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N856MA has Assigned/Multiple Records

N-Number Entered: 856ma Aircraft Description
Serial Number 208B5084 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 10/30/2019
Model 208B Expiration Date 10/31/2029
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) 52737266
MFR Year 2013 Mode S Code (Base 16 / Hex) ABBEB6
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-140 Category Normal
A/W Date 12/09/2013 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 20170418
INSATLLED TEMPORARY FUEL SYSTME CONSISTING OF (4) FOUR ALUMINUM FERRY TANKS, FUEL VALVE MANIFOLD, (2) TWO 24 VOLT ELECTRONIC TRANSFER PUMPS,AND ASSOCIATED FUEL LLINES IAW ENCLOSED DRAWINGS LABELED (CARAVAN FERRY FUEL DRAWING #1) TNAKS ARE INSTALLED IN THE CABIN AREA ON A RACKCONSISTING OF 2X4 AND 1/2 INCH PLYWOOD BASE FOR EVEN LOAD DISTRIBUTIONTANKS ARE GROUNDED TO THE AIRFRAME FOR STATIC DISCHARGE, TANKS ARE RECTANGULAR BAFFELED INTERNALLY, CONSTRUCTED OF WELDED 5052 ALUMINUM 100" THOUSANDS THICK AND PRESSURE TESTED IAW FAR 23.965A(1). THE TANKSSECURED FOR AND AFT AND VERTICALLY TO THE PASSENGERS INBOARD MIDDLE AND OUTBOARD SEAT TRACKS USING AIRCRAFT TIE-DOWN RINGS AND (4) FOUR 3000# LB RATING CARGO STRAPS MEETING OR EXCEEDING FAA TSO C22. THE TANKS ARE SUPPORTED LATERALLY BY AIRCRAFT SID STRUCTURE AND ARE PROTECTED USING SOFT VINYL PADDING. THE FERRY FUEL SYSTEM IS PLUMMED INTO THE AIRCRAFT FUEL SYSTEM BY INSTALLATION OF A "T" IN THE INTER- TANK EQUALIZER VENT TUBE IN THE RIGHT WING ROOT. THIS INSTALLATION DOES NOT HAMPER VENTING OF THE AIRCRAFT FUEL SYSTEM. ALL FEED FITTINGSAND HOSES ARE 1/2" INCH AND FUEL TOLERANT HOSE IS USED THROUGHOUT. FERRY FUEL MANIFOLD AND TSO'D AIRBORNE ELECTRONIC PUMPS ARE MOUNTED BESIDE THE PILOT SEAT. EACH PUMP IS CAPABLE OF DELIVERING ENOUGH FUEL FOR CONTINUED FLIGHT. POWER FOR THE FUEL PUMPS IS TAKEN FROM THE AIRCRAFT MAIN BATTERY BUS AND PROTECTED BY TEMPORARY MAIN 30 AMP FUSE AND SEPERATE 5 AMP CIRCUT BREAKERS, ALL ACCESSIBLE TO THE PILOT IN FLIGHT. THE FERRY FUEL SYSTEM IS VENTED TO THE EXTERIOR OF THE AIRCRAFT THROUGH A TEMPORARY ENT PROTRUDING BENEATH THE RIGHT WING ANDSUPPLYING RAM AIR TO THE TANK SYSTEM. A PLACARD FOR OPERATION OF THE
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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