AEROSPACE LOGIC FUEL FLOW KIT SINGLE ENGINE

От 284 100 до 284 100
Арт. MPN Описание Цена Add to cart form
10-05516
FF200K60
ASL SINGLE ENGINE FUEL FLOW MAX 60GPH
284 100
10-05172
FF200K30
AEROSPACE LOGIC FUEL FLOW KIT SINGLE ENGINE
284 100
Описание
Aerospace Logic AOG Expedite Available, additional charges will apply.

This kit includes both instrument and fuel flow transducer. The FF200 instrument is an advanced, next generation airborne fuel flow instrument that displays fuel flow in a single fuel line.
Fuel flow functionality is TSO'd and meets the repeatable accuracy requirements of SAE AS407B, +/- 0.1US Gallon per hour.

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 instrument kits are TSO'd and STC'd as a primary replacement instrument under all flight conditions (day/night VFR and IFR).
These instrument kits includes the full installation wiring harness, fuel flow transducer for a maximum fuel flow of 30-60gph and all necessary install hardware for the instrument. Installer supplied couplings are needed to be supplied by the installer to mate to the fuel flow transducer, as required.
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
    Range0.6 to 30-60 USG/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

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