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N8537M is Assigned

N-Number Entered: 8537m Aircraft Description
Serial Number TD-534 Status Valid
Manufacturer Name BEECH Certificate Issue Date 02/18/2014
Model D95A Expiration Date 02/28/2030
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 52732726
MFR Year 1963 Mode S Code (Base 16 / Hex) ABB5D6
Type Registration LLC Fractional Owner NO
Registered Owner The Registered owner has requested to keep this data private under Title 49 of the United States Code Section 44114.
Name
Street
City State
County Zip Code
Country
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 LYCOMING Classification Standard
Engine Model I0360 SER Category Normal
A/W Date 05/24/1965 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
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 20120703
THIS MAJOR ALTERATION CONSISTS OF A MODIFICATION TO THE AIRCRAFT FUEL SYSTEM TO INCORPORATE A TEMPORARY EXTENDED RANGE FUEL SYSTEM, CONSISTING OF FOUR ALUMINUM FERRY FUEL TANKS, 6 FUEL SELECTOR VALVES AND ASSOCIATED FERRY FUEL FEED LINES AND FITTINGS. A TEMPORARY OIL SYSTEM IS INCORPORATED WITH A HAND PUMP TO REPLENISH THE ENGINE OIL SUPPLY. THE SYSTEMS ARE REQUIRED TO EXTEND THE RANGE FOR A ONE TIME DELIVERY FLIGHT FROM NORTH LAS VEGAS, NEVADA TO HONOLULU, HAWAII. THISMAJOR ALTERATION WILL CONSIST OF REMOVING THE AIRCRAFT COPILOT SEAT, CENTER SEATS REAR SEAT AND CARPETS FROM THE PASSENGER COMPARTMENT AND INSTALLING A TEMPORARY FERRY FUEL SYSTEM IN THE CABIN. THE TEMPORARY FERRY FUEL SYSTEM WILL BE CONNECTED TO THE AIRCRAFT MAIN FUEL SYSTEM. THE FERRY FUEL TANK SYSTEM CONSISTS OF ONE 30 GALLON NOSE TANK AND THREE 60 GALLON CABIN TANKS. THIS PROVIDES A TOTAL OF 210 GALLONS OF ADDITIONAL FERRY FUEL. TANK NUMBER AND CAPACITY LOCATION IN INCHES NUMBER 1 60 GALLONS RIGHT SIDE CABIN STATION 90. NUMBER 2 60 GALLONS LEFT SIDE CABIN STATION 124. NUMBER 3 60 GALLONS LATERAL CENTER STATION 124. NOSE TANK 30 GALLONS NOSE BAGGAGE STATION 15. THE TANKS ARE RECTANGULAR IN DESIGN AND CONSTRUCTED FROM 5052 ALUMINUM. 100 INCHES THICK BY ROYALL MANUFACTURING OF PLACERVILLE, CA. THE TANKS AREPRESSURE AND LEAKED CHECKEDD PER PERTINENT FARS. THE TANKS ARE ELECTICALLY GROUNDED TO AIRCRAFT STRUCTURE. THE TANKS ARE VENTED TO POSITIVE AIR PRESSURE, THROUGH A VENTED SYSTEM AND A RAM AIR VENT FITTING. THE TANKS ARE MOUNTED ON 1/2 INCH PLYWOOD PALLETS, AND THE CABIN TANKS ARE FURTHER BLOCKED ON THE SEAT RAILS WITH 2X4 SPACER SPACER BLOCKS. THE TANKS ARE SECURED TO THE AIRFRAME USING THE FOLLOW

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