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N7207L has Assigned/Multiple Records

N-Number Entered: 7207l Aircraft Description
Serial Number EA-438 Status Valid
Manufacturer Name BEECH Certificate Issue Date 06/03/2016
Model B36TC Expiration Date 06/30/2029
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) 52323344
MFR Year 1984 Mode S Code (Base 16 / Hex) A9A6E4
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SPARKMAN AVIATION
Street PO BOX 13590
City ODESSA State TEXAS
County ECTOR Zip Code 79768-3590
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 Utility
A/W Date 05/03/1985 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 19940224
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE JET SOURCE INTERNATIONAL INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER JET SOURCE INTERNATIONAL INC DRAWINGS AF-BE-30-II, AF-BE-30-FS, AF-BE-ID, AF-BE-ID-2, AF-BE-30-FM, AND THE FOLLOWING FUEL TANK DRAWINGAF-TYP:124. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TOT HE PILOT AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IFTHE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMEDDRAWINGS, 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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