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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N167CD is Assigned

N-Number Entered: 167cd Aircraft Description
Serial Number 1073 Status Ineffect/Invalid
Manufacturer Name CIRRUS DESIGN CORP Certificate Issue Date 07/09/2019
Model SR20 Expiration Date 07/31/2029
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) 50205745
MFR Year None Mode S Code (Base 16 / Hex) A10BE5
Type Registration Corporation Fractional Owner NO
Registered Owner
Name SOUTHERN AIRCRAFT CONSULTANCY INC TRUSTEE
Street GLEBE COTTAGE COOKES RD
City BERGH APTON NFLK State
County Zip Code NR15 1AA
Country UNITED KINGDOM
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-360 SER Category Normal
A/W Date 09/30/2000 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 T195254 Issue Date 07/09/2019 Expiration Date 08/08/2019
Fuel Modifications
Mod Code 28 Mod Date 20001017
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 02-02-00 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-CI-20-OI, AF-CI-20-FS, AF-CI-20-ID, AF-CI-20-II, AND AF-TYP(S): 105. 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 11/18/00.

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