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Garmin Fuel Flow Transducer (Experimental)

SKU: 494-10001-00 Category: Tag: Brand: Garmin

Available on backorder

AUD $415.00 

Fuel Flow, 1/4″ Female NPT.

Fuel flow transducer for use in aircraft with engine-driven fuel pumps & Horsepower up to 350 HP.

 

Available on backorder

FAA Approved Instrument

  • FAA TSO’d and STC’d
  • Up to 350 HP engines, engine driven fuel pumps only.
  • Red anodize aluminium body, 5.3 ounces.
  • 1/4” female NPT, 1.375 in. (height) x 1.620 in. (width) x 1.90 in. (length)
  • .6 to 70+ GPH, .6 PSI drop at 30 GPH, 2.3 PSI drop at 60 GPH

FT-60 Cube Fuel Flow Sensor kit

Model: FT-60 (Red Cube)

K-Factor: 68,000 Pulses/Gal (installation configurations can affect the K-Factor) (use 680 when programing the KFactor in the FP-5(L).

Pressure Drop (with 6.0 Lbs/Gal fuel), (blocked or unblocked rotor) : 0.5PSI @ 28 Gal/Hr 2.0PSI @ 56 Gal/Hr

To Calculate Pressure Drop: P = (Flow) 2 x Wf P = Pressure Drop in PSI 9573 Flow = Fuel Flow in Gal/Hr. Wf = Weight of Fuel in Lbs/Gal

Non-Flow Restricting Design (a blocked rotor does not restrict flow)

Fuel Flow Range: 0.6 to 70+ Gal/Hr.

Fuel Flow Over Range (with no damage to transducer):

Unlimited Linearity: +/- 1% over an engine’s normal operating range.

Repeatability: +/- 1/4%

Burst Pressure: 4,000 psi minimum

Working Pressure: 250 psi

Temperature Range: -65°C to 125°C Weight: 5.26 Oz.

Life Expectancy: 10,000 Hrs. Min.

FAA TSO’d, STC’d and PMA’d

  • Red Cube FT-60 and pigtail wiring

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FAA Approved Instrument

  • FAA TSO’d and STC’d
  • Up to 350 HP engines, engine driven fuel pumps only.
  • Red anodize aluminium body, 5.3 ounces.
  • 1/4” female NPT, 1.375 in. (height) x 1.620 in. (width) x 1.90 in. (length)
  • .6 to 70+ GPH, .6 PSI drop at 30 GPH, 2.3 PSI drop at 60 GPH