FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N8213Y is Assigned

N-Number Entered: 8213y Aircraft Description
Serial Number 30-1340 Status Valid
Manufacturer Name PIPER Certificate Issue Date 12/05/2015
Model PA-30 Expiration Date 12/31/2028
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) 52633552
MFR Year 1966 Mode S Code (Base 16 / Hex) AB376A
Type Registration Individual Fractional Owner NO
Registered Owner
Name BOOMER JOSHUA G
Street 3700 MIRVILLE CT
City FLOYDS KNOBS State INDIANA
County FLOYD Zip Code 47119-9782
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 A1EA Type Certificate Holder PIPER AIRCRAFT INC
Engine Manufacturer LYCOMING Classification Standard
Engine Model IO-320 SERIES Category Normal
A/W Date 11/14/1966 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 19920326
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON JULY 13, 1990 AND THE ORIGINAL 337 APROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK INSTALLED PER AEROFUSION DRAWINGS AF-PA30-II, AF-PA30-ID, AF-PA30-FS, AF-PA30-OI AND MANU- FACTURED PER FUEL TANK DRAWING AF-TYP-85. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND THE AIRCRAFT IS WITHINTHE WEIGHT AND C.G.LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT A STRUCTURAL EVALUATION LETER 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 FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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