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N-Number Inquiry Results

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N2454Y is Assigned

N-Number Entered: 2454y Aircraft Description
Serial Number 18280918 Status Ineffect/Invalid
Manufacturer Name CESSNA Certificate Issue Date 01/17/2020
Model 182S Expiration Date 01/31/2030
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) 50442615
MFR Year 2000 Mode S Code (Base 16 / Hex) A2458D
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE
Street GLEBE COTTAGE COOKES RD
City BERGH APTON NFLK State
County Zip Code NR15 1AA
Country UNITED KINGDOM
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 12/22/2000 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 T200430 Issue Date 01/17/2020 Expiration Date 02/16/2020
Fuel Modifications
Mod Code 28 Mod Date 20010105
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 09-27-97 AND ORIGINAL 337 APPROVAL IS RETAINED IN 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): 124. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT,A STRUCTURAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATEPROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 2/5/01.

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