FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N2342C is Assigned

N-Number Entered: 2342c Aircraft Description
Serial Number 30642 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 06/24/1991
Model 180 Expiration Date 08/31/2027
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) 50414775
MFR Year 1953 Mode S Code (Base 16 / Hex) A219FD
Type Registration Individual Fractional Owner NO
Registered Owner
Name HITE DONALD L
Street 10030 N AMERICAN LN
City MC KINNEY State TEXAS
County COLLIN Zip Code 75070-6553
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 O-470 SERIES Category None
A/W Date 01/16/1956 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 20090529
INSTALLED FLINT AERO AUXILIARY FUEL SYSTEM S/N 09H-1223 IAW STC SA1705WE, INSTALLATION DRAWINGS FA180 AND CESSNA SERVICE MANUAL GUIDE-LINES. ALL PARTS INSTALLED IAW INSTALLATION DRAWINGS FA 180. AUX. FUEL PUMPS, AUX. FUEL SWITCHES, AND FUEL GUAGUES PLACARDED IAW APPLI- CABLE STC INSTRUCTIONS. AUX. FUEL SYSTEM FLUSHED BEFORE FIRST FLIGHT AND AGAIN AFTER 5 FLIGHT HOURS IAW INSTALLATION DRAWINGS FA180. AUX. FUEL PUMPS AND CHECK VALVES CHECKED FOR PROPER FUNCTION WITH AUX SWITCHES IN BOTH ON AND OFF POSITIONS. OPERATION AND AUCCURACY OF AUX. FUEL GAUGES & ON-OFF SWITCHES VERFIED ACCORDING TO INSTALLATION DRAWING FA180. FLIGHT CHECK PERFORMED TO VERIFY PROPER OPERATION OF AUX FUEL SYSTEM AND A/C LOG ENTRIES MADE VERIFYING AIRWORTHINESS OF INSTALLATION. A/C WEIGHT/BALANCE DATA REVISED.

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