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FAA REGISTRY

N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N511TE is Assigned

N-Number Entered: 511te Aircraft Description
Serial Number TE511 Status Notice Ineff/Inval
Manufacturer Name BEECH Certificate Issue Date 03/31/2025
Model D55 Expiration Date 03/31/2032
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) 51463324
MFR Year None Mode S Code (Base 16 / Hex) A666D4
Type Registration Non Citizen Corporation Fractional Owner NO
Registered Owner
Name PIERONI CORP
Street 10708 BELO HORIZONTE AVE
City CLERMONT State FLORIDA
County LAKE Zip Code 34711-6319
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 Unknown Classification Unknown
Engine Model Unknown Category None
A/W Date None 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 20000405
THIS DATA WAS FIELD APPROVED BY FAA NE-FSDO-5 12/31/96 AND ORIGINAL 337 APPROVAL RETAINED IN THE TELFORD AVIATION SERVICES INC (J2SR196J) REPAIR STATION MANUAL. LONG RANGE FUEL TANK(S) INSTALLED PER TELFORD AVIATION SERVICES INC DRAWINGS AF-BE-55-II, AF-BE-55-OI, AF-BE-55-FS, AF-BE-55-ID, AND AF-TYP(S): 98. NEW WEIGHT AND BALANCE COMPUTED AND PROVIDED TO PILOT AND AIRCRAFT WITHIN WEIGHT A C.G. LIMITS. IF GROSS WEIGHT EXCEEDS 110% OF MAXIMUM CERTIFICATED WEIGHT, A STRUCTURAL EVAL-UATION LETTER FROM APPROPRIATE ACO IS ATTACHED. THIS FUEL SYSTEM HAS BEEN INSTALLED IN ACCORDANCE WITH ABOVE NAMED DRAWINGS, OPERATES PRO- PERLY, AND DOES NOT LEAK. MAGNETIC COMPASS CHECKED FOR ACCURACY. PILOTFURNISHED FUEL MANAGEMENT INSTRUCTIONS. SEE 337 FOR FURTHER INFO. EXPIRY DATE IS 5/4/2000.

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