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N4827U has Assigned/Multiple Records

N-Number Entered: 4827u Aircraft Description
Serial Number U20605119 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 10/15/1999
Model TU206G Expiration Date 08/31/2028
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) 51371547
MFR Year 1979 Mode S Code (Base 16 / Hex) A5F367
Type Registration Individual Fractional Owner NO
Registered Owner
Name HAGEN RAINER
Street 381 LAS COLINAS BLVD E APT 2004
City IRVING State TEXAS
County DALLAS Zip Code 75039-5555
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 None Type Certificate Holder None
Engine Manufacturer CONT MOTOR Classification Standard
Engine Model TSIO-520 SER Category Normal
A/W Date 06/30/1979 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 T996681 Issue Date 10/15/1999 Expiration Date 11/14/1999
Fuel Modifications
Mod Code 28 Mod Date 19920814
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON JUNE 10, 1988 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-CE-100/200-VRII, AF-CE-100/200-1, AF-C-100/200-1, AF-C-100/200-3-ID, AF-C-100/200-2-ID AND THE FOLLOWING FUEL TANK DRAWINGS - AF-TYP:-150. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT, AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFI-CATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATED PROPERLY AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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