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N912MN is Assigned

N-Number Entered: 912mn Aircraft Description
Serial Number BB1468 Status Valid
Manufacturer Name BEECH Certificate Issue Date 07/19/2013
Model B200 Expiration Date 07/31/2029
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) 53117471
MFR Year 1993 Mode S Code (Base 16 / Hex) AC9F39
Type Registration Corporation Fractional Owner NO
Registered Owner
Name AVERA MCKENNAN
Street C/O CAREFLIGHT
1325 S CLIFF AVE
City SIOUX FALLS State SOUTH DAKOTA
County MINNEHAHA Zip Code 57105-1007
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-42 Category Normal
A/W Date 05/09/2013 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 20130108
TEMPORARY FERRY FUEL SYSTEM IS INSTALLED IN THE PASSENGER CABIN. THE FERRY FUEL SYSTEM CONSISTS OF ONE BLADDER FUEL CELL WITH A CAPACITY OF500 GALLONS INSTALLED AT STATION 190. THE BLADDER FUEL CELL IS SECUREDUSING FOUR STRAPS RATED AT 3,335 LBS. ATTACHED TO THE EXISTING FLOOR TRACK ASSEMBLIES. FACTORY PANEL PN 101-364287-1 WAS REMOVED AND A DUPLICATE PANEL WAS MANUFACTURED WITH AN AN833-8 BULKHEAD FITTING INSTALLED. THE LHS WING MAIN TANK DRAIN PANEL HAS A -8 FITTING INSTALLED IN PLACE OF THE PLUG ASSEMBLY. THE BLADDER FUEL CELL HAS A -8 HOSE ASSEMBLY FROM THE FUEL BLADDER TO A 1/4 TURN FUEL SHUTOFF VALVE. THE VALVE IS CONNECTED TO THE BULLHEAD FITTING. A FUEL HOSE IS THEN ROUTED FROM THE BULKHEAD FITTING THROUGH THE WING CUFF AREA TO THE INBOARD FUEL DRAIN FITTING ON THE LHS WING MAIN FUEL TANK DRAIN PANEL. AIRCRAFT PRESSURIZATION IS THE MOTIVE FORCE FOR TRANSFERRING FUEL FROM THE BLADDER TO THE LHS WING. THE PILOT SHALL SELECT FERRY FUEL SYSTEM TO "ON" AS REQUIRED WHICH WILL DELIVER FERRY FUEL FROM THEBLADDER TO THE LHS WING. THE PILOT SHALL USE THE AIRCRAFT CROSSFEED FUEL SYSTEM TO FEED FUEL THE RHS ENGINE AS APPLICABLE TO MAINTAIN FUEL BALANCE. UPON ARRIVAL AT FINAL DESTINATION PER THE "SPECIAL FLIGHT PERMIT" ISSUED BY THE FAT-FSDO THIS DATE. THE FERRY FUEL SYSTEMSHALL BE REMOVED BY REMOVING THE MANUFACTURED PANEL AND REINSTALLING THE FACTORY PANEL PN 101-364287-1 AND REMOVING THE FITTING INSTALLED AT THE LHS WING DRAIN AND REINSTALLING THE PLUG ASSEMBLY.
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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