FAA REGISTRY
N-Number Inquiry Results
Serial Number | 21064697 | Status | Valid |
Manufacturer Name | CESSNA | Certificate Issue Date | 08/12/2010 |
Model | T210N | Expiration Date | 01/31/2028 |
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) | 52533446 |
MFR Year | 1982 | Mode S Code (Base 16 / Hex) | AAB726 |
Type Registration | LLC | Fractional Owner | NO |
Name | BACH II LLC | ||
Street | 621 DUHON RD | ||
City | LAFAYETTE | State | LOUISIANA |
County | LAFAYETTE | Zip Code | 70506-7605 |
Country | UNITED STATES |
Type Certificate Data Sheet | None | Type Certificate Holder | None |
Engine Manufacturer | CONT MOTOR | Classification | Standard |
Engine Model | TSIO-520 SER | Category | Normal |
A/W Date | 04/01/1982 | 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 |
Certificate Number | T241181 | Issue Date | 11/01/2024 | Expiration Date | 12/01/2024 |
Mod Code | 28 | Mod Date | 19920728 |
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON JUNE 10, 1988 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-CE-100/200-VRII, AF-CE-100/200-1, AF-C-100/200-1, AF-C-100/200-3-ID, AF-C-100/200-2-ID AND THE FOLLOWING FUEL TANK DRAWINGS - AF-TYP:-100. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT, AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDXS 110% OF THE MAXIMUM CERTIF-ICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACOIS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATED PROPERLY AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. |