N143UP

Service difficulty reports · 311

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 = 'N143UP' 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 IPXA2026092198456Bushing · damagedLH WING LOWER SKIN COVER LANDING BETWEEN RBS 26 - 27 16.5 OUTBOARD OF RIB 26 AFT HAS A .545" HOLE AT NUTPLATE LOCATION. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98641-REQ1 AND STE PNA EA 300-5720-27-A4609, REV. _.Aug 24, 2026 · N143UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2026092956718Floorbeam · corrodedMAIN DECK, AFTER REMOVAL FLOOR STRUCTURE NEXT TO FR22, FOUND CORROSION AT FLOOR BEAM FR23 BTWN Y1456 AND Y1959. 4 GIVEN OK (INSTALL) RESTORE INITIAL CONDITION AT MAIN CABIN COMPARTMENT, FLOOR STRUCTURE NEXT TO FR 22 AND FR23Jul 20, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2026091199459Floor Panel · damagedMAJOR REPAIR, FWD CARGO COMP FLOOR PANEL 132MG HAS CORNER BROKEN. PANEL 132MG IS FABRICATED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATIONJul 16, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092569549Bracket · crackedMAJOR REPAIR, FWD CARGO PIT, AFTER REMOVAL OF PRESSURE DECK UPPER SURFACE FR39/40, FOUND BRACKET DAMAGED AT FR39 Y0. DOT 90-101. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-98656-REQ1 AND STE PNA EA 300-5315-27-A4568, REV. _.Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026080375486Support Fitting · corrodedAFTER REMOVAL OF MAIN DECK ENTRY STOWAGE, FOUND INBD STOWAGE LOWER AFT SUPPORT FITTING WITH CORROSION. INSTALLED CLOSET SUPPORT FITTING IAW SRM 51-40-21-001Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026080175550Support Fitting · corrodedAFTER REMOVAL OF MAIN DECK ENTRY STOWAGE, FOUND I/B STOWAGE LOWER AFT SUPPORT FITTINGS (2EA) WITH CORROSION. DOT 28-103. INSTALLED FITTINGS (2EA) IAW SRM 51-40-21-001.Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026072216724Floor Panel · brokenMAJOR REPAIR, FAULT-MCD FLOOR PANEL 241DN IS BROKEN FABRICATION OF PANEL 241DN IS COMPLETE IAW SREO-16407-REQ001 ((APPX B) MAIN DECK CARGO BAY FLOOR PANEL FABRICATION. PANEL INSERTS EDGE FILL, GLUE,Jun 29, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026083103971Bracket · corrodedMAIN DECK, AT FR20 NEXT TO Y1959, FLOOR STRUCTURE HAS CORROSION. VERIFIED APPLICATION OF SURFACE PROCTECTION ON NEW BRACKET IAW SRM 51-21-10-001 AND SRM 51-75-10-201.Jun 28, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100189074Floorbeam · corrodedMAJOR REPAIR, MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 22 BETWEEN Y1456-1959 FLOORBEAM BELOW THRUST BRACKET HAS CORROSION. DOT 28-53. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97978-REQ1 AND STE PNA EA 300-5313-27-A4539, REV. _.Jun 27, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2026082989052Bracket · corroded***MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 21 BETWEEN Y1456-1959 FLOOR BEAM BELOW THRUST BRACKET HAS CORROSION.Jun 27, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082980480Support · corrodedAFT CARGO COMP LH SIDEWALL PANEL STRUCTURE HAS SURFACE CORROSIONS BETWEEN FR.57.3 TO FR.59. INSTALLED NEW PROFILE IAW SRM 51-40-21-001.Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082980668Sidewall Support · corrodedAFT CARGO COMP. RH SIDEWALL PANEL SUPPORT FITTING HAS SURFACE CORROSION AT FR.57. INSTALLED NEW RH SIDEWALL PANEL SUPPORT FITTING IAW A300-600 SRM 51-40-21-001.Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082980617Sidewall Panel · corrodedAFT CARGO COMP. RT SIDEWALL PANEL STRUCTURE CORRODED AT UPPER LT CORNER BS 3353. FR.54. INSTALLED NEW CORNER PROFILE IAW SRM 51-40-21-001.Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070675642Bracket · corrodedMAIN DECK, FROM FR21 TO FR22, NEXT TO SEAT TRACK Y1959, FLOOR STRUCTURE HAS CORROSION. FABRICATED NEW BRACKET IAW GMM 09.08.01.03 AND SRM 53-13-15-001 FIGURE 5 ITEM 90.Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026062975154Wire · disconnectedDISCONECT EMERGENCY LIGHT ELECTRICAL WIRES FROM CREW DOOR SURROUND PANELJun 26, 2026 · N143UP · Airbus A300F4622R · Light System WiringSDR IPXA2026081961801Seat Track · corrodedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 28-32 RH -Y2462 SEAT TRACK HAS (7EA) SPOTS WITH CORROSION. . INSTALLATION OF NEW SEAT TRACK P/N: R5307007120600, 2EA SPLICE, 12EA ANGLE AND 6EA PROFILE-U AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 28-32 RH -Y24Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026090562461Adapter · corrodedMAIN DECK, AT FR 27 BTWN Y2462 AND Y1959, CLS ADAPTER TRACK HAS CORROSION. INSTALLED A NEW PLATE LINING AT MAIN DECK, AT FR 27 BTWN Y2462 AND Y1959 IAW SRM 51-40-21-001.Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026081962461Adapter · corrodedMAIN DECK, AT FR 27 BTWN Y2462 AND Y1959, CLS ADAPTER TRACK HAS CORROSION.Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026072062512Seat Track · corrodedMAIN DECK, FROM FR21 TO FR26, BTWN Y0 AND Y450, CLS ADAPTER TRACK HAS CORROSION. REMOVED CLS ADAPTER TRACK FROM MAIN DECK FR21 TO FR27, BTWN Y0 AND Y450 IAW A300-600 SRM 51-40-21-001. INSTALLED NEW PART (CLS ADAPTER TRACK) AT MAIN DECK, FROM FR21 TO FR26, BTJun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026062660012Seat Track · corrodedMAIN DECK CARGO CORRODED FASTENERS (4EACH) BETWEEN FR 19 AND FR 20 .-Y2462 AND -Y1959/DOT.130.040 PERFORMED CORROSION REMOVAL (4EA) FASTENERS, FOUND FASTENERS WITH NO MATERIAL LOSS AND FASTENER CODE STILL LEGIBLE. REF SRM 51-74-10-201, CHAPTER D, & SRM 51-7Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026062659967Seat Track · corrodedMAIN DECK CARGO CORRODED FASTENERS, 2 EACH AT FR 19 -Y2462. FASTENERS TREATED AND PAINTED IAW SRM 51-21-10-001Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026062659521Seat Track · corrodedMDC FR 24 FLOOR PNL 232SG SEAT TRACK EVIDENCE OF CORROSION. CORROSION WAS FOUND ON THE MAIN DECK CARGO CLS ADAPTER BETWEEN FR26 & FR27 Y0 RH. AFTER FURTHER EVALUATION, EXFOLIATION CORROSION WAS IDENTIFIED. DAMAGE WAS FOUND OUTSIDE LIMITS IAW SRM 53-10-15-101Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026092436790Floor Panel · damagedMAJOR REPAIR, FLOOR PANEL 221UF WITH DAMAGE AT FASTENER HOLES. VERIFIED FABRICATED PANEL 221UF IAW SREO-16407-REQ001 ((APPX B) JOB COMPLETEJun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026082936086Adapter · corrodedMAIN DECK CARGO CLS ADAPTER CORRODED AT BETWEEN FR 29 & FR 28 STR Y0. INSTALLED A NEW CLS ADAPTER STR-MAIN DECK CARGO, AT BETWEEN FR.29 & FR.28 STR.Y0 IAW SRM 51-40-21-001.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082930108Adapter · corrodedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 30 Y0 LH CLS ADAPTER HAS CORROSION. INSTALLED NEW CLS ADAPTER MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 30 Y0 LT IAW SRM 51-40-21-001.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082930030Adapter · corrodedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 33 Y0 LT CLS ADAPTER HAS CORROSION. INSTALLED NEW CLS ADAPTER FLOOR STRUCTURE FR 33 Y0 LT IAW SRM 51-40-21-001.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082636758Fitting · crackedE&E, CHANNEL BROKEN BETWEEN FR 14-FR16&CL-Y-450 UNDERNEATH PANEL 221UF (REFERENCE, PANEL 106VU BACK UPPER SIDE). INSTALLED 2 NEW FITTINGS I.A.W. SRM 51-40-21.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026081936026Seat Track · corrodedMAIN CARGO DECK SEAT TRACK FLANGE CORRODED AT FR.30 STR.-Y1959/DOT.130.029 REPAIR IAW:REPAIR SEAT TRACK PER SRM REV 43, 53-10-16-201 PARAGRAPH 4 FIGURE 201. THIS IS A CATEGORY A REPAIR AND NO FURTHER ACTION IS REQUIRED. CAUTION: THE WORK INSTRUCTIONS CONTAINEJun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026081936758Channel · brokenE & E, CHANNEL BROKEN BETWEEN FR 14- FR16 & CL - Y-450 UNDERNEATH PANEL 221UF (REFERENCE, PANEL 106VU BACK UPPER SIDE) (DOT 64-073) INSTALLED 2 NEW FITTINGS I.A.W. A300-600 SRM 51-40-21Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026071536802Floor Panel · damagedMAJOR REPAIR, FLOOR PANEL 222KG WITH DAMAGE AT FASTENER HOLES.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026071536821Floor Panel · damagedMAJOR REPAIR, PANEL 221TF WITH HONEYCOMB EXPOSED.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026070637082Floor Support · corrodedMAIN DECK, CORROSION AT INTERCOSTAL Y730 BETWEEN FR13A & FR11 UPPER AND LOWER SURFACE. REMOVED AND REPLACE INTERCOSTAL ON MAIN DECK, Y730 BETWEEN FR13A & FR11 UPPER AND LOWER SURFACE IAW SRM 51-40-21.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070630030Adapter · corrodedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 33 Y0 LT CLS ADAPTER HAS CORROSION. REMOVED CLS ADAPTER FR 33 Y0 LT IAW SRM 51-40-21-001.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070630108Adapter · corrodedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 30 Y0 LH CLS ADAPTER HAS CORROSION. REMOVED CLS ADAPTER FR 30 Y0 LH IAW SRM 51-40-21-001.Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070636086Adapter · corrodedMAIN DECK CARGO CLS ADAPTER CORRODED AT BETWEEN FRA.29 & FR.28 Y0. CORROSION IN MAIN DECK CARGO CLS ADAPTER AT BETWEEN FRA.29 & FR.28 STR.Y0. AFTER FURTHER EVALUATION FOUND EXFOLIATED CORROSION. FOUND OUT LIMITS IAW SRM 53-10-15-101. REMOVED CLS ADAPTER AT BJun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070237062Shim · corrodedMAIN DECK, BOLT RECEPTACLE AT COCKPIT ENTRY BULKHEAD LOWER SIDE, BETWEEN INTERCOASTAL Y730 & Y953 WITH CORROSION. INSTALLED AND COATED NEW SHIM FOR MAIN DECK, BOLT RECEPTACLE AT COCKPIT ENTRY BULKHEAD LOWER SIDE, BETWEEN INTERCOASTAL Y730 & Y953 IAW SRM 51-40Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR IPXA2026100117872Floor Panel · brokenMAJOR REPAIR, MDC FLOOR PANEL 231KM BROKEN.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092217125Support Angle · crackedMAIN CABIN FLOOR STRUCTURE FR 79 -Y1580.5 SEAT TRACK LOWER SUPPORT ANGLE HAS (1EA) CRACK. NEW ANGLE AT MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 79 -Y1580.5 SEAT TRACK LOWER SUPPORT IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082915608Adapter · corrodedMAIN DECK FLOOR STRUCTURE, AT FR 34 BTWN -Y0 AND -Y450, CLS ADAPTER HAD CORROSION. INSTALLED NEW CLS ADAPTER MAIN DECK FLOOR STRUCTURE, AT FR 34 BTWN -Y0 AND -Y450, IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026082915529Adapter · corrodedMAIN DECK FLOOR STRUCTURE, AT FR 30 BTWN -Y0 AND -Y450, CLS ADAPTER HAS CORROSION. INSTALLED NEW CLS ADAPTER AT FR 30 BTWN -Y0 AND -Y450, IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026090717205Shear Web · crackedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 78, O/B RH WEB HAS (1EA) CRACK. INSTALLED NEW WEB. MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 78, O/B RH IAW SRM 51-40-21.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026090317375Seat Track · crackedMDC LT SIDE, LOWER ANGLE SUPPORT OF SEAT TRACK Y1580.5 AT FR79 WITH CRACK, REMOVED AND REPLACED ANGLE ON MDC LH SIDE, LOWER ANGLE SUPPORT OF SEAT TRACK IAW SRM 51-40-21.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026080417739Seat Track · corroded***MAJOR REPAIR*** MDC LH SIDE, FLOOR SEAT TRACK Y953 AT FR 62 WITH CORROSION. REMOVED CORROSION ON MDC LH SIDE, FLOOR SEAT TRACK Y794.3 AT FR 62. INSTALLED NEW SEAT TRACK AND 4EA SEAT TRACK SPLICES IAW A300-600 SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026082617275Support Plate · crackedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR74 RH O/B WEB HAS (1EA) CRACK ON LOWER SURFACE. INSTALLED 1EA WEB AND 1 EA ANGLE IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026072717237Profile · crackedMDC LH SIDE, FLOOR "Z" PROFILE AT SIDE WALL LH FR 79 WITH CRACK DOT 31-061. INSTALLED NEW PROFILE-Z IAW A300-600 SRM 51-40-21-001. REVIEWEDJun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026072717123Profile · crackedFAULT-Z200-STR, MDC LH SIDE, FLOOR "Z" PROFILE ANGLE AT REAR BULHEAD FR 80 WITH CRACK, DOT 31-059. INSTALLED Z PROFILE ANGLE IAW A300-600 SRM 51-40-21. REVIEWEDJun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026072317101Frame · crackedRIGHT WING PYLON FAIRING 485AL FRAME NR 1 FWD OTBD SUPPORT ANGLE CRACKED AT UPPER INNER RADIUS AREA. INSTALLED A NEW ANGLE ON PYLON LOWER FAIRING 485AL FRAME NR 1 FWD OTBD SUPPORT IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026070815934Crossbeam · crackedMAIN DECK FLOOR STRUCTURE, AT FR 51 BTWN -Y450 AND -Y953, CROSSBEAM BROKEN. INSPECTED AND VERIFIED STEP#4 ACCOMPLISHED REPLACEMENT OF CROSSBEAM APPLYING STEPS 1 TO 6 OF SREO-75878-REQ001 ((APPX B) A300: MAIN DECK CARGO FLOOR CROSSBEAMS, FR48 - FR54 - MODIFY (Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026070317003Profile · crackedMAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 80-82 AFT RT OTBD ZEE PROFILE HAS (1EA) CRACK. FR82 AFT O/B, ZEE PROFILE REMOVED IAW SRM 51-40-21-001. INSTALLED NEW PART P/N P/N A53981401201, BATCH #4496047, IAW SRM 51-40-21-001.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026070617170Profile · crackedMDC LT SIDE, FLOOR TEE PROFILE AT REAR BULKHEAD FR 80 WITH CRACK, REMOVED ANGLE ON MDC LT SIDE, FLOOR ZEE PROFILE AT REAR BULKHEAD FR 80 IAW SRM 51-40-21-001. INSTALLED NEW PART (PROFILE T) AT MDC LT SIDE, AT REAR BULKHEAD FR 80.Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
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