FAA REGISTRY

N-Number Inquiry Results


Data Updated Each Federal Working Day At Midnight

N265CC has Assigned/Multiple Records

N-Number Entered: 265cc Aircraft Description
Serial Number 42.AC102 Status Valid
Manufacturer Name DIAMOND AIRCRAFT IND INC Certificate Issue Date 03/24/2026
Model DA 42 Expiration Date 03/31/2033
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) 50510705
MFR Year None Mode S Code (Base 16 / Hex) A291C5
Type Registration Corporation Fractional Owner NO
Registered Owner
Name INTERNATIONAL AIR SERVICES INC TRUSTEE
Street 123 W NYE LN STE 129
City CARSON CITY State NEVADA
County CARSON CITY Zip Code 89706-0838
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 THIELERT Classification Standard
Engine Model TAE 125-02-99 Category Normal
A/W Date 11/27/2007 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 T267298 Issue Date 04/09/2026 Expiration Date 05/09/2026
Fuel Modifications
Mod Code 28 Mod Date 20140828
INSTALLED TEMPORARY FUEL SYSTEM RESTING ON PLYWOOD SUPPORTING ON EXISTING AIRCRAFT STRUCTURE. PLYWOOD BASE IS INSTALLED TO FACILITATE EVEN LOAD DISTRIBUTION. AIRCRAFT FLOOR LOADING LIMITS ARE NOT EXCEEDEDFERRY SYSTEM CONSISTS OF 2 ALUMINUM TANKS. THE TANKING SYSTEM TOTAL CAPACITY IS 95 U.S. GALLONS. TANKS ARE CONSTRUCTED FROM .090 5052-H34 ALUMINUM WELDED AT ALL SEAMS, INTERNAL BAFFLES ARE INSTALLED AND WELDED INTO PLACE. CONSTRUCTION OF TANKS MEETS THE STANDARDS OF U.S. COAST GUARD 33 C.F.R. 183.580 SPECIFICATIONS. TANKS ARE PRESSURE AND LEAK TESTED IN ACCORDANCE WITH FAR 23.965A(1) AT POINT OF MANUFACTURE;WILLIAMS MANUFACTURING, TRACY, CA. ALL TANKS ARE SECURED TO SEAT TRACKS WITH CARGO TIE DOWNS. THESE TIE DOWN STRAPS ARE OF IDENTICAL TYPE THAT HAVE BEEN UTILIZED IN PREVIOUSLY FAA APPROVED TANKING SYSTEMSTRAPS, (2 EACH) SECURE THE TANKS LONGITUDINALLY AND LATERALLY. FERRY FUEL TANKS ARE ELECTRICALLY BONDED TO THE AIRFRAME TO FACILITATE STATIC DISCHARGE,, AND ARE VENTED TO THE ATMOSPHERE, AS OUTLINED IN AC43-13-1B. CHAPTER 11 SECTION 15 PARAGRAPH 11-191 AND CHAPTER 8 SECTION 2 PARAGRAPH 8-33. THE FERRY TANKING SYSTEM IS PLUMBED INTO THEAIRCRAFT FUEL SYSTEM AS NOTED ON THE AIRCRAFT FUEL SYSTEM SCHEMATIC. THIS IS CO-LOCATED WITH, AND IS A PART OF THE FERRY FUEL MANAGEMENT DETAILS LOCATED IN ATTACHMENT 1 OF THE TANKING INSTALLATION PACKAGE. AIRCRAFT FERRY FUEL SYSTEM OPERATION AND MANAGEMENT DETAILS IS OUTLINED IN ATTACHMENT 2. CONTINUOUS AIRWORTHINESS COMPLIANCE NOT APPLICABLE DUE TO TEMPORARY INSTALLATION. INSTALLATION TEMPORARY WEIGHT AND BALANCE IS COMPUTED ON THE ATTACHMENT TO THE FERRY TANK INSTALLATION FAA FORM 337 DATED JULY 31, 2014.

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