Factory rebuilt by HET:


Overhauled by QAA:


Turbocharger Maintenance:
Maintenance on a turbocharger is critical to obtain a long and hassle free service life. A turbocharger must regularly withstand extreme operating conditions –with exhaust inlet temperatures exceeding 1600° F and the turbine wheel rotating at over 90,000 RPM. Turbine and compression wheel blades must be carefully inspected for any cracks or damage caused by foreign object debris. It is also important to turn the wheels by hand and inspect for any drag or rubbing against the housing. One of the most important processes in the turbocharger is the lubrication system, which is provided by the aircraft engine oil. Oil contamination, foreign object debris, and oil supply problems are the most frequent reasons for premature turbocharger failure and can lead to overheating of the bearings and the center housing.


Need help troubleshooting?


Call QAA at 877-833-6948 and we will be happy to help.

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TUL: 5746 E Apache St. Tulsa, OK 74115
FXE: 1072 NW 53rd St. Fort Lauderdale, FL 33309
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  • Turbocharger

    Part#: CF600803-9001

    *Not all photographs represent the actual product for sale.

    Overhaul/Exchange

    Price: $3,250.00

    Core: $500

    The CF600803-9001 (Turbo Model Designation: 3AU2ME60H2) Aircraft Turbocharger is used on a Piper aircraft application. Maintenance on an Aircraft Turbocharger is critical to obtain a long and hassle free service life. An Aircraft Turbocharger must regularly withstand extreme operating conditions - with exhaust inlet temperatures exceeding 1600° F and the turbine wheel rotating at over 90,000 RPM. At all 100 hour inspections the turbine and compression wheel blades must be carefully inspected for any cracks or damage caused by foreign object damage. It is also important to turn the wheels by hand and inspect for any drag or rubbing against the housing. One of the most important processes in the Aircraft Turbocharger is the lubrication system, which is provided by the aircraft engine oil. Oil contamination, foreign object damage, and oil supply problems are the most frequent reasons for premature Aircraft Turbocharger failure and can lead to overheating of the bearings and the center housing.

    Aircraft: Engine:
    Piper Aerostar 700P

    TIO-540-U2A,

    LTIO-540-U2A

    If you wish to obtain more information on your aircraft turbocharger, please see the below links:

    Q: What gaskets will come with the Aircraft Turbocharger I just purchased?

    A: With the purchase of your Aircraft Turbocharger you will receive the oil gaskets for the unit. Exhause gaskets are available upon request.

    Q: What is the torque specification for the through bolts on my Aircraft Turbocharger?

    A: The turbine housing through bolt specification is 180 in/lbs for an Aircraft turbocharger.

    Q: I think my Aircraft Turbocharger is leaking oil, how can I check to make sure?

    A: Please visit our Aircraft Turbocharger resource center (http://www.qaa.com/aircraft-turbochargers-wastegates-aircraft-controllers-and-valves) for troubleshooting oil leaks in your Aircraft Turbocharger.

    Q: Does the Aircraft Turbocharger also come with a heat shield?

    A: The Aircraft Turbochargers provided by QAA do not have a heat shield included. You will need to keep your heat shield from your original Aircraft Turbocharger and swap it over the the new unit you receive.

  • Details

    The CF600803-9001 (Turbo Model Designation: 3AU2ME60H2) Aircraft Turbocharger is used on a Piper aircraft application. Maintenance on an Aircraft Turbocharger is critical to obtain a long and hassle free service life. An Aircraft Turbocharger must regularly withstand extreme operating conditions - with exhaust inlet temperatures exceeding 1600° F and the turbine wheel rotating at over 90,000 RPM. At all 100 hour inspections the turbine and compression wheel blades must be carefully inspected for any cracks or damage caused by foreign object damage. It is also important to turn the wheels by hand and inspect for any drag or rubbing against the housing. One of the most important processes in the Aircraft Turbocharger is the lubrication system, which is provided by the aircraft engine oil. Oil contamination, foreign object damage, and oil supply problems are the most frequent reasons for premature Aircraft Turbocharger failure and can lead to overheating of the bearings and the center housing.

  • Engine Applications

    Aircraft: Engine:
    Piper Aerostar 700P

    TIO-540-U2A,

    LTIO-540-U2A

  • Resources

    If you wish to obtain more information on your aircraft turbocharger, please see the below links:

  • FAQs

    Q: What gaskets will come with the Aircraft Turbocharger I just purchased?

    A: With the purchase of your Aircraft Turbocharger you will receive the oil gaskets for the unit. Exhause gaskets are available upon request.

    Q: What is the torque specification for the through bolts on my Aircraft Turbocharger?

    A: The turbine housing through bolt specification is 180 in/lbs for an Aircraft turbocharger.

    Q: I think my Aircraft Turbocharger is leaking oil, how can I check to make sure?

    A: Please visit our Aircraft Turbocharger resource center (http://www.qaa.com/aircraft-turbochargers-wastegates-aircraft-controllers-and-valves) for troubleshooting oil leaks in your Aircraft Turbocharger.

    Q: Does the Aircraft Turbocharger also come with a heat shield?

    A: The Aircraft Turbochargers provided by QAA do not have a heat shield included. You will need to keep your heat shield from your original Aircraft Turbocharger and swap it over the the new unit you receive.

We will be closed 11/23 and 11/24 for Thanksgiving and 12/25-1/1 for the Holidays.