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N201HS is Assigned

N-Number Entered: 201hs Aircraft Description
Serial Number 24-0228 Status Valid
Manufacturer Name MOONEY Certificate Issue Date 11/07/2019
Model M20J Expiration Date 11/30/2029
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) 50313172
MFR Year 1977 Mode S Code (Base 16 / Hex) A1967A
Type Registration Corporation Fractional Owner NO
Registered Owner
Name EUROAVIATION INC TRUSTEE
Street INDUSTRIEZONE 7
City KEMATEN State
County Zip Code 6175
Country AUSTRIA
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 Category Normal
A/W Date 06/20/1977 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 T223411 Issue Date 11/05/2022 Expiration Date 12/05/2022
Fuel Modifications
Mod Code 28 Mod Date 19930115
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 TNAK DRAWING: AF-TYP-50. 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 FORACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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