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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N414AK is Assigned

N-Number Entered: 414ak Aircraft Description
Serial Number 414A0321 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 08/25/2022
Model 414A Expiration Date 08/31/2029
Type Aircraft Fixed Wing Multi-Engine Type Engine Reciprocating
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 51161406
MFR Year 1979 Mode S Code (Base 16 / Hex) A4E306
Type Registration LLC Fractional Owner NO
Registered Owner
Name VALIAIR LC TRUSTEE
Street OGDEN AIRPORT GATEWAY CENTER
4248 S 1650 W BLDG 1 STE 10
City OGDEN State UTAH
County WEBER Zip Code 84405
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 CONT MOTOR Classification Standard
Engine Model TSIO-520 SER Category Normal
A/W Date 07/23/1999 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 T220248 Issue Date 08/25/2022 Expiration Date 09/24/2022
Fuel Modifications
Mod Code 28 Mod Date 20071213
INSTALL CLARENCE BRENT & AIR AMERICA INC NACELLE FUEL LOCKER TANKS STC #SA2872SW. STC DATED NOVEMBER 22, 1978 AND REVISED 12/20/78, 02/02/79, 05/08/70, 11/04/80, 12/30/80 & 3/10/82. INSTALLATION OF WING NACELLE LOCKER TANKS DONE IN ACCORDANCE TO DRAWING LIST S40000 DATED 6/19/80 AND REVISED 10/15/80 OR LAST FAA APPROVED REVISIONS. A FORWARD TANK AND AN AFT FUEL TANK WERE INSTALLED IN THE LEFT WING NACELLE (TANK S/N'S #829 & #830) AND ONLY AN AFT FUEL TANK WAS INSTALLED IN THE RIGHT WING NACELLE (TANK S/N #831). A FLIGHT MANUAL SUPPLEMENT WAS INSTALLED INTO THE AIRCRAFT APPROVED FLIGHT MANUAL SUPPLEMENT DATED 12/07/78. A NEW COMPUTED EMPTY WEIGHT AND BALANCE WAS INSTALLED INTO THE WT & BAL SECTION OF THE APPROVED FLIGHT MANUAL. CONTINUED AIRWORTHINESS INSTRUCTIONS FOR WING NACELLE LOCKER FUEL TANKS IS ADDRESSED IN THE CESSNA ANNUAL INSPECTION GUIDE FOUND IN THE CESSNA MAINTENANCE MANUAL FOR THE 414A.

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