FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 172S12058 | Status | Valid |
| Manufacturer Name | TEXTRON AVIATION INC | Certificate Issue Date | 02/24/2022 |
| Model | 172S | Expiration Date | 02/28/2029 |
| 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) | 51205705 |
| MFR Year | 2017 | Mode S Code (Base 16 / Hex) | A50BC5 |
| Type Registration | Government | Fractional Owner | NO |
| Name | UNIVERSITY OF ALASKA ANCHORAGE | ||
| Street | 2811 MERRILL FIELD DR | ||
| City | ANCHORAGE | State | ALASKA |
| County | ANCHORAGE DIV | Zip Code | 99501-4131 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | LYCOMING | Classification | Standard |
| Engine Model | IO-360-L2A | Category | Utility, Normal |
| A/W Date | 06/27/2017 | 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/ |
|||
| None |
| None |
| Mod Code | 28 | Mod Date | 20171205 |
| THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL TANK SYSTEM, CONSISTING OF TWO ALUMINUM FERRY FUEL TANKS. THE SYSTEM IS REQUIRED TOEXTEND THE RANGE FOR A FLIGHT FROM CALIFORNIA TO HONOLULU HAWAII. IN SUPPORT OF THE LONG RANGE FUEL SYSTEM A BASIC AIRCRAFT PRODUCTS, INC. TURBO ALTERNATOR PART # 50-1008-103 SERIAL # P1746 WAS EXTERNALLY MOUNTED TO THE LOWER LEFT COWLING AND CONNECTED TO THE PRIMARY BUS CIRCUIT, TO MAINTAIN AIRCRAFT ENGINE CONTROL UNIT POWER, IN THE CASE OF AN AIRCRAFT ALTERNATOR FAILURE. THE SYSTEMS SHALL BE REMOVED UPON ARRIVAL AT THE DESTINATION OR EXPIRATION OF THE SPECIAL FLIGHT PERMIT AND THE AIRCRAFT RETURNED TO NORMAL CONFIGURATION, PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. SYSTEM CONSISTS OF TWO ALUMINUM FERRY FUEL TANKS, A FUEL SELECTOR VALVE MANIFOLD AND ASSOCIATED FERRY FUEL FEED LINES FITTINGS AND VENT SYSTEM. THE FERRY FUEL SYSTEM IS CONNECTED TO A TEE FITTING MAIN FUEL LINE, BETWEEN THE AIRCRAFT LEFT MAIN TANKS ANDTHE FUEL SELECTOR. THE LEFT MAIN TANK FUEL IS ROUTED TO A SHUTOFF VALVE AND A FERRY FUEL SELECTOR VALVE AND THE POSITIVE AIRCRAFT ELECTRIC BOOST PUMP. THIS IS A DIRECT FEED SYSTEM. THERE IS A VENT FITTING INSTALLED IN THE LOWER FUSELAGE TO ALLOW POSITIVE VENT PRESSURE TO THE TWO FERRY FUEL TANKS. THE TWO FERRY FUEL TANKS ARE MOUNTED ON PALLETS ACROSS THE SEAT RAILS AND SECURED USING CARGO SYSTEMS, INC. CESSNA SEAT RAIL TYPE CARGO RINGS, AND (6) 700 POUND CARGO STRAPS. THE TANKS ARE BONDED TO THE FUSELAGE FOR GROUNDING. THISSYSTEM ALLOWS NORMAL OPERATION OF THE AIRCRAFT FUEL FEED SYSTEM TO THEENGINE, WITH EITHER THE AIRCRAFT MAN TANKS OR THE FERRY FUEL TANKS. | |||
| None |
