FAA REGISTRY
N-Number Inquiry Results
Serial Number | 289 | Status | Valid |
Manufacturer Name | CONSTRUCCIONES AERONAUTICAS SA | Certificate Issue Date | 10/07/2019 |
Model | CASA-212-200 | Expiration Date | 10/31/2029 |
Type Aircraft | Fixed Wing Multi-Engine | Type Engine | Turbo-prop |
Pending Number Change | None | Dealer | No |
Date Change Authorized | None | Mode S Code (base 8 / Oct) | 51753053 |
MFR Year | 1981 | Mode S Code (Base 16 / Hex) | A7D62B |
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 | AIRESEARCH | Classification | Special Flight Permit |
Engine Model | TPE331 SERIES | Category | Delivery or Export, Operate Excess of Maximum Weight |
A/W Date | 02/28/1983 | 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/ |
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Certificate Number | T197583 | Issue Date | 10/07/2019 | Expiration Date | 11/06/2019 |
Mod Code | 28 | Mod Date | 19951212 |
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON MAY 26, 1995, AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION INC DRAWINGS AF-CA-212-II, AF-C-A212-OI, AF-CA- 212-ID, AND THE FOLLOWING FUEL TANK DRAWINGS AF-TYP: 205,205,205. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT ANDTHE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHTEXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUA- TION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HASBEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FORACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. |
None |