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This aircraft's registration status may not be suitable for operation.
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FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 34-7970425 | Status | Notice Ineff/Inval |
| 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 |
| Name | SOUTHWINDS EXPORT INC | ||
| Street | 2631 ONEIDA LOOP | ||
| City | KISSIMMEE | State | FLORIDA |
| County | OSCEOLA | Zip Code | 34747-2789 |
| Country | UNITED STATES | ||
| 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 |
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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/ |
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| 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. | |||
