FAA REGISTRY
N-Number Inquiry Results
Serial Number | 766 | Status | Valid |
Manufacturer Name | AGUSTA SPA | Certificate Issue Date | 11/04/2022 |
Model | F.260D | Expiration Date | 11/30/2029 |
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) | 50713041 |
MFR Year | 1991 | Mode S Code (Base 16 / Hex) | A39621 |
Type Registration | LLC | Fractional Owner | NO |
Name | AEROSPACE TRUST MANAGEMENT LLC TRUSTEE | ||
Street | 1013 CENTRE RD STE 403A | ||
City | WILMINGTON | State | DELAWARE |
County | NEW CASTLE | Zip Code | 19805-1270 |
Country | UNITED STATES |
Type Certificate Data Sheet | None | Type Certificate Holder | None |
Engine Manufacturer | LYCOMING | Classification | Special Flight Permit |
Engine Model | 0-540 SERIES | Category | Operate Excess of Maximum Weight |
A/W Date | 06/23/1998 | 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 | T245011 | Issue Date | 05/21/2024 | Expiration Date | 06/20/2024 |
Mod Code | 28 | Mod Date | 20080925 |
AUGUSTA SIAI TEMPORARY AUXILIARY FUEL SYSTEM KIT #260-16-92-503 INSTALLED IN REAR CABIN. SYSTEM CONSISTS OF A 32 U.S. GALLON TANK MOUNTED INTO THE REAR SEAT STRUCTURE. TANK IS RESTRAINED USING EXISTING SEAT BELT AND SHOULDER HARNESS POINTS AND IS PLUMBED INTO THEAIRCRAFT FUEL SYSTEM USING MILL-H-6000 HOSE AND 2052-0-6 TUBING INCORPORATING A PILOT OPERATED SHUT-OFF VALVE. INSTALLATION CONFORMS TO STANDARDS OF FAA 43.13-1B & 2B. TANK IS PLACARDED REFLECTING 32 U.S. GALLONS OF 91/96 MINIMUM OCTANE FUEL. TO OPERATE THE SYSTEM THE FOLLOWING LIMITATIONS APPLY: ALL TAKE-OFFS AND LANDINGS ARE TO BE MADE ON MAIN WING TANKS. AUXILIARY FUEL SYSTEM TO BE USED IN LEVEL CRUISE FLIGHT ONLY. SMOKING IS PROHIBITED WITH AUXILIARY FUEL SYSTEM INSTALLED. IN THE EVENT OF AUX FUEL SYSTEM LEAKAGE, TURN OFF ALL UNNECESSARY ELECTRICAL CIRCUITS. INSTRUCTIONS TO BEGIN AND TERMINATE AUXILIARY FUEL SYSTEM OPERATION IS INCLUDED ON 337. MAINTENANCE FOR CONTINUED AIRWORTHINESS OF THIS INSTALLATION WILL INCLUDE MONITORING THE TANK FOR SECURITY, LEAKAGE AND PROPER OPERATION IN ACCORDANCE WITHTHE SCOPE AND DETAIL OF FAR PART 43, APPENDIX D. THIS FORM 337 MUST REMAIN IN THE AIRCRAFT AS A SUPPLEMENT OF THE AIRCRAFT FLIGHT MANUAL DURING ALL FLIGHT OPERATIONS. |
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