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Aerospace Logic Multi Engine Fuel Flow Max 60Gph
MFR Model# FF202K60
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- Overview
- Features
- Specifications
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- Q&A
Overview
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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. |
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
Q&A
Please note, Aircraft Spruce Australia'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 Australia 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.
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).