# Service difficulty reports: N145UP

A list on [N145UP](https://openairdocs.org/aircraft/N145UP.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 6 · 252 reports

- [SDR IPXA2026061686256](https://openairdocs.org/sdr/IPXA2026061686256.md): Indication Sys · no test · Jun 16, 2026 · N145UP · Airbus A300F4622R · Door Warning System
  > WHEN CLOSING ENTRY DOOR TO SECURE FOR FLIGHT DOOR BUZZER & LIGHT WOULD NOT TEST. PLACED ON DMI IAW A300 MEL 52-11-01-2-4. SLIDE BUZZER AND LIGHT TESTS NORMAL REF MM 52-73-00/0501.
- [SDR IPXA2026060289725](https://openairdocs.org/sdr/IPXA2026060289725.md): Mount · damaged · May 8, 2026 · N145UP · Airbus A300F4622R · Engine Mount Section
  > REMOVE AND ROUTE FITTING (#1 ENGINE MOUNT) P/N A5461092600000. FROM A/C N145UP TO N141UP. INSTALLATION OF THE AFT FITTING MOUNT PER AMM 54-51-85/401. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97566-REQ1 AND VT-MAE EA 300-5451-27-A4492, REV. _.
- [SDR IPXA2026051534276](https://openairdocs.org/sdr/IPXA2026051534276.md): Bracket · missing · Apr 16, 2026 · N145UP · Airbus A300F4622R · Wing Structure
  > MISSING BRACKET PN: A5796554820500 ON MOVABLE FAIRING 635BB. INSTALLED BRACKET P/N: A57965548205; TRAVELER #: T26/1865162 IN ZONE 600 ON MOVABLE FAIRING 635BB. IAW AIRBUS AIPC 27-51-65-11 ITEM 30, SRM 57-20-35-001 PAG.11 AND SRM 51-40-21-001.
- [SDR IPXA2026032132345](https://openairdocs.org/sdr/IPXA2026032132345.md): Spar Web · cracked · Feb 27, 2026 · N145UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > NR 1 PYLON LOWER SPAR EXTENTION UNDER AFT FAIRING, DRAIN LINE UNION MOUNT STRUCTURE CRACKED/BROKEN. INSTALLED SPAR EXTENTION AT #1 PYLON LOWER AFT, UNDER AFT FAIRING, DRAIN LINE UNION MOUNT STRUCTURE IAW A300-600 SRM 51-40-21-001
- [SDR IPXA2026021574651](https://openairdocs.org/sdr/IPXA2026021574651.md): Web · cracked · Feb 12, 2026 · N145UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON AFT FAIRING SURFACE WEB HAS CRACK WEB FAIRING SURFACE WAS REMOVED IAW A300/600 SRM 51-40-21 WEB WAS INSTALLED IAW A300/600 SRM 51-40-21
- [SDR IPXA2026030403971](https://openairdocs.org/sdr/IPXA2026030403971.md): Spar · cracked · Feb 4, 2026 · N145UP · Airbus A300F4622R · Wing Spar
  > RH WING FR47 CWB LOWER ANGLE. CRACK INDICATION NOTED ON HOLE T IN ALL LAYERS AT 3 O' CLOCK POSITION. REJECTED - EO-96608-REQ1 NOT ATTACHED
- [SDR IPXA2026021974608](https://openairdocs.org/sdr/IPXA2026021974608.md): Angle · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMP, FR10, BY Y1456, ANGLE PICKUP IS CRACKED. REMOVED BRACKET ANGLE PICKUP AT AVIONICS COMP, FR10, BY Y1456 WITH CRACK IAW A300-600 SRM 51-40-21. INSTALLED NEW ANGLE P/N UPA53612450200 AT STR-Z100- AVIONICS COMP, FR10, BY Y1456 IAW A300-600 SRM 51-
- [SDR IPXA2026021974623](https://openairdocs.org/sdr/IPXA2026021974623.md): Bracket · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > AVIONICS COMP, FR10, BY -Y1456, ANGLE PICKUP IS CRACKED. REMOVED ANGLE PICKUP WITH CRACK AT AVIONICS COMP, FR10, BY -Y1456 IAW A300-600 SRM 51-40-21. INSTALLED NEW ANGLE P/N UPA53610814204 AT STR-Z100- AVIONICS COMP, FR10, BY -Y1456 IAW A300-600 SRM 51-40-21
- [SDR IPXA2026021374330](https://openairdocs.org/sdr/IPXA2026021374330.md): Bracket · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > R/H WING CENTER FLAP, O/B SIDE WITH 1EA ANGLE BRACKET CRACKED. REMOVED AND REPLACED ANGLE BRACKET AT STR-Z600-RT WING CENTER FLAP OTBD SIDE IAW SRM 51-40-21.
- [SDR IPXA2026020375549](https://openairdocs.org/sdr/IPXA2026020375549.md): Support Bracket · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Bulkhead
  > AFT CARGO, AFT FACE OF BULKHEAD 54, RH SIDE, -Y1959, PANEL SUPPORT BRACKET HAS A CRACK. DOT 103-20. REMOVED BRACKET AT Z100, AFT CARGO, AFT FACE OF BULKHEAD FR54, RH SIDE, -Y1959, I.A.W. A300-600 SRM 51-40-21. ++INSTALLED NEW BRACKET I.A.W. A300-600 51-40-21,
- [SDR IPXA2026020674773](https://openairdocs.org/sdr/IPXA2026020674773.md): Support Angle · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMP, FR10, BY Y679, ANGLE SPRT IS CRACKED. REMOVED ANGLE SPRT WITH CRACK AT AVIONICS COMP, FR10, BY Y679 IAW A300-600 SRM 51-40-21 INSTALLED ANGLE SUPPORT AV. COMP. AT FR10, BY Y679 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026020674785](https://openairdocs.org/sdr/IPXA2026020674785.md): Support Angle · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT-SAVIONICS COMP, FR10, BY Y233, ANGLE SPRT IS CRACKED. REMOVED ANGLE SPRT WITH CRACK AT AVIONICS COMP, FR10, BY Y233 IAW A300-600 SRM 51-40-21 INSTALLED ANGLE SUPPORT AV. COMP. AT FR10, BY 233 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026020674727](https://openairdocs.org/sdr/IPXA2026020674727.md): Support Angle · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AVIONICS COMP, FR10, BY -Y953, ANGLE SPRT IS CRACKED. REMOVED ANGLE SPRT WITH CRACK AT AVIONICS COMP, FR10, BY -Y953 IAW SRM 51-40-21. INSTALLED ANGLE SUPPORT AV. COMP. AT FR10, BY -Y953 IAW SRM 51-40-21.
- [SDR IPXA2026020469257](https://openairdocs.org/sdr/IPXA2026020469257.md): Brace · cracked · Jan 25, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > M.C. DECK FR#38.1 RH DIAGONAL BRACE CRACKED WHERE THE FLOOR MEETS THE SIDEWALL INSTALLED SMOKE TUBE AT FR 38.1 RH MAIN DECK IAW. A300 SRM 51-40-23. REVIEWED
- [SDR IPXA2026052763514](https://openairdocs.org/sdr/IPXA2026052763514.md): Angle · corroded · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT AFT BULKHEAD FR 39-40 -Y450 UPPER SURFACE HAS EXFOLIATION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97465-REQ1 AND VT-MAE EA 300-5315-27-A4331, REV. -.
- [SDR IPXA2026030367324](https://openairdocs.org/sdr/IPXA2026030367324.md): Housing · corroded · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > NUMBER 4 R/A ANTENNA (5SA2) HOUSING CORRODED AROUND DOME NUT AND CUTOUT AREA. INSTALLED NEW R/A HOUSING IAW SRM 51-40-21.
- [SDR IPXA2026021263591](https://openairdocs.org/sdr/IPXA2026021263591.md): Support Bracket · cracked · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 RH -Y450 LINING UPPER SUPPORT BRACKET CRACKED. REMOVED SUPPORT BRACKET AT FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 RH -Y450 IAW A300 SRM 51-40-21. INSTALLED NEW SUPPORT BRACKET AT FWD CARGO COMPARTMENT AFT BULKHEAD F
- [SDR IPXA2026021363590](https://openairdocs.org/sdr/IPXA2026021363590.md): Support Bracket · cracked · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 LH Y450 LINING UPPER SUPPORT BRACKET CRACKED. REMOVED BRACKET AT -STR-ZONE 100. FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 LH Y450 LINING UPPER SUPPORT BRACKET IAW TO A300-600 51-40-21 BRAKET CRACKED. INSTALLED BRACKET
- [SDR IPXA2026021263613](https://openairdocs.org/sdr/IPXA2026021263613.md): Support Bracket · cracked · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Bulkhead
  > FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 LH Y953 LINING UPPER SUPPORT BRACKET CRACKED. DOT 28-29. REMOVED SUPPORT BRACKET AT FWD CARGO COMPARTMENT AFT BULKHEAD FR 38 LH Y953 IAW A300 SRM 51-40-21. ++INSTALLED NEW SUPPORT BRACKET AT FWD CARGO COMPARTMENT AFT BU
- [SDR IPXA2026021765232](https://openairdocs.org/sdr/IPXA2026021765232.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131GE EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 131GE IS COMPLETED.
- [SDR IPXA2026021765193](https://openairdocs.org/sdr/IPXA2026021765193.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131FE EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 131FE IS COMPLETED. PANEL FABRICATION OF PANEL 131FE IS COMPLETE IAW SREO-16407-REQ002 ((APPX C) FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO))
- [SDR IPXA2026021765271](https://openairdocs.org/sdr/IPXA2026021765271.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 132AH EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 132AH IS COMPLETED.
- [SDR IPXA2026021765279](https://openairdocs.org/sdr/IPXA2026021765279.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 132DE EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 132DE IS COMPLETED.
- [SDR IPXA2026021765236](https://openairdocs.org/sdr/IPXA2026021765236.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131BH EDGES DMAGED. VERIFIED FABRICATION OF PANEL 131BH IS COMPLETED.
- [SDR IPXA2026021765282](https://openairdocs.org/sdr/IPXA2026021765282.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131MG EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 131MG IS COMPLETED.
- [SDR IPXA2026021765313](https://openairdocs.org/sdr/IPXA2026021765313.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131SG EDGES DMAGED. VERIFIED FABRICATION OF PANEL 131SG IS COMPLETED.
- [SDR IPXA2026021765316](https://openairdocs.org/sdr/IPXA2026021765316.md): Floor Panel · damaged · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, FWD CARGO FLOOR PANEL 131RG EDGES DMAGED. VERIFIED FABRICATION OF PANEL 131RG IS COMPLETED.
- [SDR IPXA2026021067312](https://openairdocs.org/sdr/IPXA2026021067312.md): Cap · corroded · Jan 24, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > NR 3 R/A ANTENNA (4SA2) HOUSING CORRODED AROUND DOME NUT AND CUTOUT AREA. REMOVED CORROSION IAW SRM 51-74-10 FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS (.063") MATERIAL REMOVED (.020") REMAINING MATERIAL (.043")T70231. REMOVED R/A HOUSING (4SA2) IAW SRM 51-4
- [SDR IPXA2026022446419](https://openairdocs.org/sdr/IPXA2026022446419.md): Frame · cracked · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Frame
  > FR 46 LH HAS CRACK AT AREA 1. ACCOMPLISHED THE REPAIR PER EO-96738-REQ1 AND EA 300-5315-27-A4350 REV. -. MAJOR REPAIR.
- [SDR IPXA2026022053589](https://openairdocs.org/sdr/IPXA2026022053589.md): Seat Track · corroded · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MAIN DECK CARGO FLOOR PANEL 231 RJ LOWER LH FWD SKIN HAS CORROSION. INSTALLED SEAT TRACK AT FR28 AND Y1456 LH, I.A.W. A300-600 SRM-53-10-16 AND A300-600 SRM 51-40-21.
- [SDR IPXA2026022453622](https://openairdocs.org/sdr/IPXA2026022453622.md): Floor Panel · corroded · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR. MAIN DECK CARGO FLOOR PANEL 231 BH LOWER LH FWD SKIN HAS CORROSION. 89-012 REJECT- THIS IS A MAJOR REPAIR- NO CASS REPORT, SUBTASK UPS FAULT REQUIRES SIGNOFF.
- [SDR IPXA2026022652366](https://openairdocs.org/sdr/IPXA2026022652366.md): Bracket · cracked · Jan 23, 2026 · N145UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON, INBD SIDE AT RIB 8, BRACKET CRACKED. REMOVED BRACKET I.A.W. A300-600 SRM 51-40-21. INSTALLED BRACKET I.A.W. A300-600 SRM 51-40-21.
- [SDR IPXA2026021552275](https://openairdocs.org/sdr/IPXA2026021552275.md): Bracket · cracked · Jan 23, 2026 · N145UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON, AFT FAIRING LOWER SURFACE, OTBD BRACKET CRACKED. THE BRACKET WAS REMOVED IAW SRM 51-40-21 & INSTALLED IAW SRM 51-40-21.
- [SDR IPXA2026021552250](https://openairdocs.org/sdr/IPXA2026021552250.md): Bracket · cracked · Jan 23, 2026 · N145UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON, AFT FAIRING LOWER SURFACE, INBD BRACKET CRACKED. THE BRACKET WAS R & R IAW SRM 51-40-21.
- [SDR IPXA2026021750516](https://openairdocs.org/sdr/IPXA2026021750516.md): Floor Panel · damaged · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, AFT CARGO FLOOR PANEL 151UF EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 151UF IS COMPLETED.
- [SDR IPXA2026021750574](https://openairdocs.org/sdr/IPXA2026021750574.md): Floor Panel · damaged · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, AFT CARGO FLOOR PANEL 151NG EDGES DAMAGED. VERIFIED FABRICATION OF PANEL 151NG IS COMPLETED.
- [SDR IPXA2026021751305](https://openairdocs.org/sdr/IPXA2026021751305.md): Panel · damaged · Jan 23, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, AFT CARGO PANEL 152RF EDGE DAMAGED. VERIFIED FABRICATION OF PANEL 152RF IS COMPLETED.
- [SDR IPXA2026021832434](https://openairdocs.org/sdr/IPXA2026021832434.md): Seat Track · corroded · Jan 22, 2026 · N145UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MAIN DECK FLOOR STRUCTURE ON FR 80/82 AT Y1137.1 SEAT TRACK HAS CORROSION DOT 115-054. ATTACH CASS AUDIT FORM
- [SDR IPXA2026012830513](https://openairdocs.org/sdr/IPXA2026012830513.md): Floor Panel · damaged · Jan 22, 2026 · N145UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO 241DN FLOOR PANEL IS DAMAGED. PANEL 241DN FABRICATION IS COMPLETED IAW SREO-16407-REQ002.
- [SDR IPXA2026031109313](https://openairdocs.org/sdr/IPXA2026031109313.md): Door · binding · Jan 21, 2026 · N145UP · Airbus A300F4622R · Passenger/Crew Doors
  > CREW DOOR OPEN/CLOSING MECHANISM IS HARD TO OPERATE AND LOCK TO CLOSE POSITION. PERFORMED ADJUSTMENT OF GUIDE FITTINGS PERFORMED TEST OF CREW DOOR. DOOR CLOSES AND OPERATES SMOOTHLY. HANDLE FORCE IN LIMITS. IAW AMM 52-10-11/501.
- [SDR IPXA2026021713341](https://openairdocs.org/sdr/IPXA2026021713341.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION AROUND THE ADAPTER CLS FR24 Y0 RH. INSTALLED NEW ADAPTER TRACK AND 5EA CLS ADAPTER ON MAIN CABIN AT FR21 TO FR26, Y0 R/H IAW SRM 51-40-21.
- [SDR IPXA2026022114498](https://openairdocs.org/sdr/IPXA2026022114498.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > CORROSION AROUND THE ADAPTER CLS FR26 BTW Y1959 & Y2462. INSTALLED NEW TRACK ADAPTER CLS, BTW FR20 TO FR27 AND Y1959 TO Y2462 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026030114161](https://openairdocs.org/sdr/IPXA2026030114161.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > CORROSION AROUND THE ADAPTER CLS FR27 BTW Y1959 & Y2462. CLS ADAPTER TRACK WAS REPLACED ON "TASK FAULT - STR - ZONE 200 - CORROSION AROUND THE ADAPTER CLS FR26 BTW Y1959 & Y2462 DOT 06648-33 [T3F18E0084ZJX]", SDR AND CPCP CAN BE FOUND IN THE SUBTASK SECTION.
- [SDR IPXA2026021308757](https://openairdocs.org/sdr/IPXA2026021308757.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION ON ADAPTER CLS FR58 Y0 RH. ACCOMPLISHED PERMANENT REPAIR IAW EO-96334-REQ1 AND VT-MAE EA 300-5316-27-A4295 REV. - JOB COMPLETE.
- [SDR IPXA2026021312879](https://openairdocs.org/sdr/IPXA2026021312879.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION ON ADAPTER CLS FR28 Y0 LT. REMOVED ADAPTER CLS ON FR28 Y0 LH IAW A300-600 SRM 51-40-21. INSTALLED CLS ADAPTER FR28 Y0 LH IAW A300-600 SRM 51-40-21.
- [SDR IPXA2026022309077](https://openairdocs.org/sdr/IPXA2026022309077.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CORROSION ON ADAPTER CLS FR62 Y0 LH.
- [SDR IPXA2026021308559](https://openairdocs.org/sdr/IPXA2026021308559.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CORROSION ON ADAPTER CLS FR62 Y0 RH. CORROSION ON ADAPTER CLS FR62 Y0 RH.
- [SDR IPXA2026022308511](https://openairdocs.org/sdr/IPXA2026022308511.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR, CORROSION ON ADAPTER CLS FR63 Y0 RH. INSTALLED CLS ADAPTER FR63 YO RHÂ IAW A300-600 SRM 51-40-21
- [SDR IPXA2026022308620](https://openairdocs.org/sdr/IPXA2026022308620.md): Adapter · corroded · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Main, Structure
  > MAJOR REPAIR. CORROSION ON ADAPTER CLS FR57.1 Y0 RH. INSTALLED CLS ADAPTER FR57.1 Y0 RH IAW SRM 51-40-21.
- [SDR IPXA2026012914493](https://openairdocs.org/sdr/IPXA2026012914493.md): Bracket · cracked · Jan 21, 2026 · N145UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > AFT CARGO FR54 WEB AT Y953 RH CRACKED. REMOVE BRACKET FROM FR54 Y953 RH SRM 51-40-21 INSTALLED NEW BRACKET IAW 51-40-21, AFT CARGO FR54 WEB AT Y953 RH.

Next page: https://openairdocs.org/aircraft/N145UP/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 = 'N145UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N145UP/reports

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