# Service difficulty reports: N141UP

A list on [N141UP](https://openairdocs.org/aircraft/N141UP.md).

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

Page 1 of 7 · 314 reports

- [SDR IPXA2026061713896](https://openairdocs.org/sdr/IPXA2026061713896.md): Skin · cracked · May 29, 2026 · N141UP · Airbus A300F4622R · Trailing Edge Flaps
  > TASK T3F18E008M5G0 MISSING REFERENCE TO EO-97438 ACCOMPLISHED REPAIR PER VT-MAE EO-97438-REQ1 AND EA 300-5753-27-A4423, REV. -.
- [SDR IPXA2026080258533](https://openairdocs.org/sdr/IPXA2026080258533.md): Keelbeam · cracked · May 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR REPAIR, DURING HFEC INSPECTION, (2 EA) CRACK INDICATION NOTED AT THE LEVEL OF NLG CONNECTING FITTING ON THE LOWER STIFFENER BTW FR13A AND FR14, LH SIDE. MARKED IN RED. ACCOMPLISHED THE REPAIR PER EA#300-5312-27-A4499 REV -.
- [SDR IPXA2026061658446](https://openairdocs.org/sdr/IPXA2026061658446.md): Keelbeam · cracked · May 7, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Keel
  > MAJOR REPAIR, DURING ROTOTEST, (1 EA) CRACK INDICATION NOTED AT RH FWD LOWER HOLE OF THE KEEL BEAM BTW FR13A AND FR14 AT 4 O'CLOCK POSITION LOOKING I/B. ACCOMPLISHED THE REPAIR PER EA#300-5312-27-A4498 REV -.
- [SDR IPXA2026052279872](https://openairdocs.org/sdr/IPXA2026052279872.md): Skin · cracked · Apr 25, 2026 · N141UP · Airbus A300F4622R · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON, O/B SIDE, INSIDE ACCESS 424ER, AT FR 8 AFT SIDE, STRUCTURE WITH CRACK (PICTURE ATTACHED). DOT 73-184. PERFORMED WELD REPAIR PER P&W SRM 54-50-00-101-C1, FIGURE 107 ON TRAVELER T26/1865914.
- [SDR IPXA2026051932815](https://openairdocs.org/sdr/IPXA2026051932815.md): Bracket · corroded · Apr 22, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > AFT CARGO COMP, FR 54, CENTER R/H FWD BULKHEAD SIDEWALK SUPPORT WITH EXFOLIATION CORROSION. INSTALLED NEW CENTER SIDEWALL SUPPORT AND SAME ANGLE BRACKET (3EA) AT AFT CARGO COMP, FR 54, CENTER R/H FWD BULKHEAD IAW SRM 51-40-21-001.
- [SDR IPXA2026051532789](https://openairdocs.org/sdr/IPXA2026051532789.md): Support · corroded · Apr 22, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - Z100 - STR - AFT CARGO COMP, FR 54, L/H CEILING SUPPORT WITH EXFOLIATION CORROSION. DOT 73-181. AFT CARGO CEILING SUPPORT AND SPLICE ANGLE L/H FR54 REMOVED IAW A300-600F SRM51-40-21-001. INSTALLED NEW CEILING SUPPORT AT AFT CARGO COMP, FR 54, L/H IAW
- [SDR IPXA2026051532791](https://openairdocs.org/sdr/IPXA2026051532791.md): Support · corroded · Apr 22, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO COMP, FR 54, CENTER CEILING SUPPORT WITH EXFOLIATION CORROSION. INSTALLED NEW CEILING SUPPOR AT AFT CARGO COMP, FR 54 IAW SRM 51-40-21-001.
- [SDR IPXA2026061392868](https://openairdocs.org/sdr/IPXA2026061392868.md): Fitting · damaged · Apr 20, 2026 · N141UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > FAULT: STR - Z600 - PER ENG REQUEST FR47 RHS HOLE E MEASURES 0.595". ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-83044-REQ3 AND VT-MAE EA 300-5710-27-A4449, REV. _.
- [SDR IPXA2026060556348](https://openairdocs.org/sdr/IPXA2026060556348.md): Frame · cracked · Apr 17, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Frame
  > CWB CENTER SPAR WEB REINFORCEMENT LH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. VERIFIED E.A.#300-5710-27-A4452, PRELIMINARY 3, STEP 14. C/W VERIFIED BLAIN BUSHES (3EA) INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE 2, REPAIR DWGS R007-12
- [SDR IPXA2026060556413](https://openairdocs.org/sdr/IPXA2026060556413.md): Frame · cracked · Apr 17, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Frame
  > CWB CENTER SPAR WEB REINFORCEMENT RH SIDE. 1(EA) INBOARD UPPER FASTENER HOLE CRACKED. ZONE 142 OUT OF SEQ. INSTALLED WITH NITROGEN LIQUID IN AFFECTED HOLE AS PER FIGURE2, REPAIR DWGS R007-12001 ISSUE C. ACCOMPLISH THE PERMANENT REPAIR PER EO-97608-REQ1 AND
- [SDR IPXA2026042657472](https://openairdocs.org/sdr/IPXA2026042657472.md): Retainer · broken · Apr 17, 2026 · N141UP · Airbus A300F4622R · Wing Main, Frame Structure
  > FAULT-STR-ZONE 500. AFTER REMOVAL OF LH WING PANEL 572PB, (2EA) CRACKS FOUND AT INNER PANEL SEAL RETAINER. INSTALLED NEW PANEL IAW SRM 51-40-21-001.
- [SDR IPXA2026051820851](https://openairdocs.org/sdr/IPXA2026051820851.md): Floor Panel · damaged · Apr 15, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO CMPT, FLOORBOARD 131SG IS DAMAGED (EDGES DELAMINATED). 72-005. FLOORBOARD 131SG FAB IS COMPLETE IAW SREO-57698-REQ001.
- [SDR IPXA2026051120737](https://openairdocs.org/sdr/IPXA2026051120737.md): Floor Panel · damaged · Apr 15, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO CMPT, FLOORBOARD 131MG IS DAMAGED (EDGES DELAMINATED). PANEL 131MG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION
- [SDR IPXA2026051120726](https://openairdocs.org/sdr/IPXA2026051120726.md): Floor Panel · damaged · Apr 15, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > FWD CARGO CMPT, FLOORBOARD 132FE IS DAMAGED. 72-002.
- [SDR IPXA2026051120743](https://openairdocs.org/sdr/IPXA2026051120743.md): Floorboard · damaged · Apr 15, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR FWD CARGO CMPT, FLOORBOARD 132SG IS DAMAGED (EDGES DELAMINATED). 72-004.
- [SDR IPXA2026060499229](https://openairdocs.org/sdr/IPXA2026060499229.md): Skin Panel · gouged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/Skin
  > VISUAL GOUGING FOUND IN (1) HOLE LOCATED AT RT WING BOTTOM SKIN ACCESS DOOR RIBS 24 TO 25. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97614-REQ1 & VT-MAE EA 300-5720-27-A4485
- [SDR IPXA2026060902568](https://openairdocs.org/sdr/IPXA2026060902568.md): Hinge · cracked · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage, Door Hinge
  > THE FWD PIANO HINGE FASTENER #5 ON THE FUSELAGE SIDE, HAS A CRACK IND. (1EA) AT THE 3 O'CLOCK POSITION IN THE ALU. LAYER ONLY. DISCREPANT HOLE LABELED IN BLACK.ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-97613-REQ1 AND VT-MAE EA 300-5236-27-A4450, REV. -.
- [SDR IPXA2026051202947](https://openairdocs.org/sdr/IPXA2026051202947.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 151KG, HONEYCOME DAMAGE IN ALL LATERAL FACES. PANEL 151KG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2026051103069](https://openairdocs.org/sdr/IPXA2026051103069.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 152VF, HONEYCOME WITH DAMAGA ON 2 SPOTS. PANEL 152VF FABRICATED IAW SREO-16407-REQ002, APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.
- [SDR IPXA2026051102976](https://openairdocs.org/sdr/IPXA2026051102976.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 152RF, HONEYCOME BROKEN IN MULTIPLE SPOTS. PANEL 152RF FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2026051103074](https://openairdocs.org/sdr/IPXA2026051103074.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 151MG, HONEYCOME WITH CRACK. PANEL 151MG FABRICATED IAW SREO-16407-REQ002,APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.
- [SDR IPXA2026051103071](https://openairdocs.org/sdr/IPXA2026051103071.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 151UF, HONEYCOME DAMAGE IN ALL L/H SIDE. PANEL 151UF FABRICATED IAW SREO-16407-REQ002. APPX C FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.
- [SDR IPXA2026051102984](https://openairdocs.org/sdr/IPXA2026051102984.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 152UF, HONEYCOME WITH CRACK ON 3 SPOTS. PANEL 152UF FABRICATED IAW SREO-16407-REQ002, APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION SREO.
- [SDR IPXA2026051102945](https://openairdocs.org/sdr/IPXA2026051102945.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 151LG, HONEYCOME DAMAGE IN 3 SPOTS. PANEL 151LG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION.
- [SDR IPXA2026051102979](https://openairdocs.org/sdr/IPXA2026051102979.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 152QF, HONEYCOME DAMAGE ALL LATERAL FACES. PANEL 152QF FABRICATED IAW SREO-16407-REQ002, APPX C FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.
- [SDR IPXA2026051103000](https://openairdocs.org/sdr/IPXA2026051103000.md): Floor Panel · damaged · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor Panel
  > AFT CARGO COMP, FLOOR PANEL 152TF, HONEYCOME DAMAGE ON 3 SPOTS. PANEL 152TF FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO))
- [SDR IPXA2026050801614](https://openairdocs.org/sdr/IPXA2026050801614.md): Floorbeam · corroded · Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > AFT CARGO COMPARTMENT FLOOR STRUCTURE, LH FLOOR BEAM AT FR65 Y140 TO Y805 HAS (3EA) AREAS WITH CORROSION / EXFOLIATION. REMOVE CORROSION DAMAGE ON THE DISCREPANT CROSSBEAM PER A300-600F IAW SRM 51-74-10. CROSS BEAM 1EA, SPLICES 2EA UPLN9496-310-12, SPLICE 1EAU
- [SDR IPXA2026061181171](https://openairdocs.org/sdr/IPXA2026061181171.md): Rib · gouged · Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > FAULT-STR-ZONE 500. LH WING T/E SPOILER #5/6 HINGE SUPPORT FITTING I/B EDGE IS GOUGED. 28-149. ACCOMPLISH THE REPAIR PER EO-97611-REQ1 AND EA 300-5751-27-A4481, REV_.
- [SDR IPXA2026050273186](https://openairdocs.org/sdr/IPXA2026050273186.md): Adapter · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR STR, FR 34, Y0, RT CLS ADAPTER WITH CORROSION. INSTALL 1 EACH CLS ADAPTER IAW DWG B53774150 AT FR34 Y0 RT LOCATION. IAW SRM 51-40-21-001. ACCOMPLISHED PERMANENT REPAIR IAW EO-97389-REQ1 AND VT-MAE EA 300-5314-27-A4442, REV -.
- [SDR IPXA2026060974758](https://openairdocs.org/sdr/IPXA2026060974758.md): Fitting · cracked · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Structure
  > FR47 RH FORWARD FITTING UPPER RADIUS. 01(EA) CRACK INDICATION NOTED WITH A DEPTH OF APPROX. 15MM. COMPLIED WITH EO-18290-JIC004.
- [SDR IPXA2026060480423](https://openairdocs.org/sdr/IPXA2026060480423.md): Fitting · damaged · Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LEFT WING, FR 47 LOWER JUNCTION, HOLE S HAS A VISUAL DAMAGE. ACCOMPLISHED THE REPAIR PER EA 300-5710-27-A4437.
- [SDR IPXA2026050473312](https://openairdocs.org/sdr/IPXA2026050473312.md): Adapter · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STR, FR 28, Y0, L/H CLS ADAPTER WITH CORROSION. INSTALL 2 EACH CLS ADAPTER PER AIRBUS DRAWING B53774150 AT FR28 Y0 LH & RH LOCATION. I.A.W A300-600 SRM 51-40-21-001. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-97126-REQ1 AND VT-MAE EA 300-5
- [SDR IPXA2026052281357](https://openairdocs.org/sdr/IPXA2026052281357.md): Skin · cracked · Apr 13, 2026 · N141UP · Airbus A300F4622R · Wing, Center Box
  > NR 1 PYLON, L/H SIDE, RIB 8, AFT SUPPORT STRUCTURE WITH CRACK. AFTER DETAIL VISUAL INSPECTION CRACK WAS FOUND CRACK LENGTH.750" IAW A300-600 NTM 51-70-00. PERFORMED WELD REPAIR PER P&W SRM 54-50-00-101-C1, FIGURE 107 ON TRAVELER T26/1865915.
- [SDR IPXA2026050673422](https://openairdocs.org/sdr/IPXA2026050673422.md): Seat Track · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR. LT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR35-36 Y450 SEAT TRACK HAS CORROSION. REMOVED DAMAGES AT MAIN CABIN SEAT TRACK CROWN BETWEEN FR35-35 Y450 IAW SRM 51-74-10-201. PERFORMED NTM INSPECTION VISUAL IAW A300-600 SRM 51-70-00-701 AND FOUND
- [SDR IPXA2026051573404](https://openairdocs.org/sdr/IPXA2026051573404.md): Bracket · cracked · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AFT BULKHEAD LT LINNING UPPER SUPPORT BRACKET AT Y953 IS CRACKED. REMOVED BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21. INSTALLED NEW BRACKET AT FR 38.2 Y953 IAW A300 SRM 51-40-21-001.
- [SDR IPXA2026050173414](https://openairdocs.org/sdr/IPXA2026050173414.md): Seat Track · gouged · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR37 Y 0 SEAT TRACK HAS (4EA) GOUGES. REMOVED SEAT TRACK. MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR37 Y 0 IAW SRM 53-10-16-201. INSTALLED SPLICE AND SEAT TRACK. MAIN CABIN
- [SDR IPXA2026043075328](https://openairdocs.org/sdr/IPXA2026043075328.md): Plate · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT-STR-ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL HAS CORROSION. REMOVED CORROSION AT LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21 Y0-Y450 METAL RIVETED FLOOR PANEL, ORIGINAL THICKNESS IS.129", MATERIAL LO
- [SDR IPXA2026042173310](https://openairdocs.org/sdr/IPXA2026042173310.md): Adapter · broken · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FLOOR STR, FR 35, BTW -Y1959 AND -Y2462, DIAMOND CLS ADAPTER BROKEN. INSTALLED NEW DIAMOND CLS ADAPTER IAW SRM 51-40-21-001.
- [SDR IPXA2026050481474](https://openairdocs.org/sdr/IPXA2026050481474.md): Skin · gouged · Apr 13, 2026 · N141UP · Airbus A300F4622R · Trailing Edge Flaps
  > RH WING INNER FLAP UPPER SURFACE I/B AFT AREA GOUGED. REMOVED GAUGED ON RT WING INNER FLAP UPPER SURFACE I/B AFT AREA IAW SRM 51-73-10.CK LIMITS. ORIG. MAT 0.031". MAT.LOSS 0.001".MAT.REMAINING.0.030".FOUND TO BE IN LIMITS IAW SRM 57-50-00.TR99333.OK TO RESTO
- [SDR IPXA2026050175026](https://openairdocs.org/sdr/IPXA2026050175026.md): Seat Track · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR26-27 Y"0" SEAT TRACK HAS (2EA) AREAS WITH CORROSION. DOT 28-122. REMOVED CORROSION (2EA) AREAS AND REMOVED FASTENERS (5EA), UPPER AREA (1). INSTALL NEW RIVETS (5EA) IAW A300-600 SRM 51-21-10-001 AND SRM 51-75-10-201 AN
- [SDR IPXA2026042973327](https://openairdocs.org/sdr/IPXA2026042973327.md): Adapter · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STR, FROM FR 23 TO FR 27, Y0, R/H BASE CLS ADAPTER TRACK AND CLS ADAPTERS, 6 SPOTS WITH CORROSION. DOT 73-125. REMOVED MINOR CORROSION AT - Z200 - MDC FLOOR STR, FROM FR 24 TO FR 27, Y0, R/H BASE CLS ADAPTER TRACK AND ADAPTER IAW A300-600 SRM 51-74-1
- [SDR IPXA2026043075004](https://openairdocs.org/sdr/IPXA2026043075004.md): Adapter · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > LEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21-27 Y0-Y450 CLS TRACK BASE HAS (15EA) AREAS WITH CORROSION. REMOVED CORROSION AT ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR21-27 Y0-Y450 CLS TRACK IAW A300-600 SRM 51-74-10-204. INSTALLED NEW CLS TRA
- [SDR IPXA2026042173332](https://openairdocs.org/sdr/IPXA2026042173332.md): Adapter · corroded · Apr 13, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC FLOOR STR, FR 20, -Y1959, L/H CLS ADAPTER WITH CORROSION. VERIFIED CLS ADAPTER REPLACED PER SRM 51-40-21-001.JOB COMPLETE.
- [SDR IPXA2026060367876](https://openairdocs.org/sdr/IPXA2026060367876.md): Retainer · cracked · Apr 12, 2026 · N141UP · Airbus A300F4622R · Cargo/Baggage Doors
  > FAULT: APG-800-MDC DOOR UNDERNEATH NR 2 LATCHING HOOK HAS STRUCTURE DAMAGE. 33-040 ACCOMPLISHED PERMANENT REPAIR PER EA 300-5236-27-A4484 REV. -.
- [SDR IPXA2026042468432](https://openairdocs.org/sdr/IPXA2026042468432.md): Floor Support · broken · Apr 12, 2026 · N141UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT-STR-ZONE 200 MAIN CABIN DECK, FLOOR SUPPORT STRUCTURE LH SIDE NEXT TO FLOOR SUPPORT Y-1959 BTW FR12A AND FR14 WITH A BRACKET BROKEN DOT 53-118. REMOVED DAMAGE BRACKET ON MAIN CABIN DECK, AT FLOOR SUPPORT STRUCTURE R/H SIDE NEXT TO FLOOR SUPPORT Y-1959
- [SDR IPXA2026060649113](https://openairdocs.org/sdr/IPXA2026060649113.md): Longeron · gouged · Apr 11, 2026 · N141UP · Airbus A300F4622R · Nacelle/Pylon, Longeron/Stringer
  > NR 1 O/B T/R CORE AREA UPPER EDGE CLIP WORN. NR 1 O/B T/R CORE AREA UPPER EDGE CLIP WORN IT WAS REPAIRED IAW SREO-40521-REQ001 ((APPX A)
- [SDR IPXA2026060159035](https://openairdocs.org/sdr/IPXA2026060159035.md): Skin · corroded · Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Plate/Skin
  > MAIN DECK BELOW SEAT AT -Y2462 FR.47, CENTER BOX UPPER SURFACE HAS CORROSION, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-97388-REQ1 AND VT-MAE EA 300-5710-27-A4436, REV. -.
- [SDR IPXA2026051952845](https://openairdocs.org/sdr/IPXA2026051952845.md): Bracket · damaged · Apr 11, 2026 · N141UP · Airbus A300F4622R · Spoilers
  > PANEL RACK, PANEL 672GB I/B ATTACH FITTING HOLES ELOGATED 2EA. INSTALLED NEW BRACKET ATTACHMENTS, I/B BRACKET AND O/B, BRACKET IAW A300-600 SRM 51-40-21-001.
- [SDR IPXA2026052248926](https://openairdocs.org/sdr/IPXA2026052248926.md): Web · cracked · Apr 11, 2026 · N141UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > FAULT-STR-ZONE400: NO.1 PYLON WEB INSIDE PANEL 413EL IS CRACKED. DOT NO. 17-48. ACCOMPLISHED WELD REPAIR PER P&W SRM 54-50-00-101-C1, FIGURE 107 ON TRAVELER T26/1865912.
- [SDR IPXA2026042759037](https://openairdocs.org/sdr/IPXA2026042759037.md): Seat Track · corroded · Apr 11, 2026 · N141UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > LEFT MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 79-80 Y1137.1 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK AT ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR STRUCTURE FR 79-80 Y1137.1 IAW 51-40-21. INSTALLED SEAT TRACK AT ZONE 200. LH MAIN CABIN COMPARTMENT FLOOR

Next page: https://openairdocs.org/aircraft/N141UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N141UP/reports

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