FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 208B0996 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 06/16/2023 |
| Model | 208B | Expiration Date | 06/30/2030 |
| 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) | 52761176 |
| MFR Year | 2002 | Mode S Code (Base 16 / Hex) | ABE27E |
| Type Registration | Corporation | Fractional Owner | NO |
| Name | SCHUMAN CARRIAGE CO LTD | ||
| Street | 130 IOLANA PL | ||
| City | HONOLULU | State | HAWAII |
| County | HONOLULU | Zip Code | 96819-1840 |
| Country | UNITED STATES | ||
| Type Certificate Data Sheet | None | Type Certificate Holder | None |
| Engine Manufacturer | P&W | Classification | Standard |
| Engine Model | PT6A SER | Category | Normal |
| A/W Date | 11/14/2002 | 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 |
| Mod Code | 28 | Mod Date | 20080407 |
| INSTALLED TEMPORARY FERRY FUEL SYSTEM CONSISTING OF (?) ALUMINUM FERRYFUEL TANKS, FUEL VALVE MANIFOLD, PUMPS AND ASSOCIATED LINES IAW LEAHY AVIATION CESSNA 208 SERIES DATA. TANKS ARE INSTALLED IN THE CABIN AREA ON A 2X4" & 3/8" PLYWOOD BASE FOR EVEN LOAD DISTRIBUTION. TANKS ARE GROUNDED TO AIRFRAME FOR STATIC DISCHARGE. TANKS ARE RECTANGULAR,INTERNALLY BAFFLED, CONSTRUCTED FROM 5052 ALUMINUM 0.100" THICK AND PRESSURE TESTED (IAW FAR 23.965A(1). FORWARD THE TANKS ARE SECURED TOPASSENGER'S INBOARD, MIDDLE & OUTBOARD SEAT TRACKS VIA TIE DOWN RINGS AND 10000 POUND CARGO STRAPS. AFT THE TANKS ARE SECURED TO AIRCRAFT SEAT TRACKS CROSSWAYS & AFT. TANKS ARE SECURED USING 10000 POUND CARGO STRAPS MEETING OR EXCEEDING THE MATERIAL REQUIREMENTS OF FAA TSO C22. FLOOR LOADING LIMITS ARE NOT EXCEEDED. FERRY FUEL SYSTEM TEES INTO AIRCARFT FUEL SYSTEM BETWEEN AIRCRAFT FUEL TANK BALANCE LINEALL FITTINGS ARE NO. 8 OR LARGER AND PARKER FUEL HOSE USED THROUGHOUT THE FERRY FUEL SYSTEM. FERRY FUEL MANIFOLD AND TSO'D WELDON FUEL PUMPS ARE MOUNTED BEHIND PILOT'S AND CO-PILOT'S SEATS. FUEL PUMP POWER IS TAKEN FROM AIRCRAFT BUSS 2 WITH INDIVIDUAL 5 AMP CIRCUIT PRO-TECTION. FERRY FUEL SYSTEM USES A RAM AIR VENT TO PROVIDE EXTERNAL VENTING AS WELL AS PROVIDE A POSITIVE PRESSURE TO AID THE FLOW OF FERRY FUEL. FERRY FUEL SYSTEM GROUND CHECKED. FERRY FUEL SYSTEM TO BE FLIGHT TESTED AND RESULTS ENTERED IN AIRCRAFT RECORDS. SYSTEM MUSTBE OPERATED IAW THE OPERATING INSTRUCTIONS AND OPERATING LIMITS OF THESPECIAL FLIGHT PERMIT. FERRY SYSTEM OPERATIONALLY CHECKED AND FOUND SAFE FOR INTENDED OPERATION. LOGBOOK ENTRIES MADE. | |||
