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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N916KW is Assigned

N-Number Entered: 916kw Aircraft Description
Serial Number 89 Status In Question
Manufacturer Name AEROFAB INC Certificate Issue Date None
Model LAKE 250 Expiration Date None
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) 53126753
MFR Year None Mode S Code (Base 16 / Hex) ACADEB
Type Registration Individual Fractional Owner NO
Registered Owner
Name REGISTRATION PENDING
Street 60 BAY SHORE DR
City LACON State ILLINOIS
County MARSHALL Zip Code 61540-9602
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 AMA/EXPR Classification Standard
Engine Model UNKNOWN ENG Category Normal
A/W Date 04/21/1989 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
APPLICANT MURPHY PATRICK J
APPLICATION DATED 1/29/26
Temporary Certificates
None
Fuel Modifications
Mod Code 28 Mod Date 20001211
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 05-22-97 AND ORIGINAL 337 APPROVAL IS RETAINED IN TELFORD AVIATION SERVICES INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION SERVICES INC DRAWINGS AF-LA-250-OI, AF-LA-250-FS, AF-LA-250- ID, AF-LA-250-II, AND AF-TYP(S): 130. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT,A STRUCTURAL EVALUATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATEPROPERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOT FURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 12/21/00.

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