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N8360Y has Assigned/Multiple Records

N-Number Entered: 8360y Aircraft Description
Serial Number 28-8190195 Status Valid
Manufacturer Name PIPER Certificate Issue Date 09/20/2016
Model PA-28-181 Expiration Date 09/30/2029
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) 52670423
MFR Year 1981 Mode S Code (Base 16 / Hex) AB7113
Type Registration LLC Fractional Owner NO
Registered Owner
Name OTTO AVIATION LLC
Street 4112 FOREST LN
City SCHWENKSVILLE State PENNSYLVANIA
County MONTGOMERY Zip Code 19473-2508
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&VO-360 SER Category Utility, Normal
A/W Date 03/11/1981 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 19960902
INSTALLED ONE 85.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FOR FERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIRUSING THE FOLLOWING DRAWINGS: BTD063, NAI TF001, NAI TF002, NAI PS002, NAI V021, NAI M022, NAI SC002, AND TEH INSTALLATION WAS PERFORMED PERNAI INSTALLATION INSTRUCTIONS PA28-181-KIT. THE 85 GALLON TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM IN THE REAR PASSENGER SEAT LOCA- TION. THE TEMPORARY TANK IS SECURED TOT HE AIRFRAME WITH 1000 LBS. LOAD HUGGER STRAPS. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE. THE TEMPORARY TANK IS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANK IS SUPPLIED TO THE AIRCRAFT FUEL SYSTEM BETWEEN THE AIRCRAFT FUEL SELECTOR AND THE FUEL GASCOLATOR BOWL BY ON- OFF VALVE, APPROPRIATE FITTINGS, AND LOW PRESSURE HOSE. THE TEMPORARY TANK IS VENTED OVERBOARD THROUGH A MANUFACTURED VENT ATTACHED TO A TEMPORARY PANEL SECURED IN THE STORM WINDOW OPENING WITH THE LINE FORWARDFOR POSITIVE TANK PRESSURE. THE TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THIS TIME OF INSTALLATION AND WAS DETERMINED TO BE SATIS-FACTORY. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUND IN AC 43.13-1A OR ACCEPTED INDUSTRY PRACTICE.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 FURTHERINFO.
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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