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N-Number Inquiry Results

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N16TB is Assigned

N-Number Entered: 16tb Aircraft Description
Serial Number 1679TB47 Status Valid
Manufacturer Name DEHAVILLAND Certificate Issue Date 07/28/2006
Model DHC 2 MK III Expiration Date 10/31/2027
Type Aircraft Fixed Wing Single-Engine Type Engine Turbo-prop
Pending Number Change None Dealer No
Date Change Authorized None Mode S Code (base 8 / Oct) 50170400
MFR Year 1968 Mode S Code (Base 16 / Hex) A0F100
Type Registration LLC Fractional Owner NO
Registered Owner
Name EAGER BEAVER LLC
Street 3751 JOHN J MONTGOMERY DR
City SAN DIEGO State CALIFORNIA
County SAN DIEGO Zip Code 92123-1732
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 P&W Classification Standard
Engine Model PT6A SER Category Normal
A/W Date 07/26/1995 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 T065694 Issue Date 07/28/2006 Expiration Date 08/27/2006
Fuel Modifications
Mod Code 28 Mod Date 19960430
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 8-10-93 AND ORIGINAL337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-DHC-2-II, AF-DHC-2-ID, AF-DHC-2-L, AF-DHC-2-FM, AND APPROPRIATE FUEL TANK DRAWING(S) AF-TYP: 100,50. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND AIRCRAFT IS WITHIN WEIGHT AND C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUMCERTIFICATED WEIGHT, A STRUCTURAL EVALUATION LETTER FROM THE APPROPRI-ATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCEWITH THE ABOVE NAMED DRAWINGS, OPERATED PROPERLY, AND DOES NOT LEAK. THE MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCURACY. THE PILOT HAS BEENFURNISHED FUEL MANAGEMENT INSTRUCTIONS.

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