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N1024L has Assigned/Multiple Records

N-Number Entered: 1024l Aircraft Description
Serial Number P-78 Status Valid
Manufacturer Name BEECH Certificate Issue Date 07/22/2021
Model 60 Expiration Date 07/31/2028
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) 50007421
MFR Year 1969 Mode S Code (Base 16 / Hex) A00F11
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 TI0-541 SER Category Normal
A/W Date 03/23/1992 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 T216253 Issue Date 07/22/2021 Expiration Date 08/21/2021
Fuel Modifications
Mod Code 28 Mod Date 19920428
THIS DATA WAS FIELD APPROVED BY FAA, NE-FSDO-05 ON 09-27-90 AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRS SA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-B60-II, AF-B60-ID, AF-B60-FS, AF-B60-0I AND MANU- FACTURED PER FUEL TANK DRAWING AF-TYP-98. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED ADN 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 EVALUATION LETTER FROMTHE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN 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 INSTRUCTIONS.

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