# Service difficulty reports: N124UP

A list on [N124UP](https://openairdocs.org/aircraft/N124UP.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 4 · 198 reports

- [SDR IPXA2026092403392](https://openairdocs.org/sdr/IPXA2026092403392.md): Cvr · no test · Sep 24, 2026 · N124UP · Airbus A300F4622R · Data Recorders (Flight/Maintenance)
  > DURING PREFLIGHT CVR DOES NOT TEST. CVR OPS TEST GOOD PER AMM 23-71-00
- [SDR IPXA2025112989925](https://openairdocs.org/sdr/IPXA2025112989925.md): Door · dented · Nov 29, 2025 · N124UP · Airbus A300F4622R · Landing Gear Doors
  > MAJOR REPAIR, DENT AT L/H GEAR MAIN DOOR AFT UPPER SEAM ON FUSELAGE, APPROX 2 INCHES BELOW WING TO BODY FAIRING. PERMANENT REPAIR C/W PER EO-95879-REQ3 REF BARCODE [T3F18E008WC9N] EO-95879-REQ3 (FUSELAGE SKIN AT LEFT MAIN LANDING GEAR DOOR CUTOUT DAMAGE AT AP
- [SDR IPXA2025100926914](https://openairdocs.org/sdr/IPXA2025100926914.md): Panel · cracked · Sep 16, 2025 · N124UP · Airbus A300F4622R · Fuselage Structure (General)
  > PANEL 831AZ CRACKED (2 LOCATIONS).CLEANED AND PREPARED PANEL FOR ALLOWABLE REPAIRS. IAW SRM A300-600 51-77-11 PARA 3 A.1.REPAIRED PANEL WITH 08-090, BATCH 4354723. IAW SRM A300-600 51-77-11 PARA 3.A.2-7. REVIEWED
- [SDR IPXA2025092629651](https://openairdocs.org/sdr/IPXA2025092629651.md): Plate · cracked · Sep 16, 2025 · N124UP · Airbus A300F4622R · Wing, Attach Fittings
  > PANEL 613AB ATTACHMENT PLATE CRACKED AT FWD O/B CORNER. INSTALLED DOUBLER AND SHIM IAW A300 SRM 53-15-63 AND 51-40-21.
- [SDR IPXA2025092335886](https://openairdocs.org/sdr/IPXA2025092335886.md): Skin · cracked · Sep 16, 2025 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP,TOP SKIN RIB FLANGE, ONE CRACK NOTED AT RIB 13. INSTALLATION IN STEP 17, PRIMER AND TOPCOAT APPLIED. INSTALLED DOUBLER IAW-A300-SRM-51-40-21.
- [SDR IPXA2025092230389](https://openairdocs.org/sdr/IPXA2025092230389.md): Liner · damaged · Sep 16, 2025 · N124UP · Airbus A300F4622R · Passenger/Crew Doors
  > MCD, LINING PANEL 221HW HAS CRACKS, DEFORMED AND BROKEN EDGES. LINING PANEL 221HW WAS REPAIRED IAW A300 AMM 25-00-00/801. USED PAINT P/N: 34655.7619.R.S65 BTCH: 4398324 AND PUTTY P/N: 04-001-0240 BTCH: 4421121. REVIEWED
- [SDR IPXA2025091626914](https://openairdocs.org/sdr/IPXA2025091626914.md): Panel · cracked · Sep 16, 2025 · N124UP · Airbus A300F4622R · Passenger/Crew Doors
  > PANEL 831AZ CRACKED (2 LOCATIONS)
- [SDR IPXA2025091630389](https://openairdocs.org/sdr/IPXA2025091630389.md): Liner · cracked · Sep 16, 2025 · N124UP · Airbus A300F4622R · Passenger/Crew Doors
  > MCD, LINING PANEL 221HW HAS CRACKS, DEFORMED AND BROKEN EDGES. DOT 103-672
- [SDR IPXA2025100313296](https://openairdocs.org/sdr/IPXA2025100313296.md): Channel · cracked · Sep 15, 2025 · N124UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous Structure
  > AFT. ACCESORY COMP. HORIZ. STAB. FRONT SPAR RH CHANNEL CRACKED. DOT 139-19.REMOVED UPPER AND FWD APRON DISPLACED LOWER APRON IAW A300-600 AMM 55-15-11-401.REMOVED LEADING EDGES 341AB AND FAIRING SUPPORT IAW A300-600 AMM 55-12-11/401.REMOVED CHANNEL AT HORIZONT
- [SDR IPXA2025093000592](https://openairdocs.org/sdr/IPXA2025093000592.md): Floorboard · cracked · Sep 14, 2025 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC AFT FLOORBOARD 261DM BROKEN..SREO 16407-REQ001 C/W
- [SDR IPXA2025091696218](https://openairdocs.org/sdr/IPXA2025091696218.md): Bulkhead · cracked · Sep 13, 2025 · N124UP · Airbus A300F4622R · Engine Thrust Reverser
  > NUMBER 2 ENG OUTBD INLET COWL AFT BULKHEAD HAS CRACK UNDER HARDLINE AT 3 OCLOCK POS. INSTALLED DOUBLER REPAIR AND NEW WEB IAW A300 PW SRM 54-10-00 REPAIR NO. 12 AND SRM 51-40-21. REVIEWED
- [SDR IPXA2025091906218](https://openairdocs.org/sdr/IPXA2025091906218.md): Bulkhead · cracked · Sep 13, 2025 · N124UP · Airbus A300F4622R · Engine Thrust Reverser
  > NR 2 ENG OUTBD INLET COWL AFT BULKHEAD HAS CRACK UNDER HARDLINE AT 3 OCLOCK POS.
- [SDR IPXA2025100256051](https://openairdocs.org/sdr/IPXA2025100256051.md): Bracket · corroded · Sep 11, 2025 · N124UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - STR- Z100 - FR 54 RH HORIZONTAL SIDEWALL AND CEILING SUPPORT IS CORRODED AT ATTACHMENT HOLES.REMOVED ANGLE IAW A300-600 SRM 51-40-21.FABRICATED NEW ANGLE SUPPORT IAW A300-600 FABRICATION DRAWING A 53410767.INSTALLED NEW ANGLE SUPPORT AT FR54(R/H) HORIZ
- [SDR IPXA2025093056101](https://openairdocs.org/sdr/IPXA2025093056101.md): Support · corroded · Sep 11, 2025 · N124UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - STR - Z100 - AFT CARGO FR 58 LH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES.REMOVED CROSS PROFILE IAW A300-600 SRM 51-40-21.RECIVED NEW PART (CROSS PROFILE) FOR AFT CARGO FR 58 R/H HORIZONTAL CEILING SUPPORT WITH TRAVELER# T25/1833679, P.O
- [SDR IPXA2025093055741](https://openairdocs.org/sdr/IPXA2025093055741.md): Support · corroded · Sep 11, 2025 · N124UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - STR - Z100 - AFT CARGO FR 58 CNT HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES.REMOVED CROSS PROFILE IAW A300-600 SRM 51-40-21.RECIVED NEW PART (CROSS PROFILE) FOR AFT CARGO FR 58 (CNT) HORIZONTAL CEILING SUPPORT WITH TRAVELER# T25/1833678,
- [SDR IPXA2025093056112](https://openairdocs.org/sdr/IPXA2025093056112.md): Support · corroded · Sep 11, 2025 · N124UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FAULT - STR - Z100 - AFT CARGO FR 58 RH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES.REMOVED CROSS PROFILE IAW A300-600 SRM 51-40-21.RECIVED NEW PART (CROSS PROFILE) FOR AFT CARGO FR 58 R/H HORIZONTAL CEILING SUPPORT WITH TRAVELER# T25/1833677, P.O
- [SDR IPXA2025091256051](https://openairdocs.org/sdr/IPXA2025091256051.md): Support · corroded · Sep 11, 2025 · N124UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 54 RH HORIZONTAL SIDEWALL AND CEILING SUPPORT IS CORRODED AT ATTACHMENT HOLES
- [SDR IPXA2025060189672](https://openairdocs.org/sdr/IPXA2025060189672.md): Hydraulic Line · kinked · Jun 1, 2025 · N124UP · Airbus A300F4622R · Hydraulic System, Main
  > WHILE PARKED WITH PARKING BREAK SET LOST YELLOW HYDRAULIC SYSTEM AIRCRAFT STARTED TO ROLL AIRCRAFT CONTINUE TO MOVE IN ALL BREAK SETTINGS REMOVED AND REPLACED HYD LINE REF AIPC 32-14-58-02B ITEM 210 AND AMM 32-42-27.RAN MOTOR TO VERIFY NO AIR IN SYSTEM LEAK CH
- [SDR IPXA2024121988012](https://openairdocs.org/sdr/IPXA2024121988012.md): Landing Gear · malfunctioned · Dec 19, 2024 · N124UP · Airbus A300F4622R · Landing Gear Retraction/Extension System
  > LANDING GEAR TOOK 3 ATTEMPTS TO COME DOWN WITH GEAR SELECTOR. REPLACED L/G CONTROL LEVER REF AMM 32-31-11/401 AND L/G SELECTOR VALVE 3GA REF AMM 32-31-12/401. OPS CHECKS AND LEAK CHECKS GOOD. GEAR SWING ON BAR CODE T3F18E005ST7M.
- [SDR IPXA2024110856860](https://openairdocs.org/sdr/IPXA2024110856860.md): Warning Message · illuminated · Nov 8, 2024 · N124UP · Airbus A300F4622R · Door Warning System
  > CREW ENTRY DOOR SHOWS CLOSED ON ECAM AFTER OPENING DOOR R&R'D SWITCH 7WS W/REF TO MM 52-71-00 PB0401. ADJ/TEST W/REF TO MM 52-71-000 OPS NORMAL THIS CLEARS DEFERRAL
- [SDR IPXA2024010926055](https://openairdocs.org/sdr/IPXA2024010926055.md): Frame · cracked · Jan 8, 2024 · N124UP · Airbus A300F4622R · Fuselage Main, Frame
  > DURING SURFACE HFEC INSP PER EO-18290-JIC005, FOUND 1EA CRACK ON THE L/H SIDE FRAME 47 FWD FITTING UPPER RADIUS. AREA MARKED IN RED. PERFORMED UT INSP. IAW NTM 57-10-43 PART 4 FOUND 01 E/A CRACK WITH 19 MM DEPTH AT THIS TIME INSP. ONLY T90093. AUDIT COMPLETE.
- [SDR IPXA2023071193643](https://openairdocs.org/sdr/IPXA2023071193643.md): Cylinder · inoperative · Jul 10, 2023 · N124UP · Airbus A300F4622R · Passenger/Crew Doors
  > INSPECTION TYPE:NAPER WAN 3806436 - R&R L1 DAMPER & EMERGENCY OPERATION CYLINDERBEGAN REMOVAL OF DOOR DAMPER * OPERATIONAL CYLINDER UP TO & INCLUDING STEP B. (1)(G) AMM 52-10-14-0401 [LC 4553072] R&R DOOR DAMPER PER MM 52-10-14-0401 OPS CK NORMAL PER MM 52-10-
- [SDR IPXA2023051993274](https://openairdocs.org/sdr/IPXA2023051993274.md): Rudder · delaminated · May 9, 2023 · N124UP · Airbus A300F4622R · Rudder Structure
  > INSPECTION TYPE:1C2C*** MAJOR REPAIR *** R/H SIDE OF RUDDER AFT FASTENER ROW. 6TH SCREW UP FROM THE BOTTOM.REPAIRED PANEL IAW A300 SRM 55-41-12 PARA 23.
- [SDR IPXA2023050893149](https://openairdocs.org/sdr/IPXA2023050893149.md): Adapter · broken · May 8, 2023 · N124UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1C*MAJOR REPAIR* FWD CABIN SEAT TRACK ADAPTER BROKEN AT FR20 BETWEEN -Y1456 AND -Y1959 (RH SIDE).INSTALLED NEW CLS ADAPTER IAW-SRM 51-40-21.
- [SDR IPXA2023051693249](https://openairdocs.org/sdr/IPXA2023051693249.md): Floor Panel · damaged · May 4, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:C*MAJOR REPAIR* PNL 242RH IS DAMAGEDFABBED, IAW SREO A300-5320-40552-B
- [SDR IPXA2023051693248](https://openairdocs.org/sdr/IPXA2023051693248.md): Floor Panel · damaged · May 4, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* MAIN CARGO COMPARTMENT, FLOOR PANEL 232UG IS CRACKEDFABBED PANEL IAW SREO A300-5320-40552-B
- [SDR IPXA2023051693247](https://openairdocs.org/sdr/IPXA2023051693247.md): Floor Panel · damaged · May 4, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:C*MAJOR REPAIR* PNL 251EN CRACKEDFABBED IAW SREO A300-5320-40552-B
- [SDR IPXA2023051693246](https://openairdocs.org/sdr/IPXA2023051693246.md): Floor Panel · damaged · May 4, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:C*MAJOR REPAIR* PNL 251G DAMAGEDFABBED IAW SREO A300-5320-40552-B
- [SDR IPXA2023051693245](https://openairdocs.org/sdr/IPXA2023051693245.md): Floor Panel · damaged · May 4, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:C*MAJOR REPAIR* PNL 252ZG IS CRACKEDFABBED IAW SREO A300-5320-40552-B
- [SDR IPXA2023050493120](https://openairdocs.org/sdr/IPXA2023050493120.md): Fitting · cracked · May 4, 2023 · N124UP · Airbus A300F4622R · Wing, Attach Fittings
  > INSPECTION TYPE:1C*MAJOR REPAIR* AFT CARGO FITTING AT FR54, -Y1959 CRACKED.REMOVED AND REPLACED FITTING IAW SRM 51-40-21
- [SDR IPXA2023050493119](https://openairdocs.org/sdr/IPXA2023050493119.md): Plate · cracked · May 4, 2023 · N124UP · Airbus A300F4622R · Wing Main, Frame Structure
  > INSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SIDE PLATE R/H SIDE BETWEEN FR76 AND FR77 CRACKED.REMOVED AND REPLACED PLATE IAW-SRM 51-40-21
- [SDR IPXA2023050993171](https://openairdocs.org/sdr/IPXA2023050993171.md): Floor Panel · damaged · Apr 30, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 131AH DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023042793008](https://openairdocs.org/sdr/IPXA2023042793008.md): Crossbeam · bent · Apr 27, 2023 · N124UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CMAIN DECK CARGO FLOOR CROSS BEAM AT FR 49 R/H BENT.REMOVED AND REPLACED CROSS BEAM IAW SRM 51-40-21.
- [SDR IPXA2023042793006](https://openairdocs.org/sdr/IPXA2023042793006.md): Crossbeam · bent · Apr 27, 2023 · N124UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CMAIN DECK CARGO FLOOR CROSS BEAM AT FR 38 R/H BENT.REMOVED AND REPLACED CROSS BEAM IAW SRM 51-40-21.
- [SDR IPXA2023042793009](https://openairdocs.org/sdr/IPXA2023042793009.md): Crossbeam · bent · Apr 27, 2023 · N124UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CMAIN DECK CARGO FLOOR CROSS BEAM AT FR 50 R/H BENT.REMOVED AND REPLACED CROSS BEAM IAW SRM 51-40-21.
- [SDR IPXA2023050993181](https://openairdocs.org/sdr/IPXA2023050993181.md): Floor Panel · damaged · Apr 24, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 152MG DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023050393106](https://openairdocs.org/sdr/IPXA2023050393106.md): Support Fitting · cracked · Apr 24, 2023 · N124UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:1CSUPPORT FITTING AT FR 54 - Y1959 CRACKEDREMOVED AND REPLACED IAW SRM 51-40-21
- [SDR IPXA2023051593226](https://openairdocs.org/sdr/IPXA2023051593226.md): Rib · cracked · Apr 22, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5YR*MAJOR REPAIR* RIB 21 ON RH WING CENTER FLAP HAS 1EA CRACKREPAIRED PER SRM 57-50-00 FIG 201 AND 205
- [SDR IPXA2023051593223](https://openairdocs.org/sdr/IPXA2023051593223.md): Rib · cracked · Apr 22, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5YR*MAJOR REPAIR* RIB 19 ON RH WING CENTER FLAP HAS 1EA CRACKREPAIRED PER SRM 57-50-00 FIG 201 AND 205
- [SDR IPXA2023051593225](https://openairdocs.org/sdr/IPXA2023051593225.md): Rib · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5YR*MAJOR REPAIR* RIB 26 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 26 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A-A3213-A
- [SDR IPXA2023051593224](https://openairdocs.org/sdr/IPXA2023051593224.md): Rib · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5YR*MAJOR REPAIR* RIB 27 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 27 PER UPS EO A300-5750-27-A3213-A
- [SDR IPXA2023051393214](https://openairdocs.org/sdr/IPXA2023051393214.md): Flap · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Wing, Control Surfaces
  > INSPECTION TYPE:5Y*MAJOR REPAIR* RIB 27 ON CENTER FLAP FOUND CRACKEDREPAIRED RIB 27 PER UPS EO A300-5750-8612-A AND VTMAE FINAL EA 300-5750-27-A3212-A
- [SDR IPXA2023051393218](https://openairdocs.org/sdr/IPXA2023051393218.md): Flap · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5Y*MAJOR REPAIR* RIB 17 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 17 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A3213-A
- [SDR IPXA2023051393217](https://openairdocs.org/sdr/IPXA2023051393217.md): Flap · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5Y*MAJOR REPAIR* RIB 18 ON RH CENTER FLAP FOUND CRACKEDREPAIRED RIB 18 PER UPS EO A300-5750-8611-A AND VTMAE FINAL EA 300-5750-27-A3213-A
- [SDR IPXA2023051393215](https://openairdocs.org/sdr/IPXA2023051393215.md): Flap · cracked · Apr 21, 2023 · N124UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:5Y*MAJOR REPAIR* RIB 26 ON CENTER FLAP FOUND CRACKEDREPAIRED RIB 26 PER UPS EO A300-5750-8612-A AND VTMAE FINAL EA 300-5750-27-A3212-A
- [SDR IPXA2023050993178](https://openairdocs.org/sdr/IPXA2023050993178.md): Floor Panel · damaged · Apr 21, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 151LG DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023050993177](https://openairdocs.org/sdr/IPXA2023050993177.md): Floor Panel · damaged · Apr 21, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 152KG DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023050993176](https://openairdocs.org/sdr/IPXA2023050993176.md): Floor Panel · damaged · Apr 21, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 1515F DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023050993175](https://openairdocs.org/sdr/IPXA2023050993175.md): Floor Panel · damaged · Apr 21, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 1515F DAMAGEDFABBED PER SREO A300-5320-16407-E
- [SDR IPXA2023050993174](https://openairdocs.org/sdr/IPXA2023050993174.md): Floor Panel · damaged · Apr 21, 2023 · N124UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1C2C*MAJOR REPAIR* PNL 151RF DAMAGEDFABBED PER SREO A300-5320-16407-E

Next page: https://openairdocs.org/aircraft/N124UP/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 = 'N124UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N124UP/reports

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