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N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N403SW has Assigned/Multiple Records

N-Number Entered: 403sw Aircraft Description
Serial Number 18280830 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 07/20/2023
Model 182S Expiration Date 07/31/2030
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) 51134553
MFR Year None Mode S Code (Base 16 / Hex) A4B96B
Type Registration LLC Fractional Owner NO
Registered Owner
Name BSF SKYLANE LLC
Street 1670 PATRICK MILL PL
City BUFORD State GEORGIA
County GWINNETT Zip Code 30518-2270
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-AB1A5 Category Normal
A/W Date 12/10/2019 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
None
Fuel Modifications
Mod Code 28 Mod Date 20000926
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-172S-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 10/27/00.

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