FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 208B1084 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 08/31/2024 |
| Model | 208B | Expiration Date | 08/31/2031 |
| 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) | 51472525 |
| MFR Year | 2004 | Mode S Code (Base 16 / Hex) | A67555 |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | DOG IS MY COPILOT INC | ||
| Street | PO BOX 3399 | ||
| City | JACKSON | State | WYOMING |
| County | TETON | Zip Code | 83001-3399 |
| 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 | 06/02/2012 | 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 | 20140219 |
| INSTALLED TEMPORARY FUEL SYSTEM CONSISTING OF 4 ALUMINUM FUEL TANKS, FUEL VALVE MANIFOLD, TWO 24 VOLT ELECTRIC FUEL TRANSFER PUMPS, AND ASSOCIATED FUEL LINES IAW ATTACHED FUEL SYSTEM DRAWING LABELED "CARAVAN FUEL SYSTEM DRAWIN #1". TANKS ARE INSTALLED IN THE CABIN AREAON A RECK CONSISTING OF 2X4 AND 1/2" PLYWOOD BASES FOR EVEN LOAD DISTRIBRUTION. TANKS ARE GROUNDED TO AIRFRAME FOR STATIC DISCHARGE. TANKS ARE RECTANGULAR, INTERNALLY BAFFLED, CONSTRUCTED FROM WELDED 5052 ALUMINUM .100 INCH THICK AND PRESSURE TESTED IAW FAR 23.965(A)1. THE TANKS ARE SECURED FOR AND AFT AND VERTICALLY TO THE PASSENGER CABIN INBOARD, MIDDLE,AND OUTBOARD SEAT RAILS USING AIRCRAFT TIE-DOWN RINGS AND 4 CARGO STRAPS OF 3000 POUNDS TENSILE STRENGTH AND CONFORMING TO TSO C22. THE TANKS ARE SUPPORTED LATERALLY BY CONTACT WITH THE AIRCRAFT SIDE STRUCTURE AND PROTECTED BY INTERIOR UPHOLSTERY AND VINYL PADDING. THE FERRY FUEL SYSTEM T'S INTO THE AIRCRAFT FUEL SYSTEM BY INSTALLATION OF A T IN THE AIRCRAFT FUEL TANK BALANCE FUEL VENT LINE LOCATED IN THE RIGHT WING ROOT. THE INSTALLATION DOES NOT INTERFERE WITH THE NORMAL FUEL TANK CROSS VENTING. ALL FITTINGS ARE #8OR LARGER AND FUEL AND OIL TOLERANT HOSE I USED THROUGHOUT THE INSTALLATION. FERRY FUEL SELECTOR MANIFOLD AND 2 TSO'ED AIRBORNE FUEL PUMPS ARE MOUNTED BESIDE THE PILOTS SEAT. EACH PUMP IS CAPABLE OF DELIVERY OF ENOUGH FUEL FOR CONTINUED FLIGHT. POWER FOR THE FUEL PUMPSIS TAKEN FROM THE MAIN BATTERY BUSS AND PROTECTED THROUGH A TEMPORARY 30 AMP FUSE AND SEPERATE 10 AMP FUEL PUMP CIRCUIT BREAKERS, ALL ACCESSIBLE TO THE PILOT IN FLIGHT. FERRY FUEL SYSTEM IS VENTED TO THE EXTERIOR OF THE AIRCRAFT THROUGH A TEMPORARY VENT PROTRUDING THROUGH | |||
| Mod Code | 28 | Mod Date | 20120607 |
| INSTALLED FOUR ALUMINUM FERRY FUEL TANKS, FUEL VALVE MANIFOLD, AND ASSOCIATED FUEL LINES IAW ATTACHED DRAWING. TANKS ARE INSTALLED IN PASSENGER CABIN ON 1/2" PLYWOOD BASED FOR LOAD DISTRIBUTION AND FLOOR PROTECTION. ALL TANKS ARE ELECTRICALLY BONDED ON THE AIRFRAME. TANKS ARE CONSTRUCTED OF 5052 ALUMINUM,.100" THICK. TNAKS ARE INTERNALLY BAFFLED. TANKS HAVE BEEN PRESSURE TESTED IAW FAR 23.965 A (1). TANKS ARE SECURED TO PASSENGER SEAT RAILS USING FAA APPROVED TIE DOWN RINGS AND RATCHET STRAPS MEETING THE STANDARDS OF FAA TSO C22. FLOOR LOADINGLIMITS ARE NOT EXCEEDED. TANKS ARE SECURED FORE AND AFT AND VERTICALLYBY THE POISTIONING OF THE RATCHET STRAPS, AND LATERALLY BY THE CABIN WALLS. FERRY TANK VENTING IS PROVIDED BY ATTACHMENT TO A VENT TUBE SYSTEM EXTENDING IN OT THE RIGHT WING ROOT LOWER INNER PANEL AREA TO ADRILLED HOLE, AND THENCE THROUGH THE PANEL INTO THE SLIPSTRAM IN AN ORIENTATION CAUSING A PRESSURE VENTING PROCESS. THE DRILLED VENT TUBE HOLE SHALL BE REPAIRED BY INSTALLATION OF AN APPROPRIATE AN BOLT NUT, AND WASHERS WHEN FERRY VENT SYSTEM IS REMOVED. THER IS NO TANK VENTINGINTO THE AIRCRAFT FUSELAGE.THE FERRY FUEL SYSTEM T'S INTO THE AIRCRAFTFUEL SYSTEM BY REMOVAL OF THE AIRCRAFT FUEL TANK PRESSURE EQUALIZER VENT TUBE IN THE RIGHT WING ROOT. THIS TUBE IS REPLACED WITH A T ALLOWING PUMPING OF AUX FUEL FORM THE AUX TANKS INTO THE PRESSURE EQUALIZER CROSS VENT. FUEL IS THENCE TRANSFERRED TO EACH TANK. AIRCRAFT NORMAL TANK EXTERNAL VENTING IS NOT NEGATIVELY AFFECTED, AND CROSS VENTING IS MAINTAINED. THE FERRY FULE PUMPS AND TANK VALVE SELECTOR MANIFOLD IS LOCATED BETWEEN THE PILOT SEATS WITHIN RACH OF THE PILOT. THE FERRY FUEL PUMPS ARE POWERED BY A #8 WIRE CONNECTED TO | |||
