FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N115HP is Assigned

N-Number Entered: 115hp Aircraft Description
Serial Number 3246115 Status Valid
Manufacturer Name PIPER Certificate Issue Date 01/25/2017
Model PA-32R-301 Expiration Date 01/31/2030
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) 50037603
MFR Year 1998 Mode S Code (Base 16 / Hex) A03F83
Type Registration LLC Fractional Owner NO
Registered Owner
Name MJD LEASING LLC
Street 1227 E 42ND ST
City TEXARKANA State ARKANSAS
County MILLER Zip Code 71854-1505
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 IO-540 SER Category Normal
A/W Date 06/03/1998 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 19990317
INSTALLED ONE 100.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FORFERRY PURPOSES ONLY. TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIR USING THE FOLLOWING DRAWINGS: NAI PS002, NAI TF001, NAI TF002, NAI M007, NAI V021, NAI SC002, NAI BTD078, AND INSTALLATION WAS PERFORMED PER NAI INSTALLATION INSTRUCTIONS PA32R-301 KIT. TANK IS PLACED ON A WOODEN PLATFORM AT THE MID PASSENGER SEAT LOCATION. TANK IS SECURED TOTHE AIRFRAME WITH TWO 1000 LB LOAD HUGGER STRAPS, ATTACHED TO THE FWD SEAT TRACKS AND THE REAR SEAT BELT ATTACH POINTS. TEMPORARY TANK IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE AND WAS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM TEMPORARY TANK IS PLUMBED INTO FUEL SUPPLY SYS-TEM BETWEEN AIRCRAFT SELECTOR VALVE AND AIRCRAFT ELECTRIC FUEL PUMP BYAN ON-OFF VALVE, APPROPRIATE FITTINGS AND LOW PRESSURE HOSE. TANK IS VENTED OVERBOARD THROUGH THE PILOTS VENT WINDOW WITH A PITOT FACING FORWARD FOR POSITIVE TANK PRESSURE. THIS 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 43.13-1B CHAPTER 8 SECTION 2. 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. EXPIRY DATE IS 4/14/99.

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