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N683EA is Assigned

N-Number Entered: 683ea Aircraft Description
Serial Number E3863 Status Valid
Manufacturer Name HAWKER BEECHCRAFT CORP Certificate Issue Date 02/22/2016
Model G36 Expiration Date 02/28/2029
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) 52207301
MFR Year 2008 Mode S Code (Base 16 / Hex) A90EC1
Type Registration LLC Fractional Owner NO
Registered Owner
Name RED BARON LLC
Street 755 30TH AVE SW
City DICKINSON State NORTH DAKOTA
County STARK Zip Code 58601
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 CONT MOTOR Classification Standard
Engine Model IO-550-B Category Utility
A/W Date 07/11/2008 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 T161224 Issue Date 02/22/2016 Expiration Date 03/23/2016
Fuel Modifications
Mod Code 28 Mod Date 20081119
THIS AIRCRAFT HAS BEEN EQUIPPED WITH A TEMPORARY FERRY FUEL SYSTEM, CONSISTING OF ONE 150 GALLON TANK INSTALLED IAW NE-FSDO-05 APPROVED DATA AND TELFORD AVIATION SERVICES INC REPORT TAS-BE-A36 AND ENGINEE- RING REPORT TAS03-018. SEE ATTACHED TEMPORARY WEIGHT AND BALANCE DATA. THIS TEMPORARY WEIGHT AND BALANCE DATA WILL REMAIN IN EFFECT FOR THE DURATION OF THE SPECIAL FLIGHT PERMIT (FAA FORM 8130-7) AND/ORTHE TEMPORARY FUEL SYSTEM IS REMOVED. REQUIREMENTS FOR ADDITIONAL OILHAS BEEN ESTABLISHED IAW AC23.1011-1. REMOVAL INSTRUCTIONS ARE INCLUDED ALONG WITH FERRY FUEL SYSTEM MANAGEMENT INSTRUCTIONS. NOTE: THIS IS A TEMPORARY INSTALLATION. UPON ARRIVAL AT DESTINATION,THE TEMPORARY FERRY FUEL SYSTEM MUST BE REMOVED; THE AIRCRAFT INSPECTED FOR DAMAGE AND PROPER OPERATIONS; AND THE COMPASS CHECKED FOR ACCURACYBEFORE RETURNING THIS AIRCRAFT TO SERVICE. THE CURRENT WEIGHT AND BALANCE DATA IN THE FAA APPROVED AIRPLANE FLIGHT MANUAL OR PILOTS OPERATING HANDBOOK WILL AGAIN APPLY.

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