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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N13188 is Assigned

N-Number Entered: 13188 Aircraft Description
Serial Number 17262557 Status Cert Terminated
Manufacturer Name CESSNA Certificate Issue Date None
Model 172M Expiration Date None
Type Aircraft Fixed Wing Single-Engine Type Engine 4 Cycle
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50101171
MFR Year 1973 Mode S Code (Base 16 / Hex) A08279
Type Registration Individual Fractional Owner NO
Registered Owner
Name SALE REPORTED
Street SONNENHILGELWEG 2A
City OBERUZWIL State
County Zip Code 9242
Country SWITZERLAND
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 LYCOMING Classification Standard
Engine Model 0-320 SERIES Category Normal
A/W Date 11/17/1973 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
SOLD TO DUNKL STEVEN ROBERT
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 19920518
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON JUNE 10, 1988, AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-CE-100/200 II, AF-CE-100/200-2, AF-CE-100-2, AF--C-100/200-3-ID, AF-C-100/200-2-ID AND THE FOLLOWING FUEL TANK DRAWINGS AF-TYP-124. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT, AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATED PROPERLY AND DOES NOT LEAK. THE MAG- NETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURN-ISHED FUEL MANAGEMENT INSTRUCTIONS.

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