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N4976W is Assigned

N-Number Entered: 4976w Aircraft Description
Serial Number 14296 Status Valid
Manufacturer Name ROCKWELL INTERNATIONAL Certificate Issue Date 01/24/2023
Model 114 Expiration Date 01/31/2030
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) 51426530
MFR Year 1977 Mode S Code (Base 16 / Hex) A62D58
Type Registration LLC Fractional Owner NO
Registered Owner
Name QUALITAIR LLC TRUSTEE
Street FLUGPLATZ MICHELSTADT
MOSSAUER STRASSE 17
City MICHELSTADT State
County Zip Code 64720
Country GERMANY
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 TI0-540 SER Category Utility, Normal
A/W Date 06/07/1977 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 T230981 Issue Date 01/24/2023 Expiration Date 02/23/2023
Fuel Modifications
Mod Code 28 Mod Date 19930428
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON MAY 21, 1990 AND THEORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRS SA55190N RE- PAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AEROFUSION DRAWINGS AF-114-II, AF-114-ID, AF-114-FS, AF-114-0I AND THE FOLLOWING FUEL TANK DRAWING AF-TYP-60. A NEW WEIGHT AND BALANCE HAS BEEN COM- PUTED AND PROVIDED TO THE PILOT, AND THE AIRCRAFT IS WITHIN THE WEIGHTAND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CER-TIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATED 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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