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N6TK has Assigned/Multiple Records

N-Number Entered: 6tk Aircraft Description
Serial Number 180-53186 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 06/14/2024
Model 180K Expiration Date 06/30/2031
Type Aircraft Fixed Wing Single-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51742100
MFR Year 1981 Mode S Code (Base 16 / Hex) A7C440
Type Registration Individual Fractional Owner NO
Registered Owner
Name PRITCHARD JAMES A III
Street 415 PARSON CIR
City MAYSVILLE State GEORGIA
County BANKS Zip Code 30558-5025
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 CONT MOTOR Classification Standard
Engine Model O-470 SERIES Category Normal
A/W Date 06/22/1982 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 20140619
INSTALLATION OF ONE FUEL TANK MANUFACTURED BY TURTLE-PAC PTY. LTD. SPECIFICALLY FOR THE AIRCRAFT, 160 GALLON COLLAPSIBLE TURTLE-PAC FUEL BLADDER. DATA FOR ELECTRICAL DETAILS, FUEL SYSTEMS AND STRUCTURAL ASPECTS FOR MAJOR ALTERATION TO THIS AIRCRAFT APPROVED BY JAMES ROGER GRACE (DERT-500725-CE). SEE ATTACHED FAA FORM 8110-3 DATED 10/29/10. A WEIGHT AND BALANCE REV. WAS CALCULATED BASED UPON THE CURRENT W&B REPORT PROVIDED BY QUEST AVIONICS, INC. DATED 5/2/2012. AIRCRAFT WEIGHT AND BALANCE HAS BEEN COMPUTED. IT IS THE RESPONSIBILITY OF THE PILOT IN COMMAND TO ENSURE THAT THE AIRCRAFT IN A LOADED FULLY LOADED CONFIGURATION FALLS WITHIN THE MANUFACTURERS APPROVED CG LIMITS AND THE WEIGHT RESTRICTIONS OF THE AIRCRAFT. A COPY OF THIS 337 SHALL REMAIN ON BOARD THE AIRCRAFT WHILE OPERATING WITH SYSTEM INSTALLED. SYSTEM OPERATIONAL AND LEAK CHECKED SATISFACTORY. THIS SYSTEM IS A TEMPORARY INSTALLATION FOR A RELOCATION FLIGHT AND IS TO BE REMOVED BY AUTHORIZED PERSONNEL UPON COMPLETION OF FERRY FLIGHT.

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