FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 208B5075 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 02/04/2020 |
| Model | 208B | Expiration Date | 02/28/2027 |
| 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) | 52715356 |
| MFR Year | 2013 | Mode S Code (Base 16 / Hex) | AB9AEE |
| Type Registration | LLC | Fractional Owner | NO |
| Name | SOUTHERN AIRWAYS PACIFIC LLC | ||
| Street | 101 N RIVERSIDE DR STE 211 | ||
| City | POMPANO BEACH | State | FLORIDA |
| County | BROWARD | Zip Code | 33062-5011 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | P&W CANADA | Classification | Standard |
| Engine Model | PT6A-140 | Category | Normal |
| A/W Date | 11/10/2013 | 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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| Mod Code | 28 | Mod Date | 20170528 |
| INSTALLED TEMPORARY FUEL SYSTEM CONSISTING OF (4) FOUR ALUMINUM FERRY TANKS, FUEL VALVE MANIFOLD, (2) TWO 24 VOLT ELECTRONIC TRNASFER PUMPS,AND ASSOCIATED FUEL LINES IAW ENCLOSED DRAWINGS LABLED (CARAVAN FERRY FUEL DRAWING #1) TANKS ARE INSTALLED IN THE CABIN AREA ON A RACK CONSISTING OF 2X4 AND 1/2 INCH PLYWOOD BASE FOR EVEN LOAD DISTRIBUTIONTANKS ARE GROUNDED TO THE AIRFRAME FOR STATIC DISCHARGE, TANKS ARE RECTANGULAR , BAFFELED INTERNALLY, CONSTRUCTED OF WELDED 5052 ALUMINUM100" THOUSANDS THICK AND PRESSURE TESTED IAW FAR 23.965A(1). THE TANKSARE SECURED FOR AND AFT AND VERTICALLY TO THE PASSENGERS INBOARD MIDDLE AND OUTBOARD SEAT TRACKS USING AIRCRAFT TIE-DOWN RINGS AND (4) FOUR 3000# LB RATING CARGO STRAPS MEETING OR EXCEEDING FAA TSO C22. THE TANKS ARE SUPPORTED LATERALLY BY AIRCRAFT SIDE STRUCTURE AND ARE PROTECTED USING SOFT VINYL PADDING. THE FERRY FUEL SYSTEM IS PLUMBED INTO THE AIRCRAFT FUEL SYSTEM BY INSTALLATION OF A "T" IN THE INTER- TANK EQUALIZER VENT TUBE IN THE RIGHT WING ROOT. THIS INSTALLATION DOES NOT HAMPER VENTING OF THE AIRCRAFT FUEL SYSTEM. ALL FEED FITTINGSAND HOSES ARE 1/2" AND FUEL TOLERANT HOSE IS USED THROUGHOUT FERRY FUEL MANIFOLD AND TSO'D AIRBORNE ELECTRONIC PUMPS ARE MOUNTED BESIDE THE PILOT SEAT. EACH PUMP IS CAPABLE OF DELIVERING ENOUGH FUEL FOR CONTINUED FLIGHT. POWER FOR THE FUEL PUMPS IS TAKEN FROM THE AIRCRAFT MAIN BATTERY BUS AND PROTECTED BY TEMPORARY MAIN 30 AMP FUSE AND SEPERATE 5 AMP CIRCUT BREAKERS. ALL ACCESSIBLE TO THE PILOT IN FLIGHT.THE FERRY FUEL SYSTEM IS VENTED TO THE EXTERIOR OF THE AIRCRAFT THROUGH A TEMPORARY ENT PROTRUDING BENEATH THE RIGHT WING AND SUPPLYING RAM AIR TO THE TANK SYSTEM. A PLACARD FOR OPERATION OF THE | |||
| Mod Code | 28 | Mod Date | 20131213 |
| THIS MAJOR ALTERATION IS A TEMPORARY INSTALLATION AND WILL CONSIST OF RMOVING THE REQUIRES AIRCRAFT SEAT, FURNISHINGS AND EQUIPMENT FROM THEPASSENGER COMPARTMENT AN INSTALLING A TEMPORARY FERRY FUEL SYSTEM IN THE CABIN. THE TEMPORARY FERRY FUEL SYSTEM WILL BE CONNECTED TO THE AIRCRAFT THROUGH A DUAL MALLORY HIGH CAPACITY DIESEL ELECTRIC PUMP SYSTEM TO THE LEFT MAIN FUEL TANK. THE FUEL PUMPS ASLO HAVE THIER OWN 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 TAK 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 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 VALVE AUTHORITY IN ONE DIRECTION. THERE IS A FERRY TANK SELECTOR VALVEAND A FERRY SYSTEM SUPPLY VALVE USED TO CONTROL THE FERRY SYSTEM. THIS IS A TEMPORARY INSTALLATION THAT REQUIRES A SPECIAL FLIGHT PERMIT | |||
