# Service difficulty reports: N143UP

A list on [N143UP](https://openairdocs.org/aircraft/N143UP.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 · 311 reports

- [SDR IPXA2026092198456](https://openairdocs.org/sdr/IPXA2026092198456.md): Bushing · damaged · Aug 24, 2026 · N143UP · Airbus A300F4622R · Wing Main, Frame Structure
  > LH 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. _.
- [SDR IPXA2026092956718](https://openairdocs.org/sdr/IPXA2026092956718.md): Floorbeam · corroded · Jul 20, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MAIN 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 FR23
- [SDR IPXA2026091199459](https://openairdocs.org/sdr/IPXA2026091199459.md): Floor Panel · damaged · Jul 16, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR 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 FABRICATION
- [SDR IPXA2026092569549](https://openairdocs.org/sdr/IPXA2026092569549.md): Bracket · cracked · Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR 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. _.
- [SDR IPXA2026080375486](https://openairdocs.org/sdr/IPXA2026080375486.md): Support Fitting · corroded · Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF MAIN DECK ENTRY STOWAGE, FOUND INBD STOWAGE LOWER AFT SUPPORT FITTING WITH CORROSION. INSTALLED CLOSET SUPPORT FITTING IAW SRM 51-40-21-001
- [SDR IPXA2026080175550](https://openairdocs.org/sdr/IPXA2026080175550.md): Support Fitting · corroded · Jul 2, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Structure
  > AFTER 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.
- [SDR IPXA2026072216724](https://openairdocs.org/sdr/IPXA2026072216724.md): Floor Panel · broken · Jun 29, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR 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,
- [SDR IPXA2026083103971](https://openairdocs.org/sdr/IPXA2026083103971.md): Bracket · corroded · Jun 28, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026100189074](https://openairdocs.org/sdr/IPXA2026100189074.md): Floorbeam · corroded · Jun 27, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MAJOR 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. _.
- [SDR IPXA2026082989052](https://openairdocs.org/sdr/IPXA2026082989052.md): Bracket · corroded · Jun 27, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > ***MAIN CABIN COMPARTMENT, FLOOR STRUCTURE FR 21 BETWEEN Y1456-1959 FLOOR BEAM BELOW THRUST BRACKET HAS CORROSION.
- [SDR IPXA2026082980480](https://openairdocs.org/sdr/IPXA2026082980480.md): Support · corroded · Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2026082980668](https://openairdocs.org/sdr/IPXA2026082980668.md): Sidewall Support · corroded · Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2026082980617](https://openairdocs.org/sdr/IPXA2026082980617.md): Sidewall Panel · corroded · Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR IPXA2026070675642](https://openairdocs.org/sdr/IPXA2026070675642.md): Bracket · corroded · Jun 26, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026062975154](https://openairdocs.org/sdr/IPXA2026062975154.md): Wire · disconnected · Jun 26, 2026 · N143UP · Airbus A300F4622R · Light System Wiring
  > DISCONECT EMERGENCY LIGHT ELECTRICAL WIRES FROM CREW DOOR SURROUND PANEL
- [SDR IPXA2026081961801](https://openairdocs.org/sdr/IPXA2026081961801.md): Seat Track · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 -Y24
- [SDR IPXA2026090562461](https://openairdocs.org/sdr/IPXA2026090562461.md): Adapter · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026081962461](https://openairdocs.org/sdr/IPXA2026081962461.md): Adapter · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK, AT FR 27 BTWN Y2462 AND Y1959, CLS ADAPTER TRACK HAS CORROSION.
- [SDR IPXA2026072062512](https://openairdocs.org/sdr/IPXA2026072062512.md): Seat Track · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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, BT
- [SDR IPXA2026062660012](https://openairdocs.org/sdr/IPXA2026062660012.md): Seat Track · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 51-7
- [SDR IPXA2026062659967](https://openairdocs.org/sdr/IPXA2026062659967.md): Seat Track · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO CORRODED FASTENERS, 2 EACH AT FR 19 -Y2462. FASTENERS TREATED AND PAINTED IAW SRM 51-21-10-001
- [SDR IPXA2026062659521](https://openairdocs.org/sdr/IPXA2026062659521.md): Seat Track · corroded · Jun 25, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC 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 53-10-15-101
- [SDR IPXA2026092436790](https://openairdocs.org/sdr/IPXA2026092436790.md): Floor Panel · damaged · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FLOOR PANEL 221UF WITH DAMAGE AT FASTENER HOLES. VERIFIED FABRICATED PANEL 221UF IAW SREO-16407-REQ001 ((APPX B) JOB COMPLETE
- [SDR IPXA2026082936086](https://openairdocs.org/sdr/IPXA2026082936086.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026082930108](https://openairdocs.org/sdr/IPXA2026082930108.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026082930030](https://openairdocs.org/sdr/IPXA2026082930030.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026082636758](https://openairdocs.org/sdr/IPXA2026082636758.md): Fitting · cracked · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > E&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.
- [SDR IPXA2026081936026](https://openairdocs.org/sdr/IPXA2026081936026.md): Seat Track · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 CONTAINE
- [SDR IPXA2026081936758](https://openairdocs.org/sdr/IPXA2026081936758.md): Channel · broken · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > E & 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 51-40-21
- [SDR IPXA2026071536802](https://openairdocs.org/sdr/IPXA2026071536802.md): Floor Panel · damaged · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FLOOR PANEL 222KG WITH DAMAGE AT FASTENER HOLES.
- [SDR IPXA2026071536821](https://openairdocs.org/sdr/IPXA2026071536821.md): Floor Panel · damaged · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, PANEL 221TF WITH HONEYCOMB EXPOSED.
- [SDR IPXA2026070637082](https://openairdocs.org/sdr/IPXA2026070637082.md): Floor Support · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026070630030](https://openairdocs.org/sdr/IPXA2026070630030.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026070630108](https://openairdocs.org/sdr/IPXA2026070630108.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026070636086](https://openairdocs.org/sdr/IPXA2026070636086.md): Adapter · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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 B
- [SDR IPXA2026070237062](https://openairdocs.org/sdr/IPXA2026070237062.md): Shim · corroded · Jun 24, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Bulkhead
  > MAIN 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 51-40
- [SDR IPXA2026100117872](https://openairdocs.org/sdr/IPXA2026100117872.md): Floor Panel · broken · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR PANEL 231KM BROKEN.
- [SDR IPXA2026092217125](https://openairdocs.org/sdr/IPXA2026092217125.md): Support Angle · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026082915608](https://openairdocs.org/sdr/IPXA2026082915608.md): Adapter · corroded · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026082915529](https://openairdocs.org/sdr/IPXA2026082915529.md): Adapter · corroded · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026090717205](https://openairdocs.org/sdr/IPXA2026090717205.md): Shear Web · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026090317375](https://openairdocs.org/sdr/IPXA2026090317375.md): Seat Track · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MDC 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.
- [SDR IPXA2026080417739](https://openairdocs.org/sdr/IPXA2026080417739.md): Seat Track · corroded · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > ***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.
- [SDR IPXA2026082617275](https://openairdocs.org/sdr/IPXA2026082617275.md): Support Plate · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026072717237](https://openairdocs.org/sdr/IPXA2026072717237.md): Profile · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC 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. REVIEWED
- [SDR IPXA2026072717123](https://openairdocs.org/sdr/IPXA2026072717123.md): Profile · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT-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. REVIEWED
- [SDR IPXA2026072317101](https://openairdocs.org/sdr/IPXA2026072317101.md): Frame · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > RIGHT 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.
- [SDR IPXA2026070815934](https://openairdocs.org/sdr/IPXA2026070815934.md): Crossbeam · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAIN 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 (
- [SDR IPXA2026070317003](https://openairdocs.org/sdr/IPXA2026070317003.md): Profile · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR IPXA2026070617170](https://openairdocs.org/sdr/IPXA2026070617170.md): Profile · cracked · Jun 23, 2026 · N143UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC 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.

Next page: https://openairdocs.org/aircraft/N143UP/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 = 'N143UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N143UP/reports

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