# Service difficulty reports: N126UP

A list on [N126UP](https://openairdocs.org/aircraft/N126UP.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 5 · 233 reports

- [SDR IPXA2026081116362](https://openairdocs.org/sdr/IPXA2026081116362.md): Bleed Air Sys · odor · Aug 11, 2026 · N126UP · Airbus A300F4622R · APU Bleed Air System
  > UPON TURNING ON APU BLEED AIR, NOTICED A STRONG FUEL ODOR COMING OUT OF THE VENTILATION AREAS IN COCKPIT AND SUPERNUMARY COMPARTMENT. T/S AND FOUND TORQUE MOTOR ON APU FUEL CONTROL LEAKING FUEL INTO THE APU INTAKE. R/R TORQUE MOTOR SEAL PER CMM 49-31-61. OPS A
- [SDR IPXA2026071448898](https://openairdocs.org/sdr/IPXA2026071448898.md): Fitting · cracked · Jul 1, 2026 · N126UP · Airbus A300F4622R · Cargo/Baggage Doors
  > MCD FWD ACUATOR FITTING REQUIRES REPLACEMENT. MCD AFT ACTUATOR FITTING (P/N A5237112300200& QTY 1 SPACER PN A523711540000, QTY 1 ANGLE FITTING ASSY) IS INSTALLED.
- [SDR IPXA2026071248945](https://openairdocs.org/sdr/IPXA2026071248945.md): Fitting · cracked · Jul 1, 2026 · N126UP · Airbus A300F4622R · Cargo/Baggage Doors
  > MCD AFT ACUATOR FITTING REQUIRES REPLACEMENT VERIFIED APPLIED TOP COAT AND RESTORED CIC IAW SRM 51-22-00-001 AND IAW SRM 51-21-00-001.
- [SDR IPXA2025111372654](https://openairdocs.org/sdr/IPXA2025111372654.md): Skin · gouged · Nov 8, 2025 · N126UP · Airbus A300F4622R · Horizontal Stabilizer Structure
  > WHILE GIVING OK TO INSTALL RT VERTICAL ROOT PANEL 323AR, FOUND GOUGE ON FUSELAGE UNDER PANEL, ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95674-REQ1 AND VT-MAE EA 300-5319-27-A4225 REV IR.
- [SDR IPXA2025111135069](https://openairdocs.org/sdr/IPXA2025111135069.md): Skin · corroded · Oct 30, 2025 · N126UP · Airbus A300F4622R · Wing, Plate/Skin
  > LEFT WING HAS DISBOND PLY ON LOWER SURFACE OF THE OUTBOARD TRAILING EDGE COVERED BY SPEED TAPE. INSTALLED NEW EXTRUSION (SECTION PANEL TRAILING EDGE) AT LT WING O/B IAW SRM 51-40-21. REMOVED CORROSION AT ALUMINUM EXTRUSION IAW SRM 51-74-10. FOUND TO BE OUT LI
- [SDR IPXA2025111101314](https://openairdocs.org/sdr/IPXA2025111101314.md): Skin · corroded · Oct 28, 2025 · N126UP · Airbus A300F4622R · Wing, Plate/Skin
  > RIGHT WING OTBD TRAILING EDGE HAS 3 PIECES OF SPEED TAPE. REMOVED CORROSION AT ALUMINUM EXTRUSION IAW SRM 51-74-10. FOUND TO BE OUT LIMITS IAW SRM 57-51-12 PAR.(3)(H). INSTALLED REPAIR PLATES (2EA) AND INSERTS (2EA) AT RT WING OTBD TRAILING EDGE IAW SRM 57-51-
- [SDR IPXA2025111186416](https://openairdocs.org/sdr/IPXA2025111186416.md): Panel · cracked · Oct 27, 2025 · N126UP · Airbus A300F4622R · Wing, Attach Fittings
  > RIGHT WING, L/E, KRUGER FLAP BOX AREA, BY RIB2, PANEL STR HAS A CRACK ON A CORNER. REMOVED OTBD ZEE ANGLE P/N: A5724228220547, INBD ZEE ANGLE P/N: A57242282203, AND THREE STIFFENERS (UPPER, MIDDLE, LOWER) FROM PANEL P/N: A57242282001 TO FOM IAW SRM 51-40-21.
- [SDR IPXA2025110483757](https://openairdocs.org/sdr/IPXA2025110483757.md): Floor Panel · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 261DM BROKEN AT UPPER SURFACE. DOT 21-02. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2025110484021](https://openairdocs.org/sdr/IPXA2025110484021.md): Floor Panel · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 262DM BROKEN ON FWD RH CORNER DOT 1/034. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) A300 MAIN CARGO DECK COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2025110484163](https://openairdocs.org/sdr/IPXA2025110484163.md): Floor Panel · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR PANEL 261JM BROKEN. DOT 21-08. FLOOR PANEL FABICATION IS COMPLETED IAW SREO-16407-REQ001 ((APPX B) MAIN DECK CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).
- [SDR IPXA2025103085340](https://openairdocs.org/sdr/IPXA2025103085340.md): Bracket · cracked · Oct 27, 2025 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > RIGHT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW SRM 51-40-21.
- [SDR IPXA2025110386316](https://openairdocs.org/sdr/IPXA2025110386316.md): Skin · cracked · Oct 27, 2025 · N126UP · Airbus A300F4622R · Wing, Plate/Skin
  > RH WING, L/E, CUTOUT OF 613AB ACCESS, HAS A CRACK ON FWD O/B SCREW HOLE. INSTALLED REPAIR DOUBLERS 1 AND 3 ON RH WING LEADING EDGE CUTOUT FOR ACCESS PANEL 613AB IAW SRM 53-15-63 PARAGRAPH 2 (M,N).
- [SDR IPXA2025103085335](https://openairdocs.org/sdr/IPXA2025103085335.md): Bracket · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > LEFT WING CENTER FLAP OUTBD SIDE BRACKET IS BROKEN OFF. INSTALLED BRACKET IAW A300-600 SRM 51-40-21 P/N CR3223-4-2 BATCH# 0004423484 3EA.
- [SDR IPXA2025110184125](https://openairdocs.org/sdr/IPXA2025110184125.md): Angle · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FLOOR STRUSCTURE "Z" ANGLE IS CRACKED AT 2EA LOCATIONS BTWN FR 74 AND FR 75 AT L/H SIDE. Y2127.5. DOT 21-07. INSTALLED "Z" ANGLE AT MAIN CARGO FLOOR STRUCTURE Y2127.5 BETWEEN FR 74 AND FR 75 AT L/H SIDE. Y2127.5 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025110184470](https://openairdocs.org/sdr/IPXA2025110184470.md): Angle · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR STRUCTURE "Z" ANGLE IS CRACKED AT -Y2127.5 BETWEEN FR73 AND FR74 DOT 1/038. INSTALLED "Z" ANGLE AT MAIN CARGO FLOOR STRUCTURE -Y2127.5 BETWEEN FR73 AND FR74 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025110183754](https://openairdocs.org/sdr/IPXA2025110183754.md): Angle · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MCD FLOOR STRUSCTURE WITH Z ANGLE CRACKED AT FR 80/82 L/H SIDE. Y1580.5. DOT 21-01. INSTALLED "Z" ANGLE AT MCD FLOOR STRUCTURE FR80 AND FR82 L/H SIDE Y1580.5 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025110183463](https://openairdocs.org/sdr/IPXA2025110183463.md): Angle · broken · Oct 27, 2025 · N126UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > CRACK ON Z ANGLE FR 80/82 Y2127.5. INSTALLED "Z" ANGLE AT Z ANGLE FR 80/82 Y2127.5 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025110562627](https://openairdocs.org/sdr/IPXA2025110562627.md): Fairing · cracked · Oct 26, 2025 · N126UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous Structure
  > AFT FAIRING 485AL HAS A CRACK AT AFT I/B SIDE. PERFORMED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921 RED. VERIFIED PERFORED WELDING AT CRACKED AREA AT AFT FAIRING 485AL AT AFT I/B SIDE. IAW SRM 54-55-51 AMS 4921.
- [SDR IPXA2025103141487](https://openairdocs.org/sdr/IPXA2025103141487.md): Rib · cracked · Oct 24, 2025 · N126UP · Airbus A300F4622R · Wing, Rib/Bulkhead
  > FAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. CIRCLED IN RED. ++PERFORM RIB 11 REPAIR IN ACCORDANCE WITH FIGURE 5, TAKING EXISTING FASTENER PATTERN INTO ACCOUNT INSTALLING SOLID RIVETS PER DRAWING REQUIREMENTS AT THE
- [SDR IPXA2025110339883](https://openairdocs.org/sdr/IPXA2025110339883.md): Intercostal · broken · Oct 24, 2025 · N126UP · Airbus A300F4622R · Wing Miscellaneous Structure
  > RIGHT WING TRAILIN EDGE STA 1196 RIB17 INTERCOSTAL IS BROKEN. INSTALLED INTERCOSTALL AND FITTING AT R/H WING T/E STA 1196 RIB 17. IAW SRM 51-40-21-001.
- [SDR IPXA2025050599862](https://openairdocs.org/sdr/IPXA2025050599862.md): Bulb · inoperative · May 4, 2025 · N126UP · Airbus A300F4622R · Emergency Lighting
  > L1 DOOR EMERGENCY SIGN PATHWAY LIGHT INOP REMOVED AND REPLACED BULB. REF AMM 33-51-13. OPS CHECK OK
- [SDR IPXA2024122602798](https://openairdocs.org/sdr/IPXA2024122602798.md): Transfer Sys · faulted · Dec 26, 2024 · N126UP · Airbus A300F4622R · Aircraft Fuel Distribution System
  > ECAM- TRIM TANK AFT XFR NOT AVAILABLE. PERFORMED FUEL SYSTEM TRANSFER CONTROL SYSTEM TEST REF AMM 28-26-00 NO DEFECTS NOTED AT THIS TIME. REMOVED AND REPLACED TRIM TANK COMPENSATOR I.A.W. UPS A300 AMM 28-42-51-401. COMPLETED INSTALLATION OF TAIL TANK COMPENSA
- [SDR IPXA2023070793606](https://openairdocs.org/sdr/IPXA2023070793606.md): Shear Tie · cracked · Jul 6, 2023 · N126UP · Airbus A300F4622R · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:1CFRAME 45R FRAME FEET CRACKED IN AREA 1.REMOVED AND REPLACED IAW EO A300-5310-46789-G APPENDIX G.
- [SDR IPXA2023070393591](https://openairdocs.org/sdr/IPXA2023070393591.md): Flap · gouged · Jul 3, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH IB FLAP OB TOP BOUBLER HAS GOUGESREPLACED DOUBLER WITH A NEW DOUBLE IAW UPS EO A300-5750-87370-A
- [SDR IPXA2023070393586](https://openairdocs.org/sdr/IPXA2023070393586.md): Flap · cracked · Jul 2, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON FLANGE 21REPAIRED FLANG IAW SRM 57-50-00-201
- [SDR IPXA2023070393585](https://openairdocs.org/sdr/IPXA2023070393585.md): Seat Track · corroded · Jul 2, 2023 · N126UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:CSEAT TRACK AT Y1959 BETWEEN FR 30 AND 32 IS CORRODEDREPAIRED SEAT TRACK IAW SRM53-10-16-201
- [SDR IPXA2023070393584](https://openairdocs.org/sdr/IPXA2023070393584.md): Flap · cracked · Jul 2, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON FLANGE 13REPAIRED FLANG IAW SRM 57-50-00-201
- [SDR IPXA2023070193573](https://openairdocs.org/sdr/IPXA2023070193573.md): Flap · cracked · Jul 1, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRAK ON RIB 25REPAIER IAW UPS EO A300-5750-87448 REV A
- [SDR IPXA2023070193572](https://openairdocs.org/sdr/IPXA2023070193572.md): Flap · cracked · Jul 1, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON RIB 17REPAIER IAW UPS EO A300-5750-87448 REV A
- [SDR IPXA2023070193571](https://openairdocs.org/sdr/IPXA2023070193571.md): Flap · cracked · Jul 1, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:CRH WING CENTER FLAP HAS 1EA CRACK ON RIB 27REPAIER IAW UPS EO A300-5750-87448 REV A
- [SDR IPXA2023070193570](https://openairdocs.org/sdr/IPXA2023070193570.md): Flap · cracked · Jul 1, 2023 · N126UP · Airbus A300F4622R · Trailing Edge Flaps
  > INSPECTION TYPE:C, RT WING CENTER FLAP HAS 1EA CRACK ON RIB 26REPAIER IAW UPS EO A300-5750-87448 REV A
- [SDR IPXA2023062393502](https://openairdocs.org/sdr/IPXA2023062393502.md): Doubler · cracked · Jun 19, 2023 · N126UP · Airbus A300F4622R · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:1CPYLON PRECOOLER PANEL 413BL HAS A CRACK ON THE LOWER SIDE.FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-52-51 AND 51-40-21.
- [SDR IPXA2023070193568](https://openairdocs.org/sdr/IPXA2023070193568.md): Floor Panel · damaged · Jun 14, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 221FG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193564](https://openairdocs.org/sdr/IPXA2023070193564.md): Floor Panel · damaged · Jun 14, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 232SG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193563](https://openairdocs.org/sdr/IPXA2023070193563.md): Floor Panel · damaged · Jun 14, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 231WG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193562](https://openairdocs.org/sdr/IPXA2023070193562.md): Floor Panel · damaged · Jun 14, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 231RG DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.
- [SDR IPXA2023070193569](https://openairdocs.org/sdr/IPXA2023070193569.md): Floor Panel · damaged · Jun 10, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 231BH BROKENFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193575](https://openairdocs.org/sdr/IPXA2023070193575.md): Floor Panel · damaged · Jun 9, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:IC2CPANEL DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193566](https://openairdocs.org/sdr/IPXA2023070193566.md): Floor Panel · damaged · Jun 9, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 231NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B.
- [SDR IPXA2023063093558](https://openairdocs.org/sdr/IPXA2023063093558.md): Seat Track · corroded · Jun 9, 2023 · N126UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:IC*MAJOR REPAIR* AFT CABIN SEAT TRACK AT -Y450 AT FRAME 78 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293485 AND SRM 53-10-16-201.
- [SDR IPXA2023063093556](https://openairdocs.org/sdr/IPXA2023063093556.md): Seat Track · corroded · Jun 9, 2023 · N126UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SEAT TRACK AT Y1580.5 AT FRAME 79 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293484 AND SRM 53-10-16-201.
- [SDR IPXA2023062393501](https://openairdocs.org/sdr/IPXA2023062393501.md): Adapter · broken · Jun 8, 2023 · N126UP · Airbus A300F4622R · Fuselage Main, Structure
  > INSPECTION TYPE:1CMAIN DECK CARGO FLOOR SEAT ADAPTER AT FR 34 L/H BETWEEN Y1959 AND Y2462 BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR IPXA2023060793390](https://openairdocs.org/sdr/IPXA2023060793390.md): Bracket · cracked · Jun 7, 2023 · N126UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: 1C AFT CARGO FR 54 BRACKET AT Y953 LH CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR IPXA2023070193567](https://openairdocs.org/sdr/IPXA2023070193567.md): Floor Panel · damaged · Jun 6, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 232NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023070193565](https://openairdocs.org/sdr/IPXA2023070193565.md): Floor Panel · damaged · Jun 6, 2023 · N126UP · Airbus A300F4622R · Fuselage Floor Panel
  > INSPECTION TYPE:1CPANEL 232XG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-B
- [SDR IPXA2023063093557](https://openairdocs.org/sdr/IPXA2023063093557.md): Seat Track · corroded · Jun 6, 2023 · N126UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:1C*MAJOR REPAIR* AFT CABIN SEAT TRACK AT Y1137.1 AT FRAME 80 IS CORRODED.REMOVED, FABRICATED, AND INSTALLED IAW RCD 293318 AND SRM 53-10-16-201.
- [SDR IPXA2023062493508](https://openairdocs.org/sdr/IPXA2023062493508.md): Bracket · broken · Jun 4, 2023 · N126UP · Airbus A300F4622R · Horizontal Stabilizer Structure
  > INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR IPXA2023062493507](https://openairdocs.org/sdr/IPXA2023062493507.md): Bracket · broken · Jun 4, 2023 · N126UP · Airbus A300F4622R · Horizontal Stabilizer Structure
  > INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKEN.REMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR IPXA2023062493506](https://openairdocs.org/sdr/IPXA2023062493506.md): Bracket · broken · Jun 4, 2023 · N126UP · Airbus A300F4622R · Horizontal Stabilizer Structure
  > INSPECTION TYPE:1CTHREE EACH SUPPORTS FOR APRON 333AT ARE BROKENREMOVED AND REPLACED IAW SRM 51-40-21.
- [SDR IPXA2023062493505](https://openairdocs.org/sdr/IPXA2023062493505.md): Spar · cracked · Jun 3, 2023 · N126UP · Airbus A300F4622R · Nacelle/Pylon, Frame/Spar/Rib
  > INSPECTION TYPE:1CENGINE 1 I/B SIDE INLET COWL REAR SPAR HAS 1 EA CRACK AT 3 O'CLOCK POSITION.FABRICATED WEB SPAR AND REPLACED IAW SRM 51-40-21 AND P&W SRM 54-10-00.

Next page: https://openairdocs.org/aircraft/N126UP/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 = 'N126UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N126UP/reports

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