FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N236FY is Assigned

N-Number Entered: 236fy Aircraft Description
Serial Number 2842023 Status Valid
Manufacturer Name PIPER Certificate Issue Date 06/18/2025
Model PA-28-161 Expiration Date 06/30/2032
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) 50417536
MFR Year 2000 Mode S Code (Base 16 / Hex) A21F5E
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SPACE COAST AIRCRAFT CO
Street 900 AIRPORT RD
City MERRITT ISLAND State FLORIDA
County BREVARD Zip Code 32952-3742
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 Standard
Engine Model O-320-D3G Category Utility, Normal
A/W Date 08/17/2025 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 T258112 Issue Date 06/18/2025 Expiration Date 07/18/2025
Fuel Modifications
Mod Code 28 Mod Date 19971030
INSTALLED ONE 100.0 US GALLON ALUMINUM FUEL TANK IN CABIN AREA FOR FERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI TD078, NAI TF001, NAI TF002, NAI PS002, ANI V021, NAI M022, NAI SC002, AND TEH INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS PA28-161 KIT. TEMPORARY TANK IS PLACED ON WOODEN PLATFORM IN REAR PASSENGER SEAT LOCATION. TEMPORARY TANK IS SECURED TO AIRFRAME WITH 1000 LBS LOAD HUGGER STRAPS. TEMPO- RARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. TEMPORARY TANK IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM TEMPORARY TANK IS SUP-PLIED TO THE AIRCRAFT FUEL SYSTEM BETWEEN AIRCRAFT FUEL SELECTOR AND THE FUEL GASCOLATOR BOWL BY ON-OFF AN VALVE, APPROPRIATE FITTINGS, ANDLOW PRESSURE HOSE. TEMPORARY TANK IS VENTED OVERBOARD THROUGH A MANU- UFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WIN-DOW OPENING WITH THE LINE FORWARD FOR POSITIVE TANK PRESSURE. THE 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 AND ACCEPTED INDUSTRY PRACTICES. 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. EXPIRY DATE IS 11/30/97.

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