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N401MC has Assigned/Multiple Records

N-Number Entered: 401mc Aircraft Description
Serial Number LA-145 Status Valid
Manufacturer Name BEECH Certificate Issue Date 02/26/2023
Model F90 Expiration Date 02/28/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51130556
MFR Year 1981 Mode S Code (Base 16 / Hex) A4B16E
Type Registration LLC Fractional Owner NO
Registered Owner
Name SKY CHARTER LLC
Street 62512 AIRPORT RD BLDG 16
City SLIDELL State LOUISIANA
County ST TAMMANY Zip Code 70460-5282
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 U/A CANADA Classification Standard
Engine Model PT6A SERIES Category Normal
A/W Date 07/29/1981 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 19911205
THE AIRCRAFT HAS BEEN FITTED WITH AN AUXILIARY FERRY FUEL SYSTEM TO ENABLE DELIVERY TO ANCHORAGE ALASKA. THREE ALUMINUM TANKS WITH A TOTAL CAPACITY OF 270 GAL ARE SECURED TO THE AIRCRAFT SEAT TRACKS WITHCARGO STRAPS. THE TANKS HAVE BEEN PRESSURE TESTED TO 5.5 PSI. THE TANKS ARE VENTED TO THE ATMOSPHERE THROUGH AN EXISTING AIRFRAME VENT AAND IN ACCORDANCE WITH FAR AC.43.13-1A, CHAPTER 14, SECTION 2. THE FERRY FUEL SYSTEM IS PLUMBED INTO EXISTING AIRCRAFT SYSTEM AS SHOWN IN ATTACHMENT 1. OPERATION OF THE FERRY FUEL SYSTEM IS DETAILED IN SAMEATTACHMENT. THE MAXIMUM WEIGHT OF THE AIRCRAFT IN THE FERRY CONFIGU- RATION DOES NOT EXCEED 110% OF THE NORMAL CERTIFICATED GW. THE CG REMAINS WITHIN NORMAL LIMITS.

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