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N2124N has Assigned/Multiple Records

N-Number Entered: 2124n Aircraft Description
Serial Number 18-259 Status Valid
Manufacturer Name PIPER Certificate Issue Date 07/31/2015
Model PA-18 Expiration Date 07/31/2028
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) 50341741
MFR Year 1951 Mode S Code (Base 16 / Hex) A1C3E1
Type Registration Corporation Fractional Owner NO
Registered Owner
Name LIVESTOCK SERVICE INC
Street 2205 10TH ST
City DOUGLAS State ARIZONA
County COCHISE Zip Code 85607
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 0-320 SERIES Category Utility, Normal
A/W Date 04/15/2000 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 19960730
INSTALLED ONE 100.0 US GALLON ALUMINUM FUEL TANK IN THE CABIN AREA FORFERRY PURPOSES ONLY. THE TEMPORARY TANK WAS INSTALLED BY NORTHEAST AIRUSING THE FOLLOWING DRAWINGS: ANI M025, NAI SC002, NAI PS002, NAI TF002, NAI TF001, NAI V012, NAI BTD006, AND THE INSTALLATION WAS PERFORMEDPER NAI INSTALLATION INSTRUCTIONS PA-28RT-201T-KIT. TANK IS PLACED ON A WOODEN PLATFORM AT THE REAR PASSENGER SEAT LOCATION. TANK IS SECUREDTO THE AIRFRAME WITH TWO 1000 LBS LOAD HUGGER STRAPS ATTACHED TO THE FWD SEAT TRACK AND THE REAR SEAT BELT ATTACH POINTS. TEMPORARY TANKS IS PLACARDED FOR MAX. CAPACITY AND MIN. OCTANE, AND WAS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE AIRCRAFT RH WING FUEL TANK AND THE AIRCRAFT SELECTOR VALVE BY ON-OFF VALVES, APPROPRIATE FITTINGS AND LOW PRESSUREHOSE. THE TANK IS VENTED OVERBOARD THROUGH A PLATE ATTACHED TO THE AIRCRAFT LEFT HAND FRESH AIR VENT WINDOW AND WITH THE LINE FACING FOR-WARD FOR POSITIVE TANK PRESSURE. TEMPORARY FUEL SYSTEM WAS CHECKED FOROPERATION 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, CHAPTER 14, SECTION 2, OR ACCEPTED INDUSTRY PRACTICES. WEIGHT AND BALANCE FOR THIS TEMPORARY FUEL SYSTEM WAS CALCULATED AND SUBMITTED TO THE FLIGHT CREW. OPERATINGINSTRUCTIONS ARE SUBMITTED TO THE FLIGHT CREW AND IS ALSO ATTACHED TO THIS 337. SEE 337 FOR FURTHER INFO.
Mod Code 28 Mod Date 19960730
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 M025, NAI SC002, NAI PS002, NAI TF002, NAI TF001, NAI V012, NAI BTD006, AND THE INSTALLATION WAS PERFORMEDPER NAI INSTALLATION INSTRUCTIONS PA-28RT-201T-KIT. TANK IS PLACED ON A WOODEN PLATFORM AT THE REAR PASSENGER SEAT LOCATION. TANK IS SECUREDTO THE AIRFRAME WITH TWO 1000 LBS LOAD HUGGER STRAPS ATTACHED TO THE FWD SEAT TRACK AND THE REAR SEAT BELT ATTACH POINTS. TEMPORARY TANK ISPLACARDED FOR MAX. CAPACITY AND MIN. OCTANE, AND WAS PRESSURE CHECKED TO 3.5 PSI. FUEL FROM THE TEMPORARY TANK IS TEED INTO THE FUEL SUPPLY SYSTEM BETWEEN THE AIRCRAFT RH WING FUEL TANK AND AIRCRAFT SELECTOR VALVE BY ON-OFF VALVES, APPROPRAITE FITTINS AND LOW PRESSURE HOSE. THETANK IS VENTED OVERBOARD THROUGH A PLACTE ATTACHED TO AIRCRAFT LEFT HAND FRESH AIR VENT WINDOW WITH THE LINE FACING FORWARD FOR POSITIVE TANK PRESSURE. TEMPORARY FUEL SYSTEM WAS CHECKED FOR OPERATION AT THISTIME OF INSTALLATION AND WAS DETERMINED TO BE SATISFACTORY. FUEL SYS- TEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE STANDARD PRACTICES FOUNDIN AC 43.13-1A, CHAPTER 14, SECTION 2, OR 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 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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