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N835MA is Assigned

N-Number Entered: 835ma Aircraft Description
Serial Number 208B2335 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 07/12/2019
Model 208B Expiration Date 07/31/2029
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) 52666001
MFR Year 2012 Mode S Code (Base 16 / Hex) AB6C01
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-114A Category Normal
A/W Date 01/10/2012 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 T229002 Issue Date 07/29/2022 Expiration Date 08/28/2022
Fuel Modifications
Mod Code 28 Mod Date 20200417
TEMPORARY FUEL SYSTEM HAS BEEN INSTALLED CONSISITING OF FOUR (4) ALUMINUM FERRY TANKS. FUEL VALVE MANIFOLD, TWO (2) 24 VOLT ELECTRONIC TRANSFER PUMPS AND ASSOCIATED FUEL LINES IN ACCORDANCE WITH ENCLOSED DRAWINGS LABELED "CARAVAN FERRRY FUEL DRAWING #1". TANKS ARE INSTALLEDIN THE CABIN AERA ON PLATFORMS/BASES MAD OF 2X4'S AND 1/2 INCH PLY WOOD FOR EVEN LOAD DISTRIBUTION. THE FUEL TANKS ARE GROUNDED TO THE AIRFRAME FOR STATIC DISCHARGE. THE FUEL TANKS USED ARE RECTANGULAR, INTERNALLY BAFFLED AND CONSTRUCTED OF WLED 5052 ALUMINUM THAT IS .100 THIK AND SPRESSURE TESTED IAW FAR 23.965A(1). THE FUEL TANKS ARE SECURED HORIZONTALLY, VERTICALLY AND LATERALLY TO THE PASSENGER SEAT TRACKS USING AIRCRAFT TIE DOWN RINGS AND FOUR (4) 3000LB RATED CARGO STRAPS. THE FERRY FUEL SYSTEM IS PLUMMED INTO THE AIRCRAFT FUEL SYSTEM BY INSTILLATION OF A "T" FITTING IN THE INTER TANK EQULIZER VENT TUBE ON THE WING ROOT. THIS INSTALLATION DOES NOT INTERFERE WITH THE NORMAL VENTING OF THE AIRCRAFT FUEL SYSTEM TO THE OUSTSIDE AIR. ALLFITTINGS ARE SIZE 8 OR LARGER AND HOSES ARE 1/2" ID AND FUEL TOLERANT HOSES USED THROUGHOUT. FERRY FUEL VALVE MANIFOLD AND TSO'S AIRBOURNE ELECTRONIC FUEL PUMPS ARE LOCATED IN BETWEEN THE PILOTS SEATS. EACH FULE PUMP IS CAPIABLE OF DELIVERING ENOUGH FUEL FOR CONTINUED FLIGHT. POWER FOR TH FUEL PUMPS IS TAKEN FROM THE AIRCRAFT MAIN BATTERY BUS AND PROTECTED BY A SEPERATE 10AMP CIRCUIT BREAKERS ALL OF WHICH ARE ACCESSABLE TO THE PILOT DURING FLIGHT. ELECTRICAL WIRING INSTALLATION IS DONE IAW AC-43-13-1B. THE FERRY FUEL SYSTEM IS VENTED TO THE EXTERIOR OF THE AIRCRAFT THROUGH A TEMPORARY VENT PROTRUDING BENEATH THE RIGHT WING ROOT PANEL. THE VENT ALSO SUPPLIES
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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