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N8358Y is Assigned

N-Number Entered: 8358y Aircraft Description
Serial Number 30-1505 Status Valid
Manufacturer Name PIPER Certificate Issue Date 02/11/2025
Model PA-30 Expiration Date 02/29/2032
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) 52667164
MFR Year 1967 Mode S Code (Base 16 / Hex) AB6E74
Type Registration Individual Fractional Owner NO
Registered Owner
Name GRUENBAUM MICHAEL S
Street 5985 GINGER DR
City EASTVALE State CALIFORNIA
County RIVERSIDE Zip Code 92880-0807
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 A1EA Type Certificate Holder PIPER AIRCRAFT INC
Engine Manufacturer LYCOMING Classification Standard
Engine Model IO-320 SERIES Category Normal
A/W Date 06/16/1967 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 19930701
INSTALLED ONE 30.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FOR FERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI BTD023, NAI TF001, NAI TF002, NAI PS003, NAI VO12, NAI MO28, NAI SC002, AND THE INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS PA30-KIT. THE 30 GALLON TEMPORARY TANK IS PLACED ON A WOODEN PLATFORM IN THE REAR BAGGAGE LOCATION. THE TEMPORARY TANK IS SECURED TO THE AIRFRAME WITH 1000 LBSLOAD HUGGER STRAPS. THE TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITYAND 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 AIRCRAFT FUEL PUMP ON-OFF VALVES, 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 FORWARD FOR POSITIVE TANK PRESSURE.

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