FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N811PJ is Assigned

N-Number Entered: 811pj Aircraft Description
Serial Number 3051 Status Valid
Manufacturer Name AERO COMMANDER Certificate Issue Date 04/02/2015
Model 500 S Expiration Date 04/30/2028
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) 52607141
MFR Year 1969 Mode S Code (Base 16 / Hex) AB0E61
Type Registration Individual Fractional Owner NO
Registered Owner
Name OBRIEN NEAL J
Street 635 DEVONSHIRE FARMS WAY
City MILTON State GEORGIA
County FULTON Zip Code 30004-4322
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 TI0-540 SER Category Utility, Normal
A/W Date 08/15/1969 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 20070525
INSTALLATION OF 560F AUX. FUEL SYSTEM IN 500S. REFERENCE ILLUSTRATION1258-1. REMOVE 500S FUEL VAPOR BOX IN BAGGAGE AREA TO GAIN ACCESS TO MAIN FUEL SUMP. REMOVE SHUTOFF VALVES, SUMP AND BOOST PUMPS. BOOST PUMPS WILL NOT BE REUSED. SHUTOFF VALVES WILL BE SAVED FOR REINSTALL.REMOVE ALL ACCESS PANELS IN WINGS AND NACELLES, AS NEEDED FOR ACCESS. INSTALL 560F MAIN FUEL SUMP USING NEW GASKETS. LOCATE AND CUT OPENINGS TOP OF BOTH WINGS BETWEEN WING STATIONS 98.0 AND 127.0 FOR FUEL WING BAY ACCESS. INSTALL DOUBLERS FROM 560F WINGS FOR ACCESS PANELS. INSTALL FUEL TANK HANGERS. INSTALL HANGERS ON STRINGERS ACCORDING TO LOCATION OF HANGERS ON TANKS FOR LACING PURPOSES. HOLES FOR INTERCONNECTS AND VENT LINES EXIST IN 500S STRUCTURE FROM THE FACTORY IN APPROPRIATE AREAS. INSTALL GROMMETS IN EXISTING FUEL INTERCONNECT AND VENT HOLES IN STRUCTURE AS NEEDED TO PROTECT LINES. LOCATE AND INSTALL SUMP PLATES REMOVED FROM 560F WING AND DRAIN VALVE ASSEMBLIES. MARK AND DRILL HOLES FOR SNAPS AS NEEDED FOR SECURING TANKS. INSTALL FOAM PIECES FROM 560F WING FOR BOTTOM OF FUEL BAYS TO FILL VOID BETWEEN LOWER WING STRINGERS. TAPE INTERNAL STRUCTURE OF WING FUEL BAYS FOR PROTECTION AS NEEDED. INSTALL FUEL CELLS IN APPROPRIATE BAYS. LACE UP TANKS AS REQUIRED, USING APPROPRIATE LACINGCORD. FABRICATE AND INSTALL VENT LINES FOR AUX TANKS TO EXISTING 'T' CONNECTION IN 500S VENT SYSTEM. USE EXISTING HOLES IN RIBS. INSTALL GROMMETS AS NEEDED TO PROTECT VENT LINES AND RIBS. FRONT TANKS REQUIRESCALLOPED VENT TUBE FROM 560F INSTALLATION. INSTALL TANK INTERCONNECTBETWEEN FORWARD AND AFT TANKS. INSTALL TWO FUEL SHUTOFF VALVES, REMOVED FROM 500S SUMP FOR MAIN TANKS AND ADDITIONAL SHUTOFF VALVES,

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