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Aerospace Logic Fuel Flow Kit Twin Engine

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From $2013.00 to $2013.00
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Description Part Number Price Buy
Aerospace Logic Fuel Flow Kit Twin Engine 30Gph
10-05173
$2013.00
Quantity
Aerospace Logic Multi Engine Fuel Flow Max 60Gph
10-05517
$2013.00
Quantity
Subtotal $0.00
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Overview

Aerospace Logic AOG Expedite Available, additional charges will apply.

The MF200 is an advanced, next generation manifold pressure and fuel flow combination instrument for flow rates up to 30-60gph.

Manifold pressure functionality is TSO'd and meets the pressure accuracy requirements of SAE AS8042. Fuel flow functionality is TSO'd and meets the accuracy requirements of TSO C44c.

Functional displays include:
Graphical indication of fuel flow
Digital display of instantaneous fuel flow
Digital display of fuel used since flight commencement
Fully programmable color indication to meet all aircraft marking requirements.

These are TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/night VFR and IFR).

These kits include both an A200-PMP manifold pressure sensor and a A200-201A-6 or a A200-201B-6 fuel flow sensor for full functionality.
   
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Features

    Certification / Compliance:
    TSO C44bCanadian STCFAA STCCertified as primary replacement
    SoftwareDO-178B
    DC Power Source
    Input voltage 6 to 36 VDCPower consumption 100mALoad dump tolerance +60VDirect spike tolerance +/- 60VCable spike tolerance > +/- 1KV
    Operating Temperature
    Constant operating -15ºC to +55ºCShort term operating (1hr) -40ºC to +70ºCStorage -55ºC to +85ºC
    Signal Input
    Pulse width modulated DC. 0-5V
    Accuracy
    AS407B +/- 0.1 USG/hr
    Display Units
    US Gallons per hour or Litres per hour, user selectable
    Range2 Channels 0.6 to 30-60USG/hr
    Display
    Sunlight readable LCD176 X 192 display pixels65,535 colors
    Annunciator Output
    100mA sink with reverse EMF protection
    RS-232 Data
    Output 1 second per full sequence at 57.6K bps (8/N/2/N)
    Interface Connector
    DB-25
    Software Functionality
    Primary Display: Instantaneous fuel flow in graphic and digital forms, total fuel used since flight commencement
    Trend Graph: Graphic display of flow vs time, instantaneous fuel flow

Specifications

  • Dimensions: 2.45” X 2.45” X 0.96”
  • Weight (excluding harness): 4.05 oz
  • Finish: Black anodized 6061 aluminum
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Please note, Aircraft Spruce's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.

Q: Is this unit FAA Approved for use in certified aircraft?

Yes, P/N 10-05173 is approved by the standard for TSO, STC. The manifold pressure functionality is TSO'd and meets the pressure accuracy requirements of SAE AS8042. Fuel flow functionality is TSO'd meets the accuracy of TSO C44c. The unit is TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/ night VFR and IFR).

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