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N352RC is Assigned

N-Number Entered: 352rc Aircraft Description
Serial Number 0186 Status Valid
Manufacturer Name CIRRUS DESIGN CORP Certificate Issue Date 07/01/2024
Model SR22 Expiration Date 07/31/2031
Type Aircraft Fixed Wing Single-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50766665
MFR Year 2002 Mode S Code (Base 16 / Hex) A3EDB5
Type Registration Corporation Fractional Owner NO
Registered Owner
Name N352RC INC TRUSTEE
Street 1013 CENTRE RD STE 403-A
City WILMINGTON State DELAWARE
County NEW CASTLE Zip Code 19805-1270
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
Type Certificate Data Sheet A00009CH Type Certificate Holder CIRRUS DESIGN CORP
Engine Manufacturer CONT MOTOR Classification Standard
Engine Model IO-550 SERIES Category Normal
A/W Date 03/29/2002 Exception Code No
The information contained in this record should be the most current Airworthiness information available in the historical aircraft record. However, this data alone does not provide the basis for a determination regarding the
airworthiness of an aircraft or the current aircraft configuration. For specific information, you may request a copy of the aircraft record at https://aircraft.faa.gov/e.gov/ND/
Other Owner Names
None
Temporary Certificates
Certificate Number T246532 Issue Date 07/01/2024 Expiration Date 07/31/2024
Fuel Modifications
Mod Code 28 Mod Date 20090123
THIS AIRCRFAFT HAS BEEN EQUIPPED WITH A TEMPORARY FERRY FUEL SYSTEM, CONSISTING OF ONE 105 GALLON TANK INSTALLED IAW EA-FSDO-65 ACCEPTED DATA CIRRUS DRAWING #13222 DATED 10-12-99 AND TELFORD AVIATION SVCS, INC REPORT TAS-CDC-SR20/22. SEE ATTACHED TEMPORARY WEIGHT AND BALANCEDATA. THIS TEMPORARY WEIGHT AND BALANCE WILL REMAIN IN EFFECT FOR THEDURATION OF THE SPECIAL FLIGHT PERMIT (FAA FORM 8130-7) AND/OR THE TEMPORARY FUEL SYSTEM IS REMOVED. REQUIREMENT FOR ADDITIONAL OIL HAS BEEN ESTABLISHED IAW AC23.1011-1. REMOVAL INSTRUCTIONS ARE INCLUDED ALONG WITH FERRY FUEL SYSTEM MANAGEMENT INSTRUCTIONS. NOTE: THIS IS A TEMPORARY INSTALLATION. UPON ARRIVAL AT DESTINATION, THE TEMPORARY FERRY FUEL SYSTEM MUST BE REMOVED; THE AIRCRAFT INSPECTED FOR DAMAGE AND PROPER OPERATIONS; AND THE COMPASS CHECKED FOR ACCURACY BEFORE RETURNING THIS AIRCRAFT TO SERVICE. THE CURRENT WEIGHT AND BALANCE DATA IN THE FAA APPROVED AIRPLANE FLIGHT MANUAL OR PILOTS OPERATING HANDBOOK WILL AGAIN APPLY.

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