FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 2274 | Status | Valid |
| Manufacturer Name | OWEN WILLIAM D | Certificate Issue Date | 09/19/2025 |
| Model | GLASAIR | Expiration Date | 09/30/2032 |
| 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) | 52370120 |
| MFR Year | 1995 | Mode S Code (Base 16 / Hex) | A9F050 |
| Type Registration | Individual | Fractional Owner | NO |
| Name | SMITH MICHAEL R JR | ||
| Street | 144 TIMBER LN | ||
| City | FLORENCE | State | MISSISSIPPI |
| County | RANKIN | Zip Code | 39073-9263 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | LYCOMING | Classification | Experimental |
| Engine Model | O&VO-360 SER | Category | Amateur Built |
| A/W Date | 11/13/1995 | 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 | 19980708 |
| LONG RANGE FUEL TANK INSTALLED PER DRAWING(S) GLAS-OI, GLAS-II, GLAS-ID, GLAS-FS AND AF-TYP 35. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDEDTO PILOT AND AIRCRAFT IS WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVAL-UATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE FORM 337 FOR FURTHER INFO. EXPIRY DATE IS 8/10/98. | |||
| Mod Code | 28 | Mod Date | 19980708 |
| LONG RANGE FUEL TANK INSTALLED PER DRAWING(S) GLAS-OI, GLAS-II, GLAS- ID, GLAS-FS AND AF-TYP 35. NEW WEIGHT AND BALANCE COMPUTED AND PROVID-ED TO PILOT AND AIRCRAFT IS WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, STURCTURAL EVALUA-TION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROP-ERLY, AND DOES NOT LEAK. MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCUR- ACY. PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 8/10/98. | |||
