Both diodes are always of the same colour corresponding to the status of the parameter that assumes “the worst” value.
  • Page 12: Service, Diagnostics And Repairs

    Operators and Maintenance Manual Page 12/16 Display EEM MOT 01 FE03.02 5. Service, diagnostics and repairs 5.1. Service life a) TBO of the display is not defined. b) In the case of failure or error, the display must not be used any more.
  • Page 13: Repairs

    Operators and Maintenance Manual Page 13/16 Display EEM MOT 01 FE03.02 b) If no information is displayed when power is applied (Fig. 8), check connection to measurement modules. Fig. 8. Indication of no connection to measurement modules c) In the case of the instrument’s failure or malfunction, turn power off and on again.
  • Page 14: Spare Parts

    Operators and Maintenance Manual Page 14/16 Display EEM MOT 01 FE03.02 The instrument’s firmware updates are to be conducted on the basis of 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.
  • Page 15 Operators and Maintenance Manual Page 15/16 Display EEM MOT 01 FE03.02 6. If a valid warranty claim 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.
  • Page 16 Operators and Maintenance Manual Page 16/16 Display EEM MOT 01 FE03.02 The information in this document is subject to change without notice and should not be construed as commitment by Auto & Aero Technologies Sp. z o.o. These technical data and the information embodied therein are the property of Auto &...

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