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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N143SD is Assigned

N-Number Entered: 143sd Aircraft Description
Serial Number 25005C Status Valid
Manufacturer Name MAULE Certificate Issue Date 06/30/2026
Model M-7-235C Expiration Date 06/30/2033
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) 50127551
MFR Year None Mode S Code (Base 16 / Hex) A0AF69
Type Registration LLC Fractional Owner NO
Registered Owner
Name WHISKEY FOX GROUP LLC
Street 223 GULFSHORE DR
City DESTIN State FLORIDA
County OKALOOSA Zip Code 32541
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 IO-540 SER Category Normal
A/W Date 10/11/1996 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 T263098 Issue Date 06/30/2026 Expiration Date 07/30/2026
Fuel Modifications
Mod Code 28 Mod Date 19961031
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-ML-7-II, AF-ML-7-ID, AF-ML-7-FS, AF-ML-OI AND AF-TYP(S) 100. NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND AIRCRAFT IS WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVAL-UATION LETTER FROM 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 FOR ACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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