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N405MN has Assigned/Multiple Records

N-Number Entered: 405mn Aircraft Description
Serial Number 405 Status Valid
Manufacturer Name PILATUS Certificate Issue Date 07/18/2017
Model PC-12/45 Expiration Date 07/31/2027
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) 51140124
MFR Year 2001 Mode S Code (Base 16 / Hex) A4C054
Type Registration Corporation Fractional Owner NO
Registered Owner
Name BANK OF UTAH TRUSTEE
Street 50 S 200 E STE 110
City SALT LAKE CITY State UTAH
County SALT LAKE Zip Code 84111-1617
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-67B Category Normal
A/W Date 09/19/2011 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
Certificate Number T174779 Issue Date 07/18/2017 Expiration Date 08/17/2017
Fuel Modifications
Mod Code 28 Mod Date 19960726
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-PA23-II, AF-PA23-ID, AF-PA23-FS, AF-PA23-OI, AND THE FOLLOWING FUEL TANK DRAWING(S) AF-TYP: 75,75. A NEW WEIGHT AND BALANCEHAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND AIRCRAFT IS WITHIN THEWEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAX. CERTIFI- CATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVENAMED DRAWINGS, OPERATED PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASSHAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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