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N3383X is Assigned

N-Number Entered: 3383x Aircraft Description
Serial Number 1096 Status Valid
Manufacturer Name MOONEY Certificate Issue Date 04/04/2006
Model M20E Expiration Date 04/30/2030
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) 50733136
MFR Year 1966 Mode S Code (Base 16 / Hex) A3B65E
Type Registration Individual Fractional Owner NO
Registered Owner
Name HIGER MATTHEW WARD
Street 9721 SANDMIST AVE
City LAS VEGAS State NEVADA
County CLARK Zip Code 89134-6625
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 Category Normal
A/W Date 04/16/1966 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
None
Fuel Modifications
Mod Code 28 Mod Date 20070620
EXTENDED RANGE FUEL. ALTERATION BY THE INSTALLATION OF MONROY AERO- SPACE LONG RANGE FUEL TANKS FOR MOONEY M20C & M20E. THE INSTALLATION WAS ACCOMPLISHED IN ACCORDANCE WITH STC #SA1913SO AND INSTALLATION INSTRUCTIONS REV 3.0 DATED 12/20/94 USING KIT P/N MK1001-SE PARTS SUPPLIED BY MONROY AEROSPACE. DRAWINGS SUPPLIED BY MONROY AEROSPACE FOR THE INSTALLATION ARE INCLUDED IN APPENDIX A, REV DATED 12/20/94. UPON COMPLETION OF THE INSTALLATION THE TANKS WERE FUELED AND LEAK CHECKED PERFORMED SATISFACTORILY. THE CHANGE TO THE WEIGHT/BALANCE OFTHE AIRCRAFT IS 29.0 LBS AT FS 66.0 AND WAS RECORDED IN THE AIRCRAFT RECORDS. NO ELECTRICAL POWER IS REQUIRED FOR THIS INSTALLATION. INSTRUCTIONS FOR CONTINUED A/W ARE INCLUDED IN THE STC ON PAGE 24 WHICH CALL FOR VISUAL CHECKS DURING PREFLIGHT AND FUELING, ANNUAL INSPECTION OF FITTINGS, TUBING AND HOSES, SEALING DISCS FOR LEAKS. ALL PARTS OF FAR43 APPENDIX D ARE APPLICABLE.

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