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N59752 is Assigned

N-Number Entered: 59752 Aircraft Description
Serial Number 31-7612010 Status Valid
Manufacturer Name PIPER Certificate Issue Date 02/05/2004
Model PA-31-325 Expiration Date 08/31/2029
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) 51735212
MFR Year 1975 Mode S Code (Base 16 / Hex) A7BA8A
Type Registration LLC Fractional Owner NO
Registered Owner
Name VISIONAIRE ENTERPRISES LLC
Street PO BOX 5956
City STATESVILLE State NORTH CAROLINA
County IREDELL Zip Code 28687-5956
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 LYCOMING Classification Standard
Engine Model TI0-540 SER Category Normal
A/W Date 10/25/1975 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 19930119
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 12-27-89 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIRSTATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AEROFUSION DRAW-INGS AF-31-II, AF-31-FS/ID-1, AF-31-FS/ID, 2AF-31VS-ID AND AF-31-OI. THE TANKS WERE MANUFACTURED PER DRAWINGS AF-TYP-150 AND AF-TYP-98. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT ANDTHE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHTEXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUA- TION 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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