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N-Number Inquiry Results

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N106RF is Assigned

N-Number Entered: 106rf Aircraft Description
Serial Number 208B0481 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 03/04/2023
Model 208B Expiration Date 03/31/2030
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) 50016173
MFR Year 1995 Mode S Code (Base 16 / Hex) A01C7B
Type Registration LLC Fractional Owner NO
Registered Owner
Name RANDIGO LLC
Street 3200 KIRKWOOD HWY # 1093
City WILMINGTON State DELAWARE
County NEW CASTLE Zip Code 19808-6153
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-Restricted
Engine Model PT6A-114A Category Aerial Surveying, Aerial Advertising, Agriculture and Pest Control
A/W Date 04/10/2024 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 19981218
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 ON 9-26-96 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-208-OI, AF-CE-208-FS, AF-CE-208-ID, AF-CE-208-ID-2,AF-CE-208-II, AND AF-TYP(S) 205,205. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURALEVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 1/19/99.

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