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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N8151Z is Assigned

N-Number Entered: 8151z Aircraft Description
Serial Number 28R-8031052 Status Valid
Manufacturer Name PIPER Certificate Issue Date 08/25/2011
Model PA-28RT-201T Expiration Date 08/31/2027
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) 52617202
MFR Year 1979 Mode S Code (Base 16 / Hex) AB1E82
Type Registration Corporation Fractional Owner NO
Registered Owner
Name AIRCRAFT GUARANTY CORP TRUSTEE
Street 928 SW 107TH ST
City OKLAHOMA CITY State OKLAHOMA
County CLEVELAND Zip Code 73170-5244
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-360 SER Category Normal
A/W Date 01/25/1980 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 T181806 Issue Date 03/14/2018 Expiration Date 04/13/2018
Fuel Modifications
Mod Code 28 Mod Date 19940405
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION INC DRAWINGS AF-PA-28-32-C, AF-PA-28032-II/CONT, AND APPROPRIATE FUEL TANK DRAWING(S) AF-TYP:100. 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 CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THS FUEL SYSTEM HAS BEENINSTALLED 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 INSTRUC- TIONS. PRIOR TO APPROVING THIS AIRCRAFT FOR A RETURN TO SERVICE IN THE STANDARD CATEGORY, THE FUEL SYSTEM MUST BE RETURNED TO IT'S ORIGINAL CONFIGURATION.

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