FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N76JN is Assigned

N-Number Entered: 76jn Aircraft Description
Serial Number 31-7652176 Status Valid
Manufacturer Name PIPER Certificate Issue Date 03/04/2025
Model PA-31-350 Expiration Date 03/31/2032
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) 52440004
MFR Year 1976 Mode S Code (Base 16 / Hex) AA4004
Type Registration Individual Fractional Owner NO
Registered Owner
Name GROSS CHARLES C III
Street 6780 US HIGHWAY 1
City MIMS State FLORIDA
County BREVARD Zip Code 32754-5801
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 LYCOMING Classification Restricted
Engine Model TI0-540 SER Category Aerial Surveying
A/W Date 05/20/2011 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 19960725
INSTALLED TWO 100.0 US GALLON ALUMINUM FUEL TANKS IN CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANKS WERE INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI TD067, NAI TF001, NAI TF002, NAI PS002, NAI V0-20, NAI M035, NAI SC002, NAI SG001 AND THE INSTALLATION WASPERFORMED PER NAI INSTALLATION INSTRUCTIONS PA31-350 KIT. TEMPORARY TANK IS PLACED ON WOODEN PLATFORM IN THE FWD PASSENGER SEAT LOCATION. TEMPORARY TANKS ARE SECURED TO SEAT TRACKS WITH 1000 LBS LOAD HUGGER STRAPS. TEMPORARY TANKS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. THE TEMPORARY TANKS ARE PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANKS IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE AIR- CRAFT FUEL SELECTOR VALVES AND THE FUEL GASCOLATOR BOWLS FOR EACH ENGINE, BY ON-OFF AN VALVE, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. TEMPORARY TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITHTHE LINE FORWARD FOR POSITIVE TANK PRESSURE. TEMPORARY FUEL SYSTEM WASCHECKED 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. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATING INSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO.

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