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N1530X is Assigned

N-Number Entered: 1530x Aircraft Description
Serial Number 28R-7535312 Status Valid
Manufacturer Name PIPER Certificate Issue Date 11/16/2023
Model PA-28R-200 Expiration Date 11/30/2030
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) 50153702
MFR Year 1975 Mode S Code (Base 16 / Hex) A0D7C2
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 LYCOMING Classification Standard
Engine Model I0360 SER Category Normal
A/W Date 06/25/1975 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
Certificate Number T233052 Issue Date 11/16/2023 Expiration Date 12/16/2023
Fuel Modifications
Mod Code 28 Mod Date 19921105
THIS DATA WAS FIELD-APPROVED BY FAA NE-FSDO-05 ON MAY 18, 1988 AND THEORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIRSTATION MANUAL. LONG-RANGE FUEL TANK/S INSTALLED PER AEROFUSION DRAW-INGS AF-PA-28-32-ID, AF-PA-28-32L, AF-PA-28-32-FM/LYC AND APPROPRIATE FUEL TANK DRAWING/S AF-TYP:-100/PIPER & AF-TYP-30. 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 CERTIFIED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATES PROPERLY AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FORACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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