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Fuel Flow, 1/4″ Female NPT.
Fuel flow transducer for use in aircraft with engine-driven fuel pumps & Horsepower up to 350 HP.
| Part Number | Description | Condition | Price | Availability | Stock | Order Qty | |
|---|---|---|---|---|---|---|---|
| 494-10001-00 | Garmin Fuel Flow Transducer (Experimental) | NEW | $530.00 | On backorder | 0 |
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
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