FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 4300 | Status | Valid |
| Manufacturer Name | CIRRUS DESIGN CORP | Certificate Issue Date | 09/09/2024 |
| Model | SR22 | Expiration Date | 09/30/2031 |
| 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) | 51743037 |
| MFR Year | 2016 | Mode S Code (Base 16 / Hex) | A7C61F |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | TVPX AIRCRAFT SOLUTIONS INC TRUSTEE | ||
| Street | 39 E EAGLE RIDGE DR STE 201 | ||
| City | NORTH SALT LAKE | State | UTAH |
| County | DUCHESNE | Zip Code | 84054-2533 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | IO-550-N | Category | Normal |
| A/W Date | 02/23/2023 | 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 | T248955 | Issue Date | 09/09/2024 | Expiration Date | 10/09/2024 |
| Mod Code | 28 | Mod Date | 20160304 |
| INSTALLED TEMPORARY FUEL SYSTEM RESTING ON PLYWOOD SUPPORTING ON EXISTING AIRCRAFT STRUCTURE. PLYWOOD BASE IS INSTALLED TO FACILITATE EVEN LOAD DISTRIBUTION. AIRCRAFT FLOOR LOADING LIMITS ARE NOT EXCEEDEDFERRY SYSTEM CONSISTS OF 2 ALUMINUM TANKS. THE TANKING SYSTEM TOTAL CAPACITY IS 162 U.S. GALLONS. TANKS ARE CONSTRUCTED FROM .090 5052-H34ALUMINUM WELDED AT ALL SEAMS, INTERNAL BAFFLES ARE INSTALLED AND WELDED INTO PLACE. CONSTRUCTION OF TANKS MEETS THE STANDARDS OF U.S. COAST GUARD 33 C.F.R. 183.580 SPECIFICATIONS. TANKS ARE PRESSURE AND LEAK TESTED IN ACCORDANCE WITH FAR 23.965A(1) AT POINT OF MANUFACTURE;WILLIAMS MANUFACTURING, TRACY, CA. ALL TANKS ARE SECURED TO SEAT TRACKS WITH CARGO TIE DOWNS. THESE TIE DOWN STRAPS ARE OF IDENTICAL TYPE THAT HAVE BEEN UTILIZED IN PREVIOUSLY FAA APPROVED TANKING SYSTEMSTRAPS, (2 EACH) SECURE THE TANKS LONGITUDINALLY AND LATERALLY. FERRY FUEL TANKS ARE ELECTRICALLY BONDED TO THE AIRFRAME TO FACILITATE STATIC DISCHARGE,, AND ARE VENTED TO THE ATMOSPHERE, AS OUTLINED IN AC43-13-1B. CHAPTER 11 SECTION 15 PARAGRAPH 11-191 AND CHAPTER 8 SECTION 2 PARAGRAPH 8-33. THE FERRY TANKING SYSTEM IS PLUMBED INTO THEAIRCRAFT FUEL SYSTEM AS NOTED ON THE AIRCRAFT FUEL SYSTEM SCHEMATIC. THIS IS CO-LOCATED WITH, AND IS A PART OF THE FERRY FUEL MANAGEMENT DETAILS LOCATED IN ATTACHMENT 1 OF THE TANKING INSTALLATION PACKAGE. AIRCRAFT FERRY FUEL SYSTEM OPERATION AND MANAGEMENT DETAILS IS OUTLINED IN ATTACHMENT 2. CONTINUOUS AIRWORTHINESS COMPLIANCE NOT APPLICABLE DUE TO TEMPORARY INSTALLATION. | |||
| None |
