DOT logo United States Department of Transportation
Aircraft Inquiry

FAA REGISTRY

N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N2965R has Assigned/Multiple Records

N-Number Entered: 2965r Aircraft Description
Serial Number 34-7970425 Status Valid
Manufacturer Name PIPER Certificate Issue Date 07/18/2022
Model PA-34-200T Expiration Date 07/31/2029
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) 50607333
MFR Year None Mode S Code (Base 16 / Hex) A30EDB
Type Registration Non Citizen Corporation Fractional Owner NO
Registered Owner
Name SOUTHWINDS EXPORT INC
Street 2631 ONEIDA LOOP
City KISSIMMEE State FLORIDA
County OSCEOLA Zip Code 34747-2789
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 12/09/2004 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 19920507
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON JUNE 20, 2988 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-PA-34-II, AF-PA-34-ID, AF-PA-34-FS, AF-PA-34-FM ANDTHE FOLLOWING FUEL TANK DRAWINGS AF-TYP:-205. A NEW WEIGHT AND BALANCEHAS 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 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 AHS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

You are accessing a U.S. Government authorized information system, which includes (1) this computer, (2) this computer network, (3) all computers connected to this network, (4) all devices and storage media attached to this network or to a computer on this network, and (5) all cloud services and hosting environments supporting this information system. This information system is provided for U.S. Government-authorized use only.

Unauthorized or improper use of this system may result in disciplinary action, as well as civil and criminal penalties.

By logging in and using this information system, you understand and consent to the following:

  • You have no reasonable expectation of privacy regarding communications or data transiting or stored on this information system.
  • At any time, and for any lawful Government purpose, communication between the user and this information system, data transiting to/from the system, or stored on this system is subject to monitoring, interception, and search.
  • Any communications or data transiting or stored on this information system may be disclosed or used for any lawful Government purpose.


D O T Triskelion

U.S. Department of Transportation

Federal Aviation Administration

800 Independence Avenue, SW

Washington, DC 20591

(866) TELL-FAA | (866) 835-5322