FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 17251176 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 04/03/2007 |
| Model | 172E | Expiration Date | 07/31/2027 |
| 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) | 51120005 |
| MFR Year | 1964 | Mode S Code (Base 16 / Hex) | A4A005 |
| Type Registration | Co-Owned | Fractional Owner | NO |
| Name | HAMRICK STEVEN G | ||
| Street | 1120 INTERCEPTOR DR | ||
| City | PAHRUMP | State | NEVADA |
| County | NYE | Zip Code | 89060-2699 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | 0-300 SER | Category | Normal |
| A/W Date | 02/29/1964 | 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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| HAMRICK SARAH E |
| None |
| Mod Code | 28 | Mod Date | 20100811 |
| INSTALLED AN 18-GALLON AUXILLIARY FUEL TANK AND TRANSFER SYSTEM IN THEAFT BAGGAGE COMPARTMENT. INSTALLED O & N MODIFICATIONS FAA-PMA FUEL TANK PN 172201-1 SN 404 IN THE SAME MANNER AS REQUIRED PER STC SA615NEINTALLATION OF AN 18 GALLON FUEL TANKE IN THE AFT BAGGAGE COMPARTMENT AND FUEL TRANSFER SYSTEM IN ACCORDANCE WITH O & N INSTALLATION DRAWINGLIST 172100, REPORT NO. N-1012 DATED REVISION A, DATED JUNE 1, 1989, OR LATER FAA APPROVED REVISIONS. DEVIATED FROM O & N INSTALLATION DRAWING BY INSTALLING THE AUXILIARY TANK FUEL GAUGE, TRANSFER PUMP CONTROLSWITCH, AND INDICATOR LIGHT IN EXISTING, VACANT INSTURMENT PANEL MOUNTING HOLES LOCATED ABOVE THE GLOVE BOX ON THE LOWER RIGHT HAND SIDE OF THE INSTRUMENT PANEL. MOUNTING WAS ACCOMPLISHED IN ACCORDANCE WITH AC 43-13-2B, CHAPTER 11, PARA 1104 A, D, & E, PARA 1106 D, & G. THE REQUIRED PLACARDS WERE INSTALLED IN CLOSE PROXIMITY OF THE CONTROLSWITCH. WEIGHT AND BALANCE, EQUIPMENT LIST HAVE BEEN AMENDED. PLACARDSHAVE BEEN INSTALLED. ATTACHED IS AN FAA APPROVED SUPPLEMENTAL AIRPLANEFLIGHT MANUAL FOR THIS FUEL TANK INSTALLATION. A COPY OF THIS FAA 337 FOR THIS AUXILIARY FUEL TANK MODIFICATION MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES. | |||
