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N-Number Inquiry Results

Data Updated Each Federal Working Day At Midnight

N999AB is Assigned

N-Number Entered: 999ab Aircraft Description
Serial Number 32R-8029043 Status Valid
Manufacturer Name PIPER Certificate Issue Date 10/30/1996
Model PA-32R-301T Expiration Date 07/31/2028
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) 53372024
MFR Year 1979 Mode S Code (Base 16 / Hex) ADF414
Type Registration Individual Fractional Owner NO
Registered Owner
Name BENTRUP REINHARD
Street ZUM BUCHWALD 4
City D 35463 FERNWALD State
County Zip Code 35463
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 LYCOMING Classification Standard
Engine Model TI0-540 SER Category Normal
A/W Date 01/17/1980 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 T965227 Issue Date 10/30/1996 Expiration Date 11/29/1996
Fuel Modifications
Mod Code 28 Mod Date 19961101
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-PA-32-OI, AF-PA-32-II, AF-PA-32-ID, AF-PA-32-FS AND AF-TYP(S) 120. 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 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, OPERATED PROP-ERLY AND DOES NOT LEAK. MAGNETIC COMPASS HAS BEEN CHECKED FOR ACCUR- ACY. THE PILOT HAS BEEN FURNISHED FUEL MANAGEMENT INSTRUCTIONS.
Deregistered Aircraft
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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