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N41991 has Assigned/Multiple Records

N-Number Entered: 41991 Aircraft Description
Serial Number 502B-2623 Status Valid
Manufacturer Name AIR TRACTOR INC Certificate Issue Date 04/23/2020
Model AT-502B Expiration Date 04/30/2030
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) 51174474
MFR Year 2008 Mode S Code (Base 16 / Hex) A4F93C
Type Registration Individual Fractional Owner NO
Registered Owner
Name BRAVO GILDARDO F
Street 3403 LOS INDIOS PKWY
City MISSION State TEXAS
County HIDALGO Zip Code 78572-7681
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 A17SW Type Certificate Holder AIR TRACTOR INC
Engine Manufacturer P&W CANADA Classification Restricted
Engine Model PT6A-34AG Category Forest, Agriculture and Pest Control
A/W Date 02/14/2008 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 20090904
REMOVED SIDE PANELS FROM AIRCRAFT AND INSTALLED SIDE LOAD FUELING SYSTEM USING FOLLOWING PARTS IN THE MANNER LISTED BELOW. A. INSTALLED 2" ALUMINUM EMCO WHEATON DRYBREAK BUCKEYE P/N J1302-018 WITH P/N AN816-24D NIPPLE ONTO .375"6061 T6511 ALUMINUM PLATE AND ATTACHED TO FUSELAGE VERTICAL TUBING AT STA.+138 ON LEFT HAND SIDE OF AIRCRAFT USING MS21919WDG ADEL CLAMPS SIZED AS NEEDED. B. INSTALLED P/N AN824- 24D TEE FITTING ON FUSELAGE DIAGONAL TUBING AT STA.+24 USING MS21919WDG ADEL CLAMPS SIZED AS NEEDED AND INSTALLED 2 EACH P/N AN894-24-16D REDUCERS ONTO TEE FITTING. C. REMOVED FACTORY INSTALLED PLUGS FROM WING FUEL TANK INBOARD SIDE ASSEMBLY AND INSTALLED P/N AN816-16D NIPPLES IN BOTH FUEL TANK SIDE RIBS. D. INSTALLED STRATOFLEX HOSE ENDSP/N 300-24D TEE. HOSE MANUFACTURED AND INSTALLED IN ACCORDANCE WITH AC43.13-1B CHAP 8 PARA 30 AND AC43.13 CHAP 9 PARA 30. E.INSTALLED STRATOFLEX HOSE ENDS P/N 300-16D ONTO AEROQUIP HOSE P/N 302A-16 OF RE-QUIRED LENGTHS AND ATTACHED AN824-24D/AN894-24-16D ASSEMBLY TO NIPPLESAN816-16D INSTALLED ON BOTH WING INBOARD FUEL TANK SIDES. HOSES MANUFACTURED AND INSTALLED IN ACCORDANCE WITH AC 43.13-1B CHAP 8 PARA 30 AND AC 43.13-1B /CGAO 9 PARA 30. CUT DRYBREAK ACCESS HOLE IN THE LEFT HAND SIDE PANEL. INSTALLED PLACARDS ON SIDE PANEL AT FUELING POINT AND IN COCKPIT STATING REMOVE WING FUEL CAPS WHEN USING SIDE LOAD FUELING SYSTEM. FUELS TANKS FILLED USING SIDE LOAD FUELING SYSTEMAND LEAK CHECK PERFORMED. REINSTALLED SIDE PANELS ON AIRCRAFT. NEGLIGIBLE WEIGHT CHANGE.
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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