FAA REGISTRY
N-Number Inquiry Results
| Serial Number | T18209058 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 12/10/2024 |
| Model | T182T | Expiration Date | 12/31/2031 |
| Type Aircraft | Fixed Wing Single-Engine | Type Engine | Turbo-prop |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 51055365 |
| MFR Year | 2012 | Mode S Code (Base 16 / Hex) | A45AF5 |
| Type Registration | LLC | Fractional Owner | NO |
| Name | ABA AVIATION LLC | ||
| Street | 21300 KATHY FLEMING RD | ||
| City | NAVASOTA | State | TEXAS |
| County | GRIMES | Zip Code | 77868-2900 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | 3A13 | Type Certificate Holder | TEXTRON AVIATION INC |
| Engine Manufacturer | LYCOMING | Classification | Standard |
| Engine Model | TIO-540-AK1A | Category | Normal |
| A/W Date | 02/27/2012 | 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 | 20180312 |
| THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL SYSTEM, CONSIST ING OF TWO ALUMINUM FERRY FUEL TANKS. SYSTEM IS THE SAME AS PREVIOUSLYINSTALLED IN ACCORDANCE WITH FAA FORM 337 DATED 10/24/2017 WITH MINOR MODIFICATION IN THE TANK QUANTITIES. THE SYSTEM IS REQUIRED TO EXTEND THE RANGE FOR A FLIGHT FROM HAWAII TO NEVADA. THE SYSTEMS SHALL BE REMOVED UPON ARRIVAL AT THE DESTINATION OR EXPIRATION OF THE SPECIAL FLIGHT PERMIT AND THE AIRCRAFT RETURNED TO NORMAL CONFIGURATION, PRIORTO 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 FUEL SELECTOR VLAVE AND THE 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. THIS SYSTME ALLOWS NORMAL OPERATION OF THE AIRCRAFT FUEL FEED SYSTEM TO THE ENGINE, WITH EITHER THE AIRCRAFT MAIN TANKS ORTHE FERRY FUEL TANKS. OTHER MODIFICATIONS TO THE AIRCRAFT TO ACCOMMO DATE THE FERRY FUEL SYSTEM ARE THE REMOVAL OF THE COPILOTS SEAT AND SEATS 3 AND 4 TO ACCOMMODATE THE FERRY FUEL TANKS. THE SYSTEM INCORPORATES TWO FERRY FUEL TANK SELECTOR VALVES. THE FERRY FUEL VALVES SUPPLYFUEL DIRECTLY TO THE ELECTRIC BOOST PUMP, STRAINER AND ENGINE DRIVE | |||
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