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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N9123X has Assigned/Multiple Records

N-Number Entered: 9123x Aircraft Description
Serial Number 3229003 Status In Question
Manufacturer Name PIPER Certificate Issue Date None
Model PA-32R-301T Expiration Date None
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) 53120360
MFR Year 1987 Mode S Code (Base 16 / Hex) ACA0F0
Type Registration Individual Fractional Owner NO
Registered Owner
Name REGISTRATION PENDING
Street PO BOX 10045
City JACKSON State WYOMING
County TETON Zip Code 83002-0045
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 TI0-541 SER Category Normal
A/W Date 10/27/2022 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
APPLICANT IRISH FLYBOY LLC
APPLICATION DATED 102825
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 19931229
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-PA30-II, AF-PA30-ID, AF-PA30-FS, AF-PA30-0I, 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 CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMEDDRAWINGS, OPERATES 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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