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N-Number Inquiry Results

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N369AN is Assigned

N-Number Entered: 369an Aircraft Description
Serial Number 18280696 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 07/15/2025
Model 182S Expiration Date 07/31/2032
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) 51026710
MFR Year 2000 Mode S Code (Base 16 / Hex) A42DC8
Type Registration Corporation Fractional Owner NO
Registered Owner
Name JET AIRCRAFT 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 3A13 Type Certificate Holder TEXTRON AVIATION INC
Engine Manufacturer LYCOMING Classification Standard
Engine Model IO-540 SER Category Normal
A/W Date 03/08/2000 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 T259589 Issue Date 07/15/2025 Expiration Date 08/14/2025
Fuel Modifications
Mod Code 28 Mod Date 20000324
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 9-27-97 AND ORIGINAL 337APPROVAL IS RETAINED IN THE TELFORD AVIATION SERVICES INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION SERVICES INC DRAWINGS AF-CE-182S-II, AF-CE-182S-OI, AF-CE-182S-FS, AF-CE-182S-ID, AND AF-TYP(S): 100. NEW WEIGHT AND BALANCE COM- PUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMIT.IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUC- TURAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 4/23/00.

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