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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N9MN is Assigned

N-Number Entered: 9mn Aircraft Description
Serial Number 414-0851 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 03/20/2023
Model 414 Expiration Date 03/31/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 53065632
MFR Year None Mode S Code (Base 16 / Hex) AC6B9A
Type Registration LLC Fractional Owner NO
Registered Owner
Name 15 POINT LLC
Street 3 N EARL AVE
City LAFAYETTE State INDIANA
County TIPPECANOE Zip Code 47904-2812
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 Unknown Classification Standard
Engine Model Unknown Category Normal
A/W Date 12/01/1976 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 19920608
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON JUNE 7, 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-400-II, AF-CE-400-2, AF-CE-400-1, AF-CE-400-1A AND THE FOLLOWING FUEL TNAK DRAWINGS-AF-TYP-15-C3. 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 IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCEWITH HE ABOVE NAMED DRAWINGS, OPERATED RPOPERLY AND DOES NOT LEAK. THEMAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HA BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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