FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N6971V is Assigned

N-Number Entered: 6971v Aircraft Description
Serial Number 22-1338 Status Valid
Manufacturer Name MOONEY Certificate Issue Date 09/11/2019
Model M20F Expiration Date 09/30/2029
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) 52243506
MFR Year 1976 Mode S Code (Base 16 / Hex) A94746
Type Registration Individual Fractional Owner NO
Registered Owner
Name GREEN NATHAN E
Street 3325 INDIAN TRL
City FLOWER MOUND State TEXAS
County DENTON Zip Code 75022-6853
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 A&C Category Normal
A/W Date 01/26/1976 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 T199017 Issue Date 12/03/2019 Expiration Date 01/02/2020
Fuel Modifications
Mod Code 28 Mod Date 20000702
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 03-21-97 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-MO-20-II, AF-MO-20-OI, AF-MO-20-FS AF-MO-20-ID, AND AF-TYP(S): 60. 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, ASTRUCTURAL 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 8/2/00.

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