FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N198B has Assigned/Multiple Records

N-Number Entered: 198b Aircraft Description
Serial Number TH-1936 Status Valid
Manufacturer Name RAYTHEON AIRCRAFT COMPANY Certificate Issue Date 01/12/2024
Model 58 Expiration Date 01/31/2031
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50302774
MFR Year 2000 Mode S Code (Base 16 / Hex) A185FC
Type Registration LLC Fractional Owner NO
Registered Owner
Name ARKLA AVIATION LLC
Street 120 EAGLE POINT DR
City FARMERVILLE State LOUISIANA
County UNION Zip Code 71241-3852
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-C Category Normal
A/W Date 02/05/2021 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 20000316
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 ON 3-21-97 AND ORIGINAL 337 APPROVAL IS RETAINED IN TELFORD AVIATION SERVICES INC (J2SR196J) REPAIR STATION MANUL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION SERVICES INC DRAWINGS BE-58-II, AF-BE-58-OI, AF-BE-58-FS, AF-BE-58-ID AND AF-TYP(S) 98,98. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSSWEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVAL-UATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 4/14/00.

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