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N38CM has Assigned/Multiple Records

N-Number Entered: 38cm Aircraft Description
Serial Number 340A0901 Status Valid
Manufacturer Name CESSNA Certificate Issue Date 06/04/2014
Model 340A Expiration Date 06/30/2027
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) 51054457
MFR Year 1979 Mode S Code (Base 16 / Hex) A4592F
Type Registration Corporation Fractional Owner NO
Registered Owner
Name AIRCRAFT GUARANTY CORP TRUSTEE
Street 928 SW 107TH ST
City OKLAHOMA CITY State OKLAHOMA
County OKLAHOMA Zip Code 73170-5244
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 10/17/1979 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 T144460 Issue Date 06/04/2014 Expiration Date 07/04/2014
Fuel Modifications
Mod Code 28 Mod Date 19920804
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON SEPT. 14, 1989, AND THE ORIGINAL 337 APPROVAL IS RETAINED IN THE AEROFUSION CRSSA5R190N REPAIR STATION MANUAL. LONG RANGE FUEL TANK/S INSTALLED PER AERO- FUSION DRAWINGS AF-E00-II, AF-300-ID-1, AF-300-ID-2, AF-300-FS, AF-300-0I AND THE FOLLOWING TANK DRAWINGS AF-TYP-98. A NEW WEIGHT ANDBALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT, AND THE AIRCRAFT IS WITHIN THE 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 FORACCURACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.
Deregistered Aircraft
Deregistered Aircraft 1 of 1
Aircraft Description
Serial Number 3879A1101 Certificate Issue Date None
Manufacturer Name PIPER Mode S Code (base 8 / oct) 51054457
Model PA-38-112 Mode S Code (base 16 / hex) A4592F
Year Manufacturer None Cancel Date 10/28/1988
Reason For Cancellation Unknown Export To None
Type Registration Unknown
Aircraft Registration Prior to Deregistration
Name None
Street None
City None
State Zip Code None
County
Country
Deregistered Airworthiness
Engine Manufacturer None Classification Unknown
Engine Model None Category None
A/W Date None Exception Code No
Deregistered Other Owner Names
None
The duration of aircraft registration certificates has been extended up to 7 years. The Registry will be issuing revised certificates in batches based on the former expiration date. For verification purposes, even though the expiration date on the registration certificate may not match the expiration date in the FAA Aircraft Registration database, any registration certificate displaying an expiration date of January 31, 2023 or later is still valid. This applies to all foreign Civil Aviation Authorities or anyone else with a verification need.

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