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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N10PW is Assigned

N-Number Entered: 10pw Aircraft Description
Serial Number E-2950 Status Valid
Manufacturer Name BEECH Certificate Issue Date 08/03/2021
Model A36 Expiration Date 08/31/2028
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) 50001665
MFR Year 1995 Mode S Code (Base 16 / Hex) A003B5
Type Registration Corporation Fractional Owner NO
Registered Owner
Name AIRCRAFT PARTNER HOLDINGS INC TRUSTEE
Street BERLINER STR 84
City BERLIN State
County Zip Code 13189
Country GERMANY
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 IO-550 SERIES Category Utility
A/W Date 05/26/1995 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 T216655 Issue Date 08/03/2021 Expiration Date 09/02/2021
Fuel Modifications
Mod Code 28 Mod Date 19950821
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-05 ON 9-1-93 AND ORIGINAL 337 APPROVAL IS RETAINED IN THE TELFORD AVIATION INC (J2SR196J) REPAIRSTATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATIONINC DRAWINGS AF-BE-30-II, AF-BE-30-FS, AF-BE-ID, AF-BE-ID-2, AF-BE-20-FM, AND THE FOLLOWING FUEL TANK DRAWING(S) AF-TYP: 100. A NEW WEIGHT AND BALANCE HAS BEEN COMPUTED AND PROVIDED TO THE PILOT AND 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.

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