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N75048 has Assigned/Multiple Records

N-Number Entered: 75048 Aircraft Description
Serial Number 28-7690286 Status Ineffect/Invalid
Manufacturer Name PIPER Certificate Issue Date 05/06/2003
Model PA-28-181 Expiration Date 06/30/2027
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) 52416416
MFR Year 1976 Mode S Code (Base 16 / Hex) AA1D0E
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE
Street GLEBE COTTAGE COOKES ROAD
City BERGH APTON NFLK State
County Zip Code NR15 1AA
Country UNITED KINGDOM
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 04/20/1976 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
Certificate Number T032188 Issue Date 05/06/2003 Expiration Date 06/05/2003
Fuel Modifications
Mod Code 28 Mod Date 19940609
THIS DATA WAS FIELD APPROVED BY FAA NE-FSOD-05 ON 9-1-93 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PRE TELFORD AVIATION INC DRAWINGS AF-PA-28-32-ID, AF-PA-32-L, AF-PA- 28-32-FM/LYC AND APPROPRIATE FUEL TANK DRAWING AF-TYP: A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND THE AIRCRAFT IS WITHIN THE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUA- TION LETER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HASBEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUC- TIONS.

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