FAA REGISTRY
N-Number Inquiry Results
| Serial Number | LJ-903 | Status | Valid |
| Manufacturer Name | BEECH | Certificate Issue Date | 04/21/2021 |
| Model | C90 | Expiration Date | 04/30/2028 |
| 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) | 51270524 |
| MFR Year | 1980 | Mode S Code (Base 16 / Hex) | A57154 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | DAVIS AVIATION INC | ||
| Street | 200 JETPORT RD | ||
| City | BRANDON | State | MISSISSIPPI |
| County | RANKIN | Zip Code | 39047-7609 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | U/A CANADA | Classification | Standard |
| Engine Model | PT6A SERIES | Category | Normal |
| A/W Date | 04/15/1980 | 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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| Mod Code | 28 | Mod Date | 20130702 |
| THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL SYSTEM, CONSIST ING OF A SINGLE 450 GALLON AEROTEC FUEL BLADDER, 2 FUEL SELECTOR VALVES AND ASSOCIATED FERRY FUEL FEED LINE, FITTINGS AND VENT SYSTEM. THIS SYSTEM IS USED IN CONNECTION WITH AN AN833-6D 90 DEGREE BULKHEAD FITTINGS INSTALLED IN THE LOWER FUSELAGE SIDE PANELS AT STATION 185. THE INSTALLATION OF THE BULKHEAD FITTINGS MUST BE A PREVIOUSLY APPROVED INSTALLATION WITH SEPERATE FORM 337. THE SYSTEM IS REQUIRED TO EXTEND THE RANGE FOR A FLIGHT FROM HONOLULU, HAWAII TO LAS VEGAS, NEVADA. THE INSTALLATION IS TEMPORARY AND SHALL BE REMOVED UPON ARRIVAL AT THE DESTINATION. THIS MAJOR ALTERATION WILL CONSISTS OF REMOVING THE AIRCRAFT PASSENGER SEATS, FURNISHINGS AND EQUIPMENT, AS REQUIRED, FROM THE PASSENGER COMPARTMENT AND INSTALLING A TEMORARY FERRY FUEL SYSTEM IN THE CABIN. THE TEMPORARY FERRY FUEL SYSTEM WILL BE CONNECTED TO THE AIRCRAFT MAIN FUEL SYSTEM. THE FERRY FUEL SYSTEM CONSISTS OF ONE 450 GALLON BLADDER TANK. THE TANK IS A AEROTEC 450 GALLON FUEL BLADDER WITH INTEGRATED TIE DOWN STRAPS. THE TANK IS PRESSURE AND LEAKED CHECKED AS PER PERTINENT FARS. THE TANK IS ELECTRICALLY GROUNDED TO AIRCRAFT STRUCTURE. THE TANK IS COLLAPSIBLE AND DOES NOT REQUIRE VENTING. CABIN PRESSURE WILL PUSH THE TANK FLAT AND TRANSFER FUEL. THE TANK IS MOUNTED ON 1/2 INCH PLYWOOD PALLET. THECABIN TANK IS SECURED WITH (6) 2500 POUND CARGO TIE DOWN STRAPS SECURED TO (12) POINTS OF THE CARGO TIE DOWN RINGS, LOCATED IN THE EXISTING BROWNLINE FLOOR SEAT RAILS. A TWO FUEL SELECTOR VALVE MANIFOLD IS CONSTRUCTED USING 1/2 INCH PIPE FITTINGS AND 3/8 INCH | |||
| Mod Code | 28 | Mod Date | 20141128 |
| THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL SYSTEM, CONSIST ING OF A SINGLE 450 GALLON AEROTEC FUEL BLADDER, 2 FUEL SELECTOR VALVES AND ASSOCIATED FERRY FUEL FEED LINE, FITTINGS AND VENT SYSTEM. THIS SYSTEM IS USED IN CONNECTION WITH AN AN833-6D 90 DEGREE BULKHEAD FITTINGS INSTALLED IN THE LOWER FUSELAGE SIDE PANELS AT STATION 185. THE INSTALLATION OF THE BULKHEAD FITTINGS MUST BE A PREVIOUSLY APPROVED INSTALLATION WITH SEPERATE FORM 337. THE SYSTEM IS REQUIRED TO EXTEND THE RANGE FOR A FLIGHT FROM HONOLULU, HAWAII TO LAS VEGAS, NEVADA. THE INSTALLATION IS TEMPORARY AND SHALL BE REMOVED UPON ARRIVAL AT THE DESTINATION. THIS MAJOR ALTERATION WILL CONSISTS OF REMOVING THE AIRCRAFT PASSENGER SEATS, FURNISHINGS AND EQUIPMENT, AS REQUIRED, FROM THE PASSENGER COMPARTMENT AND INSTALLING A TEMORARY FERRY FUEL SYSTEM IN THE CABIN. THE TEMPORARY FERRY FUEL SYSTEM WILL BE CONNECTED TO THE AIRCRAFT MAIN FUEL SYSTEM. THE FERRY FUEL SYSTEM CONSISTS OF ONE 450 GALLON BLADDER TANK. THE TANK IS A AEROTEC 450 GALLON FUEL BLADDER WITH INTEGRATED TIE DOWN STRAPS. THE TANK IS PRESSURE AND LEAKED CHECKED AS PER PERTINENT FARS. THE TANK IS ELECTRICALLY GROUNDED TO AIRCRAFT STRUCTURE. THE TANK IS COLLAPSIBLE AND DOES NOT REQUIRE VENTING. CABIN PRESSURE WILL PUSH THE TANK FLAT AND TRANSFER FUEL. THE TANK IS MOUNTED ON 1/2 INCH PLYWOOD PALLET. THECABIN TANK IS SECURED WITH (6) 2500 POUND CARGO TIE DOWN STRAPS SECURED TO (12) POINTS OF THE CARGO TIE DOWN RINGS, LOCATED IN THE EXISTING BROWNLINE FLOOR SEAT RAILS. A TWO FUEL SELECTOR VALVE MANIFOLD IS CONSTRUCTED USING 1/2 INCH PIPE FITTINGS AND 3/8 INCH | |||
