FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N2413S is Assigned

N-Number Entered: 2413s Aircraft Description
Serial Number 337-0713 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 04/24/2023
Model 337B Expiration Date 04/30/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50433210
MFR Year 1967 Mode S Code (Base 16 / Hex) A23688
Type Registration LLC Fractional Owner NO
Registered Owner
Name QUALITAIR LLC TRUSTEE
Street FLUGPLATZ MICHELSTADT
MOSSAUER STRASSE 17
City MICHELSTADT State
County Zip Code 64720
Country GERMANY
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 None Type Certificate Holder None
Engine Manufacturer CONT MOTOR Classification Standard
Engine Model IO-360 SER Category None
A/W Date None 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 T235107 Issue Date 04/24/2023 Expiration Date 05/24/2023
Fuel Modifications
Mod Code 28 Mod Date 19990219
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-337-II, AF-337-FS, AF-337-ID, AF-337-OI, AND AF-TYP(S)150. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND THE AIRCRAFT IS WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTUAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCOR-DANCE WITH ABOVE NAMED DRAWINGS, OPERATED PROPERLY, AND DOES NOT LEAK.MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT HAS BEEN PROVIDED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 3/11/99.

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