8001080

8001080 OIL COOLER, 7 ROW, DRAWN CUP -8 STRAIGHT THREADS

PN: 8001080


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Condition: NEW

Unit of Measure: EA


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DESCRIPTION | FEATURES | SPECIFICATIONS | DOCUMENTS | VIDEO | ASK A QUESTION

DESCRIPTION


OIL COOLER, 7 Row Drawn Cup, 8

Engine Manufacturer Lycoming
Aircraft Manufacturer Piper
Aircraft Model PA-28-181
Replacement For 20710A, 85472-012
Engine Placement Remote

AERO-Classics Remote-Mount Oil Coolers

Remote-mount oil coolers mount to the airframe or engine baffle instead of directly to the engine. Hoses are used to connect the oil cooler to the engine. This type of oil cooler is used with most non-Continental engines including all Lycoming engines.

FAA-PMA Approved

  • Direct replacements for most oil coolers
  • Ideal for many certified and experimental aircraft
  • FAA 8130-3 tags included with each oil cooler

Outstanding Performance

In side-by-side comparative performance tests, AERO-Classics 7 and 9 plate oil coolers outclassed competitive models, offering better overall cooling and lower weight.

Highest Quality, Best Value

  • Corrosion protection per MIL-C-5541, Class 1A
  • Pressure tested to 400 psig
  • Optimized internal oil flow design
  • Low cost
  • Two year warranty
  • In-stock at supplier for fast delivery

FEATURES



 

SPECIFICATIONS


Package Dimensions

Length30.5 cm
Height12.7 cm
Width27.9 cm
Weight907 g

Details

MANUFACTURER INSTALLATION TIPS:

Mounting Flanges

Be sure to mount the cooler using all four mounting flanges. This will evenly distribute stress that can cause cracking.

Threads and Hoses

  • On pipe (tapered) threads, Anti-seize lubricant should always be used to prevent thread galling. Steel fittings are an additional added measure that can prevent thread galling.
  • Avoid damage to the oil cooler during operation. Hoses connecting to the oil cooler should be installed, supported, and tied down in a manner that will avoid vibration and pulling stresses being induced onto the oil cooler. Hoses must be fastened to the same structure that the cooler is attached to. If the cooler is mounted to the airframe structure, the hoses must be supported by the airframe structure. If the cooler is attached to the engine structure, the hoses must be supported by the engine structure. Do not allow engine movement stresses to be induced into the cooler through the hoses.
  • A back-up wrench should always be used when installing fittings into any oil cooler to prevent damage to the oil cooler.
  • Please note (if applicable) the threads on this part have been inspected by the manufacturer before shipment and found to be in conformity. Galling of threads is not considered a warrantable claim.

BROCHURES & DOCUMENTATIONS


List of Brochures



List of Documentation


Document 1

VIDEO


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