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N8SZ is Assigned

N-Number Entered: 8sz Aircraft Description
Serial Number 4608079 Status Valid
Manufacturer Name PIPER Certificate Issue Date 12/20/2017
Model PA-46-310P Expiration Date 12/31/2027
Type Aircraft Fixed Wing Single-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 52557323
MFR Year 1987 Mode S Code (Base 16 / Hex) AADED3
Type Registration Co-Owned Fractional Owner NO
Registered Owner
Name FINCH STANLEY F
Street 2911 GREAT OAKS DR
City SAN MARCOS State TEXAS
County HAYS Zip Code 78666-1008
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 CONT MOTOR Classification Standard
Engine Model TSIO-520 SER Category Normal
A/W Date 08/30/1991 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
COOPER EDWIN H JR
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 19950705
INSTALLED ONE 120.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FORFERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIRUSING THE FOLLOWING DRAWINGS: NAI M023, NAI V013, NAI PS002, NAI TF001NAI TF002, NAI TBD-053 AND THE INSTALLATION WAS PERFORMED PER NAI 46- 310P-KIT INSTALLATION INSTRUCTIONS. THIS TANK IS PLACED ON A WOODEN PLATFORM BETWEEN THE CENTER AND REAR PASSENGER SEAT LOCATION. THE TANKIS SECURED TO THE AIRFRAME WITH TWO 1000 LBS LOAD HUGGER STRAPS TO CENTER AND REAR SEATS SEAT BELT ATTACH STRUCTURE. THE TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE AIRCRAFT FUEL STRAINERAND THE AIRCRAFT ENGINE BY AN ON-OFF VALAVE, APPROPRIATE FITTINGS AND LOW PRESSURE HOSE. THE TANK IS VENTED OVERBOARD THROUGH AN EMERGENCY VENT VALVE AND IS "TEED" IN THE LOWER FUSELAGE SKIN. THE PRESSURE VENTIS A 3/4" CHECK VALVE ATTACHED TO THE TOP OF THE TANK IS CLOSED EXCEPTWHEN THE AIRCRAFT IS PRESSURIZING. THIS TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATISFACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A CHAPTER 14, SECTION 2AND ACCEPTED INDUSTRY PRACTICES. WEIGHT AND BALANCE FOR THIS TEMPORARYFUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATINGINSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO.
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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