FAA REGISTRY
N-Number Inquiry Results
| Serial Number | CE-141 | Status | Valid |
| Manufacturer Name | BEECH | Certificate Issue Date | 01/12/2015 |
| Model | 35-C33A | 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) | 50060715 |
| MFR Year | 1967 | Mode S Code (Base 16 / Hex) | A061CD |
| Type Registration | LLC | Fractional Owner | NO |
| Name | BONANZA LLC | ||
| Street | 603 RIDGEWOOD RD | ||
| City | HUNTINGTON | State | WEST VIRGINIA |
| County | CABELL | Zip Code | 25701-4851 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | CONT MOTOR | Classification | Standard |
| Engine Model | IO 520 SERIES | Category | Utility |
| A/W Date | 01/19/1967 | 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 | T241714 | Issue Date | 02/16/2024 | Expiration Date | 03/17/2024 |
| Mod Code | 28 | Mod Date | 19960715 |
| INSTALLED ONE 70.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANKS WERE INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI BTD066, NAI TF001, NAI TF002, NAI PS002, NAI V012, NAI M005, NAI SG001 AND THE INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS C33A-KIT. TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM IN THE REAR PASSENGER SEAT LOCATION. TEMPORARY TANK IS SECURED TO THE AIRFRAME WITH 1000 LBS LOAD HUGGER STRAPS IN THE REAR, AND THE FRONT CENTER SEAT BELT ATTACH POINTS FOR THE FRONT. TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. TEMPO- RARY TANK IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE RH WING TANK AND THE AIRCRAFT FUEL SELECTOR VALVE BY ON-OFF VALVES, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. TEMPORARY TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITH THE LINE FORWARD FOR POSITIVE TANK PRESSURE. THE TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THE TIME FO INSTAL-LATION AND WAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO. | |||
