FAA REGISTRY
N-Number Inquiry Results
| Serial Number | 208B1149 | Status | Valid |
| Manufacturer Name | CESSNA | Certificate Issue Date | 05/09/2023 |
| Model | 208B | Expiration Date | 05/31/2030 |
| 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) | 52351566 |
| MFR Year | 2005 | Mode S Code (Base 16 / Hex) | A9D376 |
| 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 CANADA | Classification | Standard |
| Engine Model | PT6A-114A | Category | Normal |
| A/W Date | 06/07/2018 | 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 |
| None |
| Mod Code | 28 | Mod Date | 20110714 |
| INSTALLED TEMPORARY AUXILIARY LONG RANGE FUEL TANKS IN ACCORDANCE WITHWINGS OF EAGLES INSTALLATION MANUAL WOE 208IM DATED 1/27/2003, DRAWINGNO. WOE 208-1 DATED 08/20/2002, WOE 3001 DATED 08/20/2002, WOE 208FL DATED 08/20/2002, WOE 208VT SHEETS 1,2 DATED 08-20-2002 WOE 200A SHEET 1 DATED 08/20/2002, WOE 250A SHEET 1 DATED 08/20/2002, WOE 250-1SHEET 2 DATED 08/20/2002, WOE 200A SHEET 4 DATE 8/20/2002, WOE 300IPF SHEET 8 DATED 08/20/2002, WOE6032 DATED 1/15/08, WOE208-2 SHEET 1,2,3,4 DATED 1/15/08 ANDAC-43-13-1B AND INDUSTRY PRACTICES PERTAINING TO HARDWARE AND FITTINGS. AUX TANKS HAVE BEEN PRESSURE TESTED TO 3.5 PSI AND FOUND TO BE SATISFACTORY FOR THE INTENDED INSTALLATION. STRUCTURALSUBSTANTIATION WAS PROVIDED IN REPORT WOE 02-06 DATED JUNE 2002 AND APPROVED BY 8110-3 DATED JUNE 9, 2002 BY DERT510375-CE AND INSTALLATION MANUAL ENGINEERING CHANGES PER WOE 208EC DATED 03/03/2008AND STRUCTUAL SUBSTANTIATION PROVIDED IN REPORT WOE 08-01 APPROVED BY 8110-3 DATED 4 MARCH 2008 BY DERT510375-CE. THE NEW WEIGHT AND BALANCEWAS COMPUTED AND PROVIDED TO THE PILOT. THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS IN ACCORDANCE WITH WICHITA ACO LETTER OF AUTHORIZATION DATED 04/04/2008. THE FUEL SYSTEM HAS BEEN OPERATIONALLYCHECKED AND THE ENGINE RUNS ON ALL TANKS. THE FUEL SYSTEM HAS BEEN OPERATIONALLLY CHECKED AND DOES NOT LEAK. THE PILOT HAS BEEN PROVIDED WITH AN "AIRPLANE AUXILIARY FUEL SYSTEM INSTRUCTIONS" BOOKLET FOR THE PROPER OPERATION OF THE AUXILIARY FUEL SYSTEM. UPON ARRIVAL AT THE DESTINATION LISTED ON THE FAA FORM 8130-7 FERRY PERMIT, THIS FIELD APPROVAL EXPIRES AND IS VOID. THE AIRCRAFT MUST BE RETURNED TO SERVICEAND THE AUXILIARY FUEL SYSTEM REMOVED IN ACCORDANCE TO THE ATTACHED | |||
