FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 208B2392 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 08/20/2019 |
| Model | 208B | Expiration Date | 08/31/2029 |
| Type Aircraft | Fixed Wing Single-Engine | Type Engine | Turbo-prop |
| Pending Number Change | None | Dealer | No |
| Date Change Authorized | None | Mode S Code (base 8 / Oct) | 52675335 |
| MFR Year | 2013 | Mode S Code (Base 16 / Hex) | AB7ADD |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | BANK OF UTAH TRUSTEE | ||
| Street | 50 S 200 E STE 110 | ||
| City | SALT LAKE CITY | State | UTAH |
| County | SALT LAKE | Zip Code | 84111-1617 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | P&W CANADA | Classification | Standard |
| Engine Model | PT6A-114A | Category | Normal |
| A/W Date | 03/16/2013 | 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 | T227253 | Issue Date | 06/24/2022 | Expiration Date | 07/24/2022 |
| Mod Code | 28 | Mod Date | 20160429 |
| THIS MAJOR ALTERATION IS A TEMPORAY INSTALLATION OF 529 GALLON TURTLE PAC F FERRY FUEL BLADDER, RESTRICTED TO 480 GALLONS, IN THE CABIN AND A DUAL PUMP TRANSFER SYSTEM TO PUMP FERRY FUEL TO THE LEFT MAIN TANK. THE SYSTEM IS INSTALLED FOR A ONE TIME FERRY FLIGHT FROM KAILUA, KONA HAWAII PHKO TO NORTH LAS VEGAS, NEVADA. OPERATION WITH THIS TEMPORARY SYSTEM INSTALLED REQUIRES A SPECIAL FLIGHT PERMIT. THE FERRY FUEL SYSTEM IS INSTALLED IN ACCORDANCE WITH FLIGHT CONTRACT SERVICES, INC. CESSNA 208 SERIES FERRY FUEL SYSTEM INSTALLATION/REMOVAL INSTRUCTIONS AND ICA-SINGLE BLADDER SYSTEM. FLIGHT CONTRACT SERVICES, INC. DOCUMENTNUMBER 208B042016-01 (16 PAGES) ATTACHED HERETO THIS FORM. SYSTEM SHALL BE REMOVED UPON ARRIVAL AT THE DESTINATION, PRIOR TO RETURNING THE AIRCRAFT TO SERVICE. | |||
| Mod Code | 28 | Mod Date | 20130405 |
| THIS MAJOR ALTERATION IS A TEMPORARY INSTALLATION OF 529 GALLON TURTLEPAC F FERRY FUEL BLADDER, RESTRICTED TO 480 GALLONS, IN THE CABIN AND DUAL PUMP TRANSFER SYSTEM TO PUMP FERRY FUEL TO THE LEFT MAIN TANK. THIS MAJOR ALTERATION IS A TEMPORARY INSTALLATION AND WILL CONSIST OF REMOVING THE REQUIRED AIRCRAFT SEATS, FURNISHINGS AND EQUIPMENT FROM THE PASSENGER COMPARTMENTS AND INSTALLING A TEMPORARY FERRY FUEL SYSTEM IN THE CABIN. THE TEMPORARY FERRY FUEL SYSTEM WILL BE CONNECTEDTO THE AIRCRAFT THROUGH A DUAL MALLORY HIGH CAPACITY DIESEL ELECTRIC PUMP SYSTEM TO THE LEFT MAIN FUEL TANK. THE FUEL PUMPS ALSO HAVE THEIROWN 12 VOLT BATTERY BACKUP POWER. THE FERRY FUEL TANK IS A 529 GALLON TURTLE PAC FERRY FUEL BLADDER, RESTRICTED AS REQUIRED BY WEIGHT AND BALANCE TO 480 GALLONS. NOTE: FOR SERVICEABLE TANKS SEE SPECIAL INSPECTION SECTION 9.0 INSTRUCTIONS. THE TANK IS A THICK WALL TURTLE PAC TANK, MANUFACTURED IN AUSTRALIA FOR FERRY FUEL SYSTEM INSTALLATIONSEE TURTLE PAC WEBSITE FOR DOCUMENTATION AND SPECIFICATIONS. THE TANK IS MOUNTED ON A PLYWOOD PALLET AND GROUNDED TO THE AIRCRAFT STRUCTURE.THE TEMPORARY WEIGHT AND BALANCE WILL SPECIFY AIRCRAFT ITEMS TO BE REMOVED AND THE LOCATION OF THE FUEL TANK AND SPECIFIC QUANTITIES FOR SERVICING. THE TANK SHALL BE SECURED IN THE CABIN IN ACCORDANCE WITH ATTACHED DRAWINGS AND DATA FROM THE CESSNA 208 OPERATING MANUAL, WEIGHT AND BALANCE AND LOADING SECTION. THE FUEL TANK IS PLACARDED WITH QUANTITIES AND SYSTEM OPERATING INSTRUCTIONS. THE FUEL PUMPS ARE POWERED THROUGH THE SECONDARY AVIONICS LOWER BUS BAR AND A 24/12 VOLT POWER CONVERTER AND PROTECTED BY TWO 20 AMP FUSES ON BOTH SIDES OF THEPOWER CONVERTER. THE PUMPS ARE FREE-FLOW THROUGH PUMPS AND HAVE CHECK | |||
