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N4100H has Assigned/Multiple Records

N-Number Entered: 4100h Aircraft Description
Serial Number 24-1029 Status Valid
Manufacturer Name MOONEY Certificate Issue Date 04/29/2021
Model M20J Expiration Date 04/30/2028
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) 51153200
MFR Year 1980 Mode S Code (Base 16 / Hex) A4D680
Type Registration Corporation Fractional Owner NO
Registered Owner
Name TJ AIR HOLDINGS INC TRUSTEE
Street 3511 SILVERSIDE RD STE 105
City WILMINGTON State DELAWARE
County NEW CASTLE Zip Code 19810-4902
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 I0360 SER A&C Category Normal
A/W Date 08/18/1980 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 T213633 Issue Date 04/29/2021 Expiration Date 05/29/2021
Fuel Modifications
Mod Code 28 Mod Date 19921027
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 10/27/88 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-MY-II, AF-MO-FS, AF-MY-21, AF-MY-ID-1, AF-MY-ID-2 AND THE FOLLOWING FUEL TANK DRAWINGS AF-TYP-50 AND AF-TYP-30. 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 CERTIFIED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE 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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