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N-Number Inquiry Results

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N422CA is Assigned

N-Number Entered: 422ca Aircraft Description
Serial Number 238 Status Valid
Manufacturer Name CONSTRUCCIONES AERONAUTICAS SA Certificate Issue Date 12/22/2009
Model C-212-CC Expiration Date 01/31/2029
Type Aircraft Fixed Wing Multi-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51201500
MFR Year 1982 Mode S Code (Base 16 / Hex) A50340
Type Registration Corporation Fractional Owner NO
Registered Owner
Name BERING AIR INC
Street PO BOX 1650
City NOME State ALASKA
County NOME DIV Zip Code 99762-1650
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 AIRESEARCH Classification Standard-Restricted
Engine Model TPE331 SERIES Category Forest, Aerial Advertising, Agriculture and Pest Control
A/W Date 05/04/1993 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 19950526
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 5/26/95 AND ORIGINAL337 APPROVAL IS REAINED IN THE TELFORD AVIAITON INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-CA-212-II, AF-CA-212-OI, AF-CA-212-ID, AND THE FOLLOW-ING FUEL TANK DRAWINGS AF-TYP: 205, 205, 205. A NEW WEIGHT AND BALANCEHAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND THE AIRCRAFT IS WITHINTHE WEIGHT AND C.G. LIMITS. IF THE GROSS WEIGHT EXCEEDS 110% OF THE MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH THE ABOVE NAMED DRAWINGS, OPERATED 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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