N141UP

Service difficulty reports · 314

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N141UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026050659214Support Bracket · gougedLEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 70 Y450 BEAM LOWER SUPPORT BRACKET GOUGED. REMOVED AND REPLACED LOWER SUPPORT AT ZONE 200. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 70 Y450 IAW A300-600 SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050753105Bracket · damagedPANEL 672CB I/B ATTACH FITTING, HOLE ELOGATED 1EA. INSTALLED 2EA.BRACKETS ON PANEL 672CB IAW SRM 51-40 21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Wing StructureSDR IPXA2026050255146Angle · crackedAVIONIC COMPARTMENT FR C10 L\H- Y1456 FWD UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE P/N A53612356200, B/N 0004482008 AT AVIONIC COMPARTMENT FR10 L/H Y1456 FWD UPPER IAW SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050255069Angle · crackedAVIONIC COMPARMENT FR C10 L\H -Y1456 AFT UPPER ANGLE CRACKED. REMOVED ANGLE AT AVIONIC COMPARMENT FR 10 L/H Y1456 AFT UPPER IAW SRM 51-40-21-001. INSTALLED NEW ANGLE P/N UPA53612218200 AT AVIONIC COMPARMENT FR 10 L/H Y1456 AFT UPPER IAW SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042359094Web · crackedLEFT MAIN CABIN FLOOR STRUCTURE FR 78 LT OTBD WEB IS CRACKED. INSPECTED THE INSTALLATION OF NEW WEB ASSY. INSTALLED NEW WEB AT FR 78 LT OTBD IAW SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042959026Floor Support · crackedLEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 78-79 O/B Z-PROFILE HAS (2EA) CRCKS. Z-PROFILE WAS REMOVAL STR-ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 78-79 O/B I.A.W A300-600 SRM 51-40-21. INSTALLED NEW Z-PROFILE AT ZONE 200, LH MAIN CABIN COMApr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042859074Seat Track · crackedLEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 79 Y 2127.5 SEAT TRACK LOWER ANGLE IS CRACKED. REMOVED ANGLE AT FLOOR STRUCTURE FR 79 Y 2127.5 LH MAIN CABIN IAW A300-600 SRM 51-40-21-001. INSTALLED NEW BRACKET P/N UPA53275449206AT FLOOR STR, FR79 Y 2127.5 SEAApr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026042953267Floor Panel · damagedMAJOR REPAIR, MCD FLOOR PANEL 251ZGHAS BROKE REPLACE FLOOR PANEL 251ZG FABRICATION IS COMPLETE IAW SREO-16407-REQ001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026042759076Seat Track · crackedMDC, FLOOR STR, FR 79, -Y1580, SEAT TRACK LOWER ANGLE WITH CRACK. REMOVED ANGLE AT FLOOR STR, FR 79 -Y1580 RH SIDE IAW SRM 51-40-21-001. INSTALLED NEW BRACKET AT FLOOR STR, FR 79 -Y1580 RT SIDE IAW SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026042759042Profile · crackedMDC FLOOR S, FR 74, -Y2127.5, Z PROFILE WITH CRACK. REMOVED Z-PROFILE FROM MDC FLOOR STR, AT FR74, -Y2127.5 RT IAW SRM 51-40-21. INSTALLED NEW Z PROFILE AT Z200 - MDC FLOOR STR, FR 74, -Y2127.5, IAW SRM 51-40-21-001.Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042159328Adapter · corrodedMAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 57.1 Y "0" LH CLS ADAPTER GOUGED. DOT 28-96. REMOVED CORROSION AND GOUGED ON MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 57.1 Y "0" LH CLS ADAPTER AND ORIGINAL THICKNEES IS .240", MATRIAL LOST IS .039" AND REMAINING THICApr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026042459149Floorbeam · bentMDC FR 48, BTW -Y450 AND -Y954, CROSSBEAM BENT. REMOVED AND REPLACED THE FLOORBEAM IAW SREO-75878-REQ001 (APPX B).Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2026042459183Floorbeam · bentMDC FR 50, BTW -Y450 AND -Y954, FLOORBEAM BENT. REMOVED AND REPLACED CROSSBEAM AT MDC FR50, BTW -Y450 AND -Y954 IAW SREO-75878-REQ001 (APPX B).Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2026042459151Crossbeam · bentMDC FLOOR STR, FR 49, BTW -Y450 AND -Y954, CROSSBEAM BENT. REMOVED AND REPLACED CROSSBEAM AT MDC FLOOR STR, FR49, BTW -Y450 AND -Y954 IAW SREO-75878-REQ001 ((APPX B)).Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026050238789Adapter · corrodedCLS ADAPTER AT Y0 FRAME 28 R/H WITH CORROSION. DOT AC-017. INSTALL 2 EACH CLS ADAPTER PER DRAWING B53774150 AT FR28 Y0 LT & RT LOCATION. IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026050736877Support · crackedFAULT: STR- Z410- NO.1 ENGINE TOP OF PYLON PRESSURE RELIEF DOOR SUPPORT IS CRACKED INSTALLED #1 ENGINE TOP OF PYLON PRESSURE RELIEF DOOR SUPPORT IAW A300-AMM 54-52-61/401 ITEM C (4).Apr 10, 2026 · N141UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026051230823Floor Support · crackedAFT CARGO DOOR SILL FLOOR SUPPORT BETWEEN C60 AND C61 HAS CORROSION. SILL FLOOR SUPPORT AFT CARGO ENTRANCE REMOVED AND REPLACED IAW A300-600F SRM 51-72-10-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050731344Seal Depressor · gougedAFT CARGO DOOR SEAL DEPRESSOR HAS MULTIPLE GOUGES FROM 3" TO 24" ABOVE THE FWD LWR CORNER. REMOVED AND REPLACED DOOR SEAL DEPRESSOR IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026050544404Skin · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL HAS (1EA) CRACK. REMOVED SKIN FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SKIN PANEL IAW A300-600 SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026050544443Bracket · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL, CURVED SUPPORT BRACKET HAS (1EA) CRACK. REMOVED CURVED SUPPORT BRACKET FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026041036299Stiffener · crackedSTIFFENER BETWEEN FRAMES 38.1-38.2 R/H SIDE WITH CRACK. INSTALLED FLOOR ANGLE AT MAIN CABIN FR38.1 TO FR38.2 IAW SRM 51-40-21-001 AND REMOVED PROTECTION ELECTRICAL (EWIS) IAW ESPM 20-54-50-02. REPLACED STIFFENER IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050536213Stiffener · crackedSTIFFENER BETWEEN FRAMES 37-38 R/H SIDE WITH CRACK. REPLACED STIFFENER BETWEEN FRAME 37-38 R/H IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042936056Web · crackedWEB BETWEEN FRAME 79-80 L/H SIDE WITH CRACK. INSTALLED NEW WEB. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 79-80: I.A.W. A300-600 SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050231525Support Bracket · crackedRIGHT WING T/E CHANNEL FWD SUPPORT BRACKET AT NR 3 SPOILER INBD HINGE IS CRACKED. VERIFIED INSTALLATION OF RT WING T/E NR 3 SPOILER INBD. CHANNEL FWD SUPPORT BRACKET IAW SRM 57-51-11-001 PAGE 89, ITEM 310, AND SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026042636124Web · crackedWEB BETWEEN FRAMES 73-74 L/H SIDE WITH CRACK. INSTALLED NEW WEB AT FRAMES 73-74 L/H: IAW SRM 51-40-21-001.Apr 10, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026052625637Floor Panel · damagedMAJOR REPAIR. THS COMPARTMENT FR83-84 LH FWD FLOOR PANEL DISBONDED. VERIFIED REMOVAL OF ACCESS PANEL FROM THS COMPT. FR83 - FR84 LH IAW A300-600 SRM 51-40-21-001Apr 9, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051825110Bracket · damagedVERTICAL STABILIZER RH FWD LOWER FAIRING SUPPORT BRACKET NR 4 HAS ELONGATED HOLE. SUPPORT BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING WAS REMOVED IAW SRM 51-40-21-001. INSTALLED NEW BRACKET ON VERTICAL STABILIZER RH FWD LOWER FAIRING IAW SRM 51-40-21Apr 9, 2026 · N141UP · Airbus A300F4622R · Vertical StabilizerSDR IPXA2026051025803Support Angle · corrodedLEFT UPPER APRON AFT ANGLE SUPPORT CORRODED. REMOVED LH UPPER APRON AFT ANGLE SUPPORT I.A.W A300-600 SRM 51-40-21. INSTALLED NEW (ANGLE SUPPORT) I.A.W SRM 51-40-21.Apr 9, 2026 · N141UP · Airbus A300F4622R · Horizontal Stabilizer StructureSDR IPXA2026040919324Floor Panel · brokenMCD FLOOR PANEL 231MJ IS BROKEN. FLOOR PANEL 231MJ FABRICATION IS COMPLETE IAW SREO-16407-REQ001.Apr 9, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026042920047Floor Panel · damagedMAJOR REPAIR. FLOOR PANEL 231RG IS DAMAGED FLOOR PANEL 231RG FABRICATION IS COMPLETE IAW SREO-16407-REQ001.Apr 9, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026041121387Profile · corruptedTEE PROFILE AT FRAME 80 RT CORNER WITH CRACK. REMOVED AND REPLACED TEE PROFILE.Apr 9, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026060691541Longeron · crackedNR 2 I/B T/R CORE AREA UPPER EDGE RUB STRIP WORN. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97494-REQ1 AND VT-MAE EA 300-5430-27-A4446. REV-.Apr 8, 2026 · N141UP · Airbus A300F4622R · Engine Thrust ReverserSDR IPXA2026053005015Skin · gougedLEFT INBD FLAP, LEADING EDGE, AT RIB 13, 2 GOUGES WITH SEPARATION OF 1.5 INCH EACH OTHER. SKIN INSERT (1EA) AND BUTTSTRAP (2EA) WAS INSTALLED IAW SRM 51-40-21-001 AND SRM 57-50-00-200.Apr 8, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026060904468Spar · crackedFR47 LT FORWARD FITTING UPPER RADIUS. CRACK INDICATION NOTED AND CRACK LENGTH MEASURED 0.245 INCHES. APPROVED.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026060904630Spar · crackedFR47 RT FORWARD FITTING UPPER RADIUS. CRACK INDICATION NOTED AND CRACK LENGTH MEASURED 0.601 INCHES.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026053004969Skin · dentedL/H I/B FLAP, LEADING EDGE, AT 3" LEFT OF RIB 19 WITH 1 DENT. ACCOMPLISHED STEP # 1 OF E.A 300-5752-27-A4487 PRELIMINARY 1. (REMOVED PAINT IAW A300-600 SRM 51-75-20-201). SKIN INSERT (1EA) AND BUTTSTRAP (2EA) WAS INSTALLED IAW A300/600 SRM 51-40-21-001 AND SApr 8, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026053004824Skin · gougedL/H I/B FLAP, LEADING EDGE, AT RIB 16, 2 GOUGES WITH SEPARATION OF 1.5 INCH EACH OTHER. ACCOMPLISHED STEP # 1 OF E.A. 300-5752-27-A4487 PRELIMINARY 1. (BLEND GOUGE DAMAGE MINIMALLY TO REMOVE DAMAGE IAW A300-600 SRM 57-50-00-101 AND SRM 51-73-10. SKIN INSERT ANApr 8, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026051496406Floor Panel · delaminatedPANEL 147AF DELAMINATED , FABRICATION OF PANEL OF 147AF IS COMPLETE IAW SREO-57698-REQ001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051496575Floor Panel · delaminatedPANEL 143DF DELAMINATED, PANEL STORED IN PANEL. FABRICATION OF PANEL OF 143DF IS COMPLETE IAW SREO-57698-REQ001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026052106050Panel · damagedLH WING, PANEL 513AT WITH A SCREW HOLE ELONGATED DOT 53-090. RECEIVED NEW PANEL IAW AIPC 53-15-63-01 ITEM 50. VERIFIED RECEIVED NEW PANEL , AND VERIFIED EFFECTIVITY IAW AIPC 53-15-63-01 ITEM 50. INSTALLATION IS CONTROLLED ON TASKCARD T3F18E007EFYB.Apr 8, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026051304987Bracket · crackedLEFT WING O/B FLAP, I/B SIDE WITH A BRACKET BROKEN DOT 53-074 REMOVED AND INSTALED BRACKET LH WING FLAP, O/B FLAP SIDE I/B PER A300-600 SRM51-40-21 PAR 6 P/N A5796040221400Apr 8, 2026 · N141UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026051392745Support · crackedNR 2 ENG PYLON, LATERAL-O/B SIDE, 424CR ACCESS DOOR PANEL, FWD CUTOUT (RIB 3A) SUPPORT PLATE HAS A CRACK. REMOVED AND REPLACED, NEW FISHPLATE LATERAL-O/B SIDE, 424CR ACCESS DOOR PANEL IAW SRM 51-40-21-001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026051304111Bracket · crackedRIGHT WING CENTER FLAP O/B SIDE BRACKET BROKEN. REMOVED AND REPLACED BRACKET IN RT WING CENTER FLAP O/B SIDE PER SRM 51-40-21 PAR 6.Apr 8, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026050796878Bracket · crackedPANEL 334ET, BRACKET HAS A CRACK. INSTALLED NEW ANGLE (BRACKET) I.A.W A300-600 SRM 51-40-21.Apr 8, 2026 · N141UP · Airbus A300F4622R · Standard Practices/StructuresSDR IPXA2026042191168Exhaust Pipe · gougedNR 2 ENGINE EXHAUST NOZZLE EXTERNAL FWD AREA AT 1 O"CLOCK POSITION IS GOUGED. NEW DOUBLER REPLACEMET INSTALLED IAW CMM 78-10-04-601-C1, & SRM 51-40-21-001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Engine Collector/Tailpipe/NozzleSDR IPXA2026042105195Adapter · corrodedCLS ADAPTER AT Y0 FRAME 57.2 RT WITH CORROSION. REMOVED AND REPLACED CLS ADATPER AT ZONE 200. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 57.2, Y0 RT IAW SRM 51-40-21-001.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026041106001Profile · crackedTEE PROFILE AT FRAME 80 LT CORNER WITH CRACK. REMOVED AND REPLACED THE TEE PROFILE.Apr 8, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042978769Skin · crackedMAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV.Apr 7, 2026 · N141UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026050885125Support Strap · corrodedAFT CARGO COMP, FR 64-65 Y450, CEILING SUPPORT STRAP HAS (2EA) AREAS WITH CORROSION. RESTORED SURFACE PROTECTION IAW SRM 51-21-10 AND SRM 51-75-10.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050785202Support Angle · corrodedAFT CARGO COMP, FR 65 Y953, CEILING SUPPORT ANGLE CORRODED. RESTORED SURFACE PROTECTION IAW A300-600 SRM 51-21-10-001 AND 51-75-10-201.Apr 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
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