Cessna R182, TR182 Shock Strut Piston NLG P/N 2243001-201 (0818-94)
Regular price $2,395.00
Shipping calculated at checkout.
Cessna R182 and TR182 Shock Strut Nose Landing Gear. P/N 2243001-201. Chrome is in great condition with no pitting or wear marks. Removed in good condition from a parted out 1978 Cessna R182 Skylane RG N199TX, S/N R18200286. TTAF 6192.84. Guaranteed to pass inspection or your money back. $6451.00 in 2018
30 Day Money Back Guaranteed less shipping costs. It is the buyers responsibility to determine the parts suitability for installation and airworthiness upon inspection.
We are a full service aircraft maintenance shop that sells new aircraft parts from surplus inventory auctions and parts from salvaged airplanes. We try to be as clear as possible in the descriptions of the items we have listed for sale. If you have any question regarding the suitability or condition of a part please let us know and we will have one of our mechanics check it out and give an honest answer as to it's condition. Unless otherwise noted we will ship the majority of our items via UPS. Free shipping is usually USPS. Tracking information will be sent to the E-mail account on file with Paypal, so please make sure your information is up to date.
Terms and Conditions:
Payment: Please pay within two (2) business days of auction's close. We accept Paypal and all major credit cards.
Shipping: We will ship with in one (1) business day of receiving payment. We will gladly ship almost any item worldwide. International buyers, please contact us prior to paying.
All buyers from OHIO please add 6.5% sales tax.
Customs/Duties: International Buyers please be aware of Tariffs/Taxes/Duties/Charges prior to purchase.
If you are in doubt as to whether we can ship to your country or province please contact us prior to your purchase.
Also, we will not declare the value of purchased merchandise to be below what the buyer paid, nor will we declare merchandise to be a gift to avoid duties.
Safe Skies Aviation, LLC, Middletown Ohio 45042
Loc. LS 113 E