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Tempest Fluid Pump (a76411-render-1.1-transp-bckgrnd.png)
Part Number A80564

A80564, PLATINUM FLUID PUMP

Part # A80564

PLATINUM FLUID PUMP


$685.92
Retail Price: $857.41
In Stock

Get everything you need

FILTER KIT, Fluid Pump

$45.20 / was $56.50

In Stock

Product Details

Specifications

Approval
FAA PMA
Condition
New
Manufacturer
Tempest
Dimensions
L: 5 x W: 5 x H: 7.5 in
Weight
3 lbs
Unit of Measure
Each
McFarlane Part Number
A80564

Product Description

Tempest Platinum Electronic Fluid Pumps

  • FAA-PMA Direct Replacement
  • Internal, high-flow filter element
  • Easy maintenance
  • Facet Gold-Flo fluid pump replacements

Easy KIT-P1 filter replacement instructions - universal to all Tempest Fluid Pumps! (instructions on page 4)

WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources

Eligible Aircraft
Make Model Start S/N End S/N Comment Eligibility Chart
Cessna 152152S/N 15279406 – 1528603315286033Comment When STC SA1035CE is installed.Eligibility Chart 6630
Cessna A152A152S/N A1520735 – A1521049A1521049Comment When STC SA1035CE is installed.Eligibility Chart 6630
Cessna F152F152S/N F15201429 – F15201980F15201980Comment When STC SA1035CE is installed.Eligibility Chart 6630
Cessna FA152FA152S/N FA1520337 – FA1520425FA1520425Comment When STC SA1035CE is installed.Eligibility Chart 6630
Cessna 172N172NS/N 17267585 – 1727400917274009Comment When STC SA615NE is installed.Eligibility Chart 6630
Cessna 172P172PS/N 17274010 – 1727665417276654Comment When STC SA615NE is installed.Eligibility Chart 6630
Cessna 172Q172QS/N 17275869 – 1727621117276211Comment When STC SA615NE is installed.Eligibility Chart 6630
Cessna 310K310KS/N 310K0001 – 310K0245310K0245Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 310L310LS/N 310L0001 – 310L0207310L0207Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 310N310NS/N 310N0001 – 310N0198310N0198Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 310P310PS/N 310P0001 – 310P0240310P0240Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 310Q310QS/N 310Q0001 – 310Q1160310Q1160Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 310R310RS/N 310R0001 – 310R2140310R2140Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna T310PT310PS/N 310P0001 – 310P0240310P0240Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna T310QT310QS/N 310Q0001 – 310Q1160310Q1160Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna T310RT310RS/N 310R0001 – 310R2140310R2140Comment When STC SA2504CE is installed.Eligibility Chart 6630
Cessna 320D320DS/N 320D0001 – 320D0130320D0130Comment When STC SA2513CE is installed.Eligibility Chart 6630
Cessna 320E320ES/N 320E0001 – 320E0110320E0110Comment When STC SA2513CE is installed.Eligibility Chart 6630
Cessna 320F320FS/N 320F0001 – 320F0045320F0045Comment When STC SA2513CE is installed.Eligibility Chart 6630
Cessna 340340S/N 340-0001 – 340-0555340-0555Comment When STC SA2513CE is installed.Eligibility Chart 6630
Cessna 340A340AS/N 340A0001 – 340A1817340A1817Comment When STC SA2513CE is installed.Eligibility Chart 6630
Cessna 401401S/N 401-0001 – 401-0322401-0322Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 401A401AS/N 401A0001 – 401A0132401A0132Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 401B401BS/N 401B0001 – 401B0221401B0221Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 402402S/N 402-0001 – 402-0322402-0322Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 402B402BS/N 402B0001 – 402B1384402B1384Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 411411S/N 411-0001 – 411-0250411-0250Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 411A411AS/N 411-0251 – 411-0300411-0300Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 414414S/N 414-0001 – 414-0965414-0965Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 421421S/N 421-0001 – 421-0200421-0200Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 421A421AS/N 421A0001 – 421A0158421A0158Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 421B421BS/N 421B0001 – 421B0970421B0970Comment When STC SA2514CE is installed.Eligibility Chart 6630
Cessna 421C421CS/N 421C0001 – 421C1807421C1807Comment When STC SA2514CE is installed.Eligibility Chart 6630
Piper PA-31-325PA-31-325S/N 31-7400990 – 31-831201931-8312019Comment When STC SA1161SW is installed.Eligibility Chart 6630
Piper PA-31-350PA-31-350S/N 31-5001 – 31-855300231-8553002Comment When STC SA1161SW is installed.Eligibility Chart 6630
Cross Reference

Reference only: Please verify the product is eligible for your aircraft before adding to your cart.

  • 480563
FAQs

I have just installed my new Fuel Pump and my engine will not start. Why?

A common cause for this problem is fuel starvation due to improper installation of the fuel pump. Make sure that the fuel lines are not crossed; that is, the inlet line should be connected to the inlet side of the pump (marked “IN” on the top of the port) and the outlet line should be attached to the fuel pump outlet port. Fuel should be present at the inlet side of the fuel pump.

 

Improper installation of the fuel pump may result in a misalignment of the operating lever with the operating plunger in the accessory case. If so, there will be no movement of the lever and no pumping motion to provide fuel flow. If misalignment is found upon removal of the pump, the lever is probably damaged or broken. If misalignment of the operating lever has occurred, it will require inspection and repair by a qualified technician.

What is causing the fuel (or oil) to leak from my Fuel Pump drain line?

Leaking fuel or oil through the fuel pump overboard drain line indicates the rotary seal is running dry or contamination happened in the field. Your fuel pump should be replaced before further flight.

What is causing my fuel pressure to fall below the “green arc”?

The most common reasons for low fuel flow/pressure are the following:

  1. A worn or broken O-ring on the inlet side fuel fitting can cause an inlet suction leak. An inlet air leak will result in low Fuel Pump output pressure.
  2. A weak operating spring in the Fuel Pump diaphragm assembly
  3. A worn fuel pressure gauge
  4. A clogged fuel vent or fuel cap
  5. A constriction in a fuel line either externally (a kinked hose), or internally (due to a collapsed hose lining)
  6. Wrong fuel pump for the installation

What is causing my fuel pressure to fluctuate?

Fluctuating fuel pressure can be the result of the following:

  1. A worn fuel pressure gauge
  2. A worn or broken O-ring on the inlet side fuel fitting
  3. An obstruction in the induction system (air intake)
  4. A clogged or dirty fuel strainer
  5. Foreign material inside the fuel body (such as fuel cell sealant, thread sealant, or a drill shaving)

Is there a mandatory replacement time for diaphragm fuel pumps?

Diaphragm fuel pumps should be replaced or overhauled:

  1. At engine TBO or after ten years in service, whichever occurs first. Replace on condition if leaks develop or performance drops for example.
  2. Refer to Lycoming Mandatory Service Bulletin 240W for information regarding engine TBO.

How do I keep contaminants out of my fuel system?

The fuel selector valve works in unscreened fuel. Contaminated fuel can cause selector valve seal damage. When fueling from possibly contaminated fuel sources McFarlane recommends the use of a fuel filter, such as Mr. Funnel or another filtering device, to reduce trash in the fuel system.

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