# Service difficulty reports: N140UP

A list on [N140UP](https://openairdocs.org/aircraft/N140UP.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 · 341 reports

- [SDR IPXA2026081706346](https://openairdocs.org/sdr/IPXA2026081706346.md): Lens · missing · Aug 14, 2026 · N140UP · Airbus A300F4622R · Emergency Lighting
  > LENS MISSING FROM EMERGENCY LIGHT 150WL NEAR LAV REPLACED EMERGENCY WALL LIGHT LENS ON LIGHT 150WL REF AMM 33-51-17. OPS CHECKED GOOD.
- [SDR IPXA2026081486346](https://openairdocs.org/sdr/IPXA2026081486346.md): Lens · missing · Aug 14, 2026 · N140UP · Airbus A300F4622R · Emergency Lighting
  > LENS MISSING FROM EMERGENCY LIGHT 150WL NEAR LAV.
- [SDR IPXA2026072022407](https://openairdocs.org/sdr/IPXA2026072022407.md): Girt Bar · fod · Jul 18, 2026 · N140UP · Airbus A300F4622R · Emergency Equipment
  > DOOR WILL NOT ARM (CREW ENTRY DOOR) REMOVED DIBRIS FROM FWD GIRT BAR SLIDE. CHECKS OK.
- [SDR IPXA2026071688761](https://openairdocs.org/sdr/IPXA2026071688761.md): Slide · binding · Jul 16, 2026 · N140UP · Airbus A300F4622R · Escape Slide
  > UNABLE TO ARM DOOR SLIDE. HANDLE JAMS ABOUT 1/3 TRAVEL FROM DISARM TO ARM. CLEANED AND INSPECTED FLOOR RECEPTACLES FOR DAMAGE AND DEBRIS, CHECKED FOR PROPER GIRT BAR ENGAGEMENT IAW AMM 25-61-21/401. DOOR SLIDE ARMING ENGAGEMENT GOOD AND ARMING LEVER OPERATES S
- [SDR IPXA2025081718692](https://openairdocs.org/sdr/IPXA2025081718692.md): Attach Angle · broken · Aug 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FR 79 +Y1589.5 AFT SEAT TRACK ATTACHMENT ANGLE IS CRACKED THROUGH THE BOTTOM AFT FASTENER HOLE ON SEAT TRACK ATTACHMENT POINT. INSTALLED ANGLE WITH FASTENERS IAW SRM 51-40-21.
- [SDR IPXA2025082834493](https://openairdocs.org/sdr/IPXA2025082834493.md): Hydraulic System · leaking · Aug 12, 2025 · N140UP · Airbus A300F4622R · Hydraulic Power System
  > FWD CARGO COMPARTMENT CENTER BILLIAGE AREA INSULATION SATURATED WITH SKYDROLL. CLEANED UNDER FWD CARGO BILLIAGE AREA FROM FR27 TO FR37 WITH 1/4 GAL IAW AMM 12-21-12/201.TREATED FOR CORROSION 2 IAW SRM 51-23-20. REPLACEED 50 FT OF INSULATION IAW AMM 25-50-21
- [SDR IPXA2025090273786](https://openairdocs.org/sdr/IPXA2025090273786.md): Bracket · corroded · Aug 8, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT, CENTER CEILING SUPPORT AT FRAME 26 HAS CORROSION. INSTALLED CENTER CEILING SUPPORT AT FRAME 26 FASTENERS P/N: MS20426AD5 (30EA) BATCH: 0004233090, P/N: MS20426AD 3 (36EA) BATCH: 0004410248, P/N: ABS0330-01A (18EA) BATCH: 004416794 I.
- [SDR IPXA2025082673697](https://openairdocs.org/sdr/IPXA2025082673697.md): Support · corroded · Aug 8, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT, LEFT CEILING SUPPORT AT FRAME 26 HAS CORROSION. INSTALLED NEW PART CEILING SUPPORT FROM FORWARD CARGO COMPARTMENT, LEFT CEILING SUPPORT AT FRAME 26 IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025082126495](https://openairdocs.org/sdr/IPXA2025082126495.md): Angle · cracked · Aug 6, 2025 · N140UP · Airbus A300F4622R · Wing Main, Frame Structure
  > KRUGER FLAP I/B REINFORCING ANGLE HAS A CRACK. INSTALLED REINFORCING ANGLE AND BRACKET AT KRUGER FLAP I/B IAW A300-600, SRM 51-40-21.
- [SDR IPXA2025081847727](https://openairdocs.org/sdr/IPXA2025081847727.md): Floorbeam · cracked · Aug 1, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > FR80 -Y1221.2 AFT FLOOR STRUCTURE HAS A CRACK. INSTALLED PROFILE T AT FR80 -Y1221.2 APPLIED IAW A300-600, SRM 51-40-21.
- [SDR IPXA2025082964745](https://openairdocs.org/sdr/IPXA2025082964745.md): Floor Support · corroded · Jul 28, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR STRUCTURE BETWEEN FRAMES 14-15, Y953 HAS CORROSION AROUND 2 EA FASTENER HOLES INSTALLED NEW SUPPORT IAW A300 SRM 51-40-21.
- [SDR IPXA2025082964689](https://openairdocs.org/sdr/IPXA2025082964689.md): Floor Support · corroded · Jul 28, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO FLOOR STRUCTURE BETWEEN FRAMES 13-14, Y1552 HAS CORROSION AT 2 EA FASTENR HOLES INSTALLED NEW FLOOR SUPPORT IAW A300-600 SRM 51-40-21 USING RETAINED HARDWARE.
- [SDR IPXA2025082638344](https://openairdocs.org/sdr/IPXA2025082638344.md): Angle · gouged · Jul 26, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > BULK CARGO SCUFF PLATE INSERT FASTENER HOLE HAS VISUAL DAMAGED ON INSIDE ANGLE INSTALLED NEW ANGLE PN UP-F5347569820800 IAW SRM A300-600 51-40-21.
- [SDR IPXA2025080538803](https://openairdocs.org/sdr/IPXA2025080538803.md): Attach Bracket · cracked · Jul 26, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Attach Fittings
  > FWD E&E BAY SUSPECTED CRACK ON L/H VERTICAL INTERCOSTAL ATTACH BRACKET. (OTBD OF LADDER FROM E&E BAY TO FLIGHT DECK) REMOVED ANGLE AT E&E BAY ON L/H VERTICAL INTERCOSTAL IAW A300-600, SRM 51-40-21.FABRICATED NEW ANGLE IAW A300-600, SRM 53-12-15, PAGE 18 AND GM
- [SDR IPXA2025072908797](https://openairdocs.org/sdr/IPXA2025072908797.md): Seat Track · corroded · Jul 24, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR, MDC FLOOR STRUCTURE SEAT TRACK WITH CORROSION BTWN FR 28 THROUGH FR 31 AT Y1959. INSTALLED 3(EA) FLOORBOARD PANELS IAW AMM 53-10-23/0401 WITH RETAINED HARDWARE. INSTALLED 2(EA) FWD CARGO SIDEWALL PANEL IAW AMM 25-54-10/201.
- [SDR IPXA2025082508264](https://openairdocs.org/sdr/IPXA2025082508264.md): Support · cracked · Jul 24, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STRUCTURE, R/H SIDE REINFORCEMENT SUPPORT CRACKED AT FR 38.2 AND -Y2462. 21-50 INSTALLED NEW SUPPORT ON MDC FLOOR STRUCTURE, R/H SIDE REINFORCEMENT AT FR 38.2 AND -Y2462. I.A.W A300-600 SRM 51-40-21
- [SDR IPXA2025082108648](https://openairdocs.org/sdr/IPXA2025082108648.md): Seat Track · corroded · Jul 24, 2025 · N140UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR. MDC FLOOR STRUCTURE SEAT TRACK WITH CORROSION BTWN FR 27 THROUGH FR 29 AT Y1456. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR PER SRM REV. 42 CHAPTER 53-10-16-201 PARAGRAPH 4 FIGURE 201.
- [SDR IPXA2025080408421](https://openairdocs.org/sdr/IPXA2025080408421.md): Floor Support · cracked · Jul 24, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MDC FLOOR STRUCTURE, L/H SIDE REINFORCEMENT SUPPORT CRACKED BTWN FR 37 AND FR38 AT Y2462. 21-53.REMOVED REINFORCEMENT SUPPORT AT MCD FLOOR STRUCTURE BTWN FR 37 AND FR 38, Y 2462 LH I.A.W. A300-600 SRM 51-40-21.LOCATED AND DRILLED REINFORCEMENT SUPPORT STRUCTUR
- [SDR IPXA2025072982984](https://openairdocs.org/sdr/IPXA2025072982984.md): Floor Panel · broken · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 252LJ CRACKED. MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.
- [SDR IPXA2025072980019](https://openairdocs.org/sdr/IPXA2025072980019.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251XJ HS EXPOSED COMPOSITE IN MULTIPLE LOCATION.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072980214](https://openairdocs.org/sdr/IPXA2025072980214.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251LJ HAS COMPOSITE DAMAGE AROUND FASTENER HOLE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072980451](https://openairdocs.org/sdr/IPXA2025072980451.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251EN HAS COMPOSITE DAMAGE AT CORNERS.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072980861](https://openairdocs.org/sdr/IPXA2025072980861.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251BN HAS EXPOSED COMPOSITE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.
- [SDR IPXA2025072983810](https://openairdocs.org/sdr/IPXA2025072983810.md): Floor Panel · cracked · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT-Z200-INT MAI CARGO FLOOR PANEL 251HM EDGE CRACKED.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072981238](https://openairdocs.org/sdr/IPXA2025072981238.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT-Z200-INT MAIN CARGO FLOOR PANEL 252ZG HAS COMPOSITE DAMAGE AT EDGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072983615](https://openairdocs.org/sdr/IPXA2025072983615.md): Floor Panel · cracked · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 252FJ CRACKED.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072986078](https://openairdocs.org/sdr/IPXA2025072986078.md): Floor Panel · damaged · Jul 23, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 251LG HAS COMPOSITE DAMAGE TO EDGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072968409](https://openairdocs.org/sdr/IPXA2025072968409.md): Floor Panel · damaged · Jul 22, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > FAULT-INT-Z200- MDC FLOOR PANEL 252DN WITH COMPOSITE MATERIAL EXPOSURE AT UPPER FACE. DOT 21-15.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025072268082](https://openairdocs.org/sdr/IPXA2025072268082.md): Floor Panel · delaminated · Jul 22, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MAJOR REPAIR, MCD FLOOR PANEL231KJ IS DELAMINATING IN SEVERAL AREAS. FABRICATED FLOOR PANEL 231KJ, I.A.W. SREO-16407-REQ001 (APPX B).
- [SDR IPXA2025081434048](https://openairdocs.org/sdr/IPXA2025081434048.md): Floor Support · cracked · Jul 21, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL. VERIFIED ACCOMPLISHMENT OF PERMANENT REPAIR IAW EA 300-5318-27-A4081, REV. -.
- [SDR IPXA2025081433299](https://openairdocs.org/sdr/IPXA2025081433299.md): Seat Track · corroded · Jul 21, 2025 · N140UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 73 AND 74, -Y2127.5 HAS CORROSION. COMPLIED WITH REMOVED AND REPLACED SEAT TRACK PER DWR SPECS AND SRM REQUIREMENTS
- [SDR IPXA2025081543299](https://openairdocs.org/sdr/IPXA2025081543299.md): Seat Track · corroded · Jul 21, 2025 · N140UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 73 AND 74, -Y2127.5 HAS CORROSION REMOVE AND REPLACE SEAT TRACK P/N: A53279221211 PER DWG SPECS AND SRM REQUIREMENTS.<BR><BR>THIS IS A MINOR REPAIR PER GMM 05.04
- [SDR IPXA2025081544048](https://openairdocs.org/sdr/IPXA2025081544048.md): Floor Support · cracked · Jul 21, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN CARGO DECK FLOOR STRUCTURE BETWEEN FRAMES 74 AND 75, Y2127.5 HAS A CRACK ON Z CHANNEL VERIFIED STEP # 16 OF EA # 300-5318-27-A4081 OF PRELIMINARY 2 WERE RII
- [SDR IPXA2025081425004](https://openairdocs.org/sdr/IPXA2025081425004.md): Profile · cracked · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 HAS A CRACK THROUGH FASTENER HOLE COMPLIED WITH EO-94650-REQ1 AND VT-MAE EA 300-5318-27-A4086, REV. -.
- [SDR IPXA2025090625333](https://openairdocs.org/sdr/IPXA2025090625333.md): Support · broken · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > FR 75, BTW Y1221.2 AND Y1580.5, CLS ADAPTER WITH CORROSION. INSTALLED ADAPTER CLS AT THE MDC, FR 75 BTW Y1221.2 AND Y1580.5. I.A.W AIRBUS SRM 51-40-21-001.
- [SDR IPXA2025081524090](https://openairdocs.org/sdr/IPXA2025081524090.md): Seat Track · corroded · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR. MAIN DECK FLOOR STRUCTURE BETWEEN FRAME 79-80 AT Y0 HAS CORROSION. COMPLIED WITH REPAIR SEAT TRACK, IAW SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201 (REV. 42).
- [SDR IPXA2025082800037](https://openairdocs.org/sdr/IPXA2025082800037.md): Profile · cracked · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, MDC, BTW FR 78 AND FR 79, Y2127.5, Z PROFILE WITH CRACK COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94651-REQ1 AND VT-MAE EA 300-5318-27-A4088, REV. -.
- [SDR IPXA2025081824990](https://openairdocs.org/sdr/IPXA2025081824990.md): Floorbeam · cracked · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Floor Beam
  > MDC FLOOR, FR 80, BTW Y1221.2 AND Y1580.5, AFT FLOOR STRUCTURE WITH CRACK. INSTALLED PROFILE T AT FR80 Y1221.2 APPLIED IAW A300-600, SRM 51-40-21.
- [SDR IPXA2025081545004](https://openairdocs.org/sdr/IPXA2025081545004.md): Floor Support · cracked · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAIN DECK FLOOR STRUCTURE AT FRAME 79, -Y1580.5 HAS A CRACK THROUGH FASTENER HOLE OUT OF SEQUENCE PRELIMINARY 1 STEP#12 E.A.#. 300-5318-27-A4086 OK TO INSTALL GIVEN
- [SDR IPXA2025072925042](https://openairdocs.org/sdr/IPXA2025072925042.md): Floor Panel · damaged · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > MDC FLOOR 261DM, CRACK ON L/H AFT CORNER.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001.
- [SDR IPXA2025072925236](https://openairdocs.org/sdr/IPXA2025072925236.md): Floor Panel · damaged · Jul 20, 2025 · N140UP · Airbus A300F4622R · Fuselage Floor Panel
  > COMP MAIN CARGO FLOOR PANEL 262DM HAS COMPOSITE DAMAGE.MCD FLOOR PANEL REPAIRED IAW A300-600 SREO-42721-REQ001
- [SDR IPXA2025082294766](https://openairdocs.org/sdr/IPXA2025082294766.md): Adapter · corroded · Jul 18, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR28 Y0 LH CLS ADAPTER HAS CORROSION ON FLANGE AND INSIDE DOT 5612-34 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94687-REQ1 AND VT-MAE EA 300-5314-27-A4053 REV. -
- [SDR IPXA2025081894800](https://openairdocs.org/sdr/IPXA2025081894800.md): Adapter · corroded · Jul 18, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR27 Y0 LH CLS ADAPTER HAS CORROSION DOT 5612-36 INSTALLED NEW CLS ADAPTER IAW A300-600 SRM 51-40-21.
- [SDR IPXA2025082294779](https://openairdocs.org/sdr/IPXA2025082294779.md): Adapter · corroded · Jul 18, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, MDC FR28 Y0 RH CLS ADAPTER HAS CORROSION INSIDE DOT 5612-35 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94687-REQ1 AND VT-MAE EA 300-5314-27-A4053 REV. -.
- [SDR IPXA2025081894736](https://openairdocs.org/sdr/IPXA2025081894736.md): Adapter · corroded · Jul 18, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Structure
  > MDC FR27 Y0 LH CLS ADAPTER HAS CORROSION DOT 5612-37 INSTALLED NEW CLS ADAPTER IAW SRM 51-40-21.
- [SDR IPXA2025081595105](https://openairdocs.org/sdr/IPXA2025081595105.md): Seat Track · corroded · Jul 18, 2025 · N140UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR, MDC FR28 Y0 SEAT TRACK HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR, SEAT TRACK PER SRM 53-10-16-201 PARAGRAPH 4 FIGURE 201.
- [SDR IPXA2025081295593](https://openairdocs.org/sdr/IPXA2025081295593.md): Rib · cracked · Jul 18, 2025 · N140UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. COMPLIED WITH ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94788-REQ1 AND VT-MAE EA 300-5750-27-A4064, REV. -.
- [SDR IPXA2025081295583](https://openairdocs.org/sdr/IPXA2025081295583.md): Rib · cracked · Jul 18, 2025 · N140UP · Airbus A300F4622R · Trailing Edge Flaps
  > MAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. CIRCLED IN RED. COMPLIED WITH ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94788-REQ1 AND VT-MAE EA 300-5750-27-A4064, REV. -.
- [SDR IPXA2025080695516](https://openairdocs.org/sdr/IPXA2025080695516.md): Skin · cracked · Jul 18, 2025 · N140UP · Airbus A300F4622R · Trailing Edge Flaps
  > RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 27. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.
- [SDR IPXA2025080695469](https://openairdocs.org/sdr/IPXA2025080695469.md): Skin · cracked · Jul 18, 2025 · N140UP · Airbus A300F4622R · Trailing Edge Flaps
  > RT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 13. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.

Next page: https://openairdocs.org/aircraft/N140UP/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 = 'N140UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N140UP/reports

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