FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 3449363 | Status | Valid |
| Manufacturer Name | PIPER AIRCRAFT INC | Certificate Issue Date | 08/31/2026 |
| Model | PA-34-220T | Expiration Date | 08/31/2033 |
| 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) | 51014240 |
| MFR Year | None | Mode S Code (Base 16 / Hex) | A418A0 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | N363NC CORP TRUSTEE | ||
| Street | PO BOX 1347 | ||
| City | WILMINGTON | State | DELAWARE |
| County | NEW CASTLE | Zip Code | 19899-1347 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | TSIO-360-RB | Category | Normal |
| A/W Date | 08/31/2007 | 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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| None |
| Certificate Number | T267842 | Issue Date | 08/31/2026 | Expiration Date | 09/30/2026 |
| Mod Code | 28 | Mod Date | 20070820 |
| TEMPORARY FUEL SYSTEM INSTALLED AND CHECKED AND FOUND TO OPERATE SATISFACTORILY. WEIGHT AND BALANCE COMPUTATION DATED JULY 2007. THISTEMPORARY LONG RANGE SYSTEM INSTALLATION WAS PERFORMED IN ACCORDANCE WITH REPORT KR-1390 AS REVISED DUPLICATION ALTERATION APPROVED ON FAA FORM 337 DATED MARCH 26, 1987 FOR PIPER PA-34-220T SN 3433041 N9120D AND EXTENDED GROSS WEIGHT PERMIT INCLUDED AS PERFORMED AND FILED WITH THIS REPAIR STATION. OIL CONSUMPTION ESTABLISHED DURING PREVIOUS FLIGHTS AND OIL SUPPLY DETERMINED TO BE ADEQUATE FOR LENGTH OF FLIGHT.FERRY SYSTEM SHALL BE REMOVED UPON ARRIVAL AT DESTINATION BY A CERTI- FIED MECHANIC OR REPAIR STATION AS REQUIRED BY THE FAA ADMINISTRATOR. LOG BOOK MUST BE COMPLETED. AIRCRAFT ACTUAL GROSS WEIGHT 4750 LBS. ALLOWABLE MAX WEIGHT AUTHORIZED FOR FERRY PURPOSES 5225 LBS. ALSO NOTE FERRY FUEL PLACARD LOCATED IN AIRCRAFT IN FULL VIEW OF THE PILOT.AIRCRAFT IS WITHIN THE FORWARD AND AFT C.G. LIMITS. PILOT IS RESPON- SIBLE FOR DETERMINING AIRCRAFT C.G. LIMITS ARE NOT EXCEEDED IN OVER- WEIGHT CONDITION. | |||
