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N753KP is Assigned

N-Number Entered: 753kp Aircraft Description
Serial Number 208B1275 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 04/04/2019
Model 208B Expiration Date 04/30/2029
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) 52423035
MFR Year 2007 Mode S Code (Base 16 / Hex) AA261D
Type Registration LLC Fractional Owner NO
Registered Owner
Name KALININ PARTNERS LLC
Street 8907 YANDUKIN DR
City JUNEAU State ALASKA
County JUNEAU DIV Zip Code 99801-8086
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 HONEYWELL Classification Standard
Engine Model TPE331-12JR Category Normal
A/W Date 03/05/2019 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 20140203
INSTALLED TEMPORARY FUEL SYSTEM CONSISTING OF FOUR ALUMINUM TANKS, FUEL VALVE MANIFOLD, TWO 24 VOLT ELECTRIC FUEL TRANSFER PUMPS, AND ASSOCIATED FUEL LINES IAW ATTACHED DRAWING LABELED "CARAVAN FUEL SYSTEM DRAWING # 1". TANKS ARE GROUNDED TO AIRFRAME FOR STATIC DISCHARGE. TANKS ARE INSTALLED IN THE CABIN AREA ON A RACK CONSISTING OF 2X4 AND 1/2 INCH PLYWOOD BASES FOR EVEN LOAD DISTRIBUTION. TANKS ARE RECTANGULAR, INTERNALLY BAFFLED, CONSTRUCTED FROM 5052 WELDED ALUMINUM .100 INCH THICK AND PRESSURE TESTED IAW FAR 23.965 (A)1. THE TANKS ARE SECURED FORE AND AFT AND VERTICALLY TO THEN CABIN INBOARD, MIDDLE, AND OUTBOARD SEAT TRACKS USING AIRCRAFT TIE DOWN RINGS AND FOUR CARGO STRAPS OF 3000# TENSILE STRENGTH AND CONFORMING TO TSO C22.THE TANKS ARE SUPPORTED LATERALLY BY THE CABIN SIDE STRUCTURE AND PROTECTED BY INTERIOR UPHOLSTERY AND VINYL PADDING. THE FERRY FUEL SYSTEM T'S INTO THE AIRCRAFT FUEL SYSTEM BY INSTALLATION OF A T IN THEAIRCRAFT FUEL TANK BALANCE VENT LINE LOCATED IN THE RIGHT WING ROOT. INSTALLATION DOES NOT INTERFERE WITH NORMAL FUEL TANK CROSS VENTING ALL FITTINGS ARE #8 OR LARGER AND FUEL TOLERANT HOSE IS USED THROUGH OUT THE INSTALLATION. FERRY FUEL SELECTOR MANIFOLD AND TWO TSO'ED AIRBORN FUEL PUMPS ARE MOUNTED BESIDE THE PILOTS SEAT. EACH PUMP IS CAPABLE OF DELIVERY OF ENOUGH FUEL FOR CONTINUED FLIGHT POWER FOR THE FUEL PUMPS IS TAKEN FROM THE MAIN BATTERY BUSS & IS PROTECTED THROUGH A TEMPORARY 30 AMP FUSE AND SEPARATE 10 AMP FUEL PUMP CIRCUIT BREAKERSALL ACCESSIBLE TO THE PILOT IN FLIGHT. FERRY FUEL SYSTEM IS VENTED TO THE EXTERIOR OF THE AIRCRAFT THROUGH A TEMPORARY VENT PROTRUDING THOUGH THEN RIGHT INBOARD LOWER PANEL AND SUPPLYING RAM AIR TO 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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