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N-Number Inquiry Results

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N208DE is Assigned

N-Number Entered: 208de Aircraft Description
Serial Number 208B0502 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 09/06/2016
Model 208B Expiration Date 09/30/2029
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) 50330013
MFR Year 1996 Mode S Code (Base 16 / Hex) A1B00B
Type Registration Individual Fractional Owner NO
Registered Owner
Name EVANS DAVID J
Street 10190 BAYOU GULCH RD
City PARKER State COLORADO
County DOUGLAS Zip Code 80134-5160
Country UNITED STATES
Airworthiness INFORMATION PROVIDED HERE SHOULD NOT BE USED TO DETERMINE THE AIRWORTHINESS OF AN AIRCRAFT.
Refer to 14 CFR Parts 39, 43, 91, and FAA Order 8130.2 for airworthiness regulations and guidance.
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 08/29/2007 Exception Code No
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/
Other Owner Names
None
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 19960129
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-CE-100/200 II, AF-CE-100/200-2, AF-CE-100-2, AF-CE-100/200-3-ID, AF-C-100/200-2-ID AND THE FOLLOWING FUEL TANK DRAWINGS AF- TYP: 205,205. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IFTHE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FORM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATED PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MGMT INSTRUCTIONS.

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