# Service difficulty reports: N250UP

A list on [N250UP](https://openairdocs.org/aircraft/N250UP.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 · 294 reports

- [SDR IPXA2025042906305](https://openairdocs.org/sdr/IPXA2025042906305.md): Battery · no test · Apr 29, 2025 · N250UP · Doug MD11F · Emergency Lighting
  > DURING THE EMERGENCY LT TEST, GOT L1 Â€ŒEMER LT BAT 1 LOÂ€? REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. OPS CHECK GOOD. THIS CLEARS DEFERRAL. REVERSED DMP, PLACARD REMOVED.
- [SDR IPXA2025031438865](https://openairdocs.org/sdr/IPXA2025031438865.md): Wire Harness · damaged · Mar 14, 2025 · N250UP · Doug MD11F · Smoke Detection
  > FIRE DET 3 FAULT DISPLAYED. REF. SUBSTASK T3F18E006A0MM. R&R WIRE HARNESS. OPS CHECK GOOD. THIS CLOSES DEFERRAL. PLACARD REMOVED.
- [SDR IPXA2024080154251](https://openairdocs.org/sdr/IPXA2024080154251.md): Window Frame · corroded · Jul 17, 2024 · N250UP · Doug MD11F · Fuselage Main, Structure
  > FOUND SURFACE CORROSION ON COPILOT WINDOW LWR FRAME AROUND FASTENER HOLES. ACCOMPLISHED REPAIR PER EO 90992-REQ1 AND VT-SAA EA 011-5310-01-B0240, REV. I/R
- [SDR IPXA2024073101707](https://openairdocs.org/sdr/IPXA2024073101707.md): Doubler · cracked · Jul 13, 2024 · N250UP · Doug MD11F · Wing, Plate/Skin
  > R/H WING LEADING EDGE BEADED DOUBLER IS CRACKED INBOARD OF #12 SLAT TRACK. ATA 57-20 RD-05 VERIFIED REPAIR IS ACCOMPLISHED PER EO-90956-REQ1 AND MD-11 SRM 57-40-02-2R-15, REPAIR 15.
- [SDR IPXA2024073101942](https://openairdocs.org/sdr/IPXA2024073101942.md): Doubler · cracked · Jul 13, 2024 · N250UP · Doug MD11F · Wing, Plate/Skin
  > R/H WING LEADING EDGE FEEDER DOUBLER IS CRACKED INBOARD OF SLAT #11 SLAT TRACK AT 2 RIVETS. ATA 57-40 RD16 ACCOMPLISHED REPAIR PER EO-90957-REQ1 AND MD11 SRM 57-40-02-2R-15 REPAIR 15 FIG 205.
- [SDR IPXA2024072797930](https://openairdocs.org/sdr/IPXA2024072797930.md): Intercostal · cracked · Jul 13, 2024 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > RH AIR-CON BAY STA 535-555 LONGERON 31R INTERCOASTAL WEB HAS CRACKED AS MARKED. 74-056 ATA CODE 53 INSTALLED NEW INTERCOSTAL AT R/H AIR-CON BAY, STA 535-555 LONGERON 31R, IAW MD-11 SRM 51-35-01-0G-0.
- [SDR IPXA2023091994193](https://openairdocs.org/sdr/IPXA2023091994193.md): Light · no test · Sep 18, 2023 · N250UP · Doug MD11F · Emergency Lighting
  > EMERGENCY LT TEST FAIL, MESSAGE-EMER LT BAT 1 LO. DEFERRED EMERGENCY LTS-MEL 33-50-4, C/N M812482. DMP C/W.R&R EMERG LIGHT POWER SUPPLY IAW AMM 33-51-01. OPS CK GOOD DMP REVERSED AND PLACARD REMOVED. THIS CLEARS THIS DEFERRED.
- [SDR IPXA2022081385198](https://openairdocs.org/sdr/IPXA2022081385198.md): Fire Detector · faulty · Aug 13, 2022 · N250UP · Doug MD11F · Fire Detection
  > INSPECTION TYPE:N/ALVL 1 FIRE DET 1 FAULT. DEFERRED FIRE DET 1 LOOP B PER MEL 26-11-1, DMP C/W. PLACARD INSTALLED. DEFERRAL # M788738 APPLIED.CFDS SHOWS LOWER FIRE DETECTION ASSY B LOOP BROKEN. REPLACED #1 LOWER B LOOP IAW AMM 26-11-03, OPS CK GOOD, THIS CLEAR
- [SDR IPXA2022072584513](https://openairdocs.org/sdr/IPXA2022072584513.md): Beam · cracked · Jul 13, 2022 · N250UP · Doug MD11F · Trailing Edge Flaps
  > INSPECTION TYPE:3CL/H O/B FLAP I/B HIMGE AFT FAIRING SUPPORT BEAM IS CRACKED.REMOVED, FABRICATED AND REPLACED BEAM IAW DWG. ARC2149 AND SRM 51-33-01 AND 51-31-01. (MINOR)
- [SDR IPXA2022072984681](https://openairdocs.org/sdr/IPXA2022072984681.md): Seat Track · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN STA. 499-515 AT X= -62.190.REPAIRED CORRODED MAIN CABIN SEAT TRACK BETWEEN STA. 499-535 AT X= -62.190 IAW VT-SAA EA 011-5310-01-A9639 REV. I/R AND UPS EO MD11-5310-84276-A, (MAJOR) REF. FAA FORM 810
- [SDR IPXA2022072784619](https://openairdocs.org/sdr/IPXA2022072784619.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CCOURIER FLOOR PANEL WSP0788-502 HAS CORROSION BETWEEN STA Y=475.000, Y=503.175 AND X=-36.00, X=-47.50REMOVED, REPLACED FLOOR PANEL WSP0788-502 IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022072584512](https://openairdocs.org/sdr/IPXA2022072584512.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0789-501 AT POS. 2 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072384467](https://openairdocs.org/sdr/IPXA2022072384467.md): Angle · cracked · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CLOWER FUSELAGE BLADDER AREA FRAME TO LONGERON SUPPORT ANGLE CRACK AT STA.1278.REMOVED AND REPLACED CRACKED SUPPORT ANGLE IAW SRM 51-33-01 AND 51-31-01 (MINOR).
- [SDR IPXA2022072184421](https://openairdocs.org/sdr/IPXA2022072184421.md): Longeron · cracked · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CBLADDER AREA, L/H SIDE FRAME TO LONGERON END ANGLE FITTING IS CRACKED AT STA 1278REMOVED, REPLACED THE CRACKED ANGLE IAW SRM 51-33-01 (MINOR)
- [SDR IPXA2022072084379](https://openairdocs.org/sdr/IPXA2022072084379.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0785-502 AT POS. 4 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084378](https://openairdocs.org/sdr/IPXA2022072084378.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0786-501 HAS CORROSION.REMOVED AMD REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084377](https://openairdocs.org/sdr/IPXA2022072084377.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0788-501 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084375](https://openairdocs.org/sdr/IPXA2022072084375.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0785-501 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084374](https://openairdocs.org/sdr/IPXA2022072084374.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0790-501 HAS CORROSION.REMOVED AMD REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084373](https://openairdocs.org/sdr/IPXA2022072084373.md): Skin Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Main, Frame
  > INSPECTION TYPE:3CMAIN CABIN FLOOR PANEL WSP0785-501 AT POS. 6 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072084372](https://openairdocs.org/sdr/IPXA2022072084372.md): Floor Panel · corroded · Jul 12, 2022 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:3CCOURIER FLOOR PANEL WSP0785-502 HAS CORROSION.REMOVED AND REPLACED FLOOR PANEL IAW SRM 51-31-01. (MINOR)
- [SDR IPXA2022072384470](https://openairdocs.org/sdr/IPXA2022072384470.md): Cap · corroded · Jul 11, 2022 · N250UP · Doug MD11F · Horizontal Stabilizer Structure
  > INSPECTION TYPE:3CLH HORIZONTAL STAB LOWER CAP HAS CORROSION AT STA XE 67 TO XE 79 REAR SPAR.REPAIRED CORRODED LOWER CAP IAW VT-SAA EA 011-5510-01-A9641 REV I/R AND UPS EO MD11-5510-84266-A (MINOR).
- [SDR IPXA2022072384466](https://openairdocs.org/sdr/IPXA2022072384466.md): Tee Angle · cracked · Jul 8, 2022 · N250UP · Doug MD11F · Wing, Plate/Skin
  > INSPECTION TYPE:3CRT WING REAR SPAR VERTICAL TEE ANGLE CRACK AT LOWER END.REMOVED AND REPLACED CRACKED TEE ANGLE IAW SRM 51-33-01 AND 51-31-01 (MINOR).
- [SDR IPXA2022072084361](https://openairdocs.org/sdr/IPXA2022072084361.md): Support Bracket · broken · Jul 8, 2022 · N250UP · Doug MD11F · Flight Compartment Lighting
  > INSPECTION TYPE:3CLH WING O/B FLAP I/B HINGE CHANNEL SUPPORT BRACKET BROKEN.REMOVED,FABRICATED AND REPLACED BROKEN SUPPORT BRACKET IAW SRM 51-31-01 (MINOR).
- [SDR IPXA2022072384468](https://openairdocs.org/sdr/IPXA2022072384468.md): Stiffener · cracked · Jul 7, 2022 · N250UP · Doug MD11F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:3CAFT CARGO COMPARTMENT VERTICAL STIFFENER CRACK AT STA.1841 LON 47R.REMOVED,FABRICATED AND REPLACED CRACKED STIFFENER IAW SRM 51-33-01 AND 51-31-01 (MINOR).
- [SDR IPXA2022072084360](https://openairdocs.org/sdr/IPXA2022072084360.md): Panel Support · cracked · Jul 7, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CRH WING FIXED L/E COMPARTMENT DOUBLER(PANEL LANDING) CRACK AT XOS STA.606.REMOVED,FABRICATED AND REPLACED CRACKED DOUBLER IAW SRM 51-33-01 (MINOR).
- [SDR IPXA2022071884261](https://openairdocs.org/sdr/IPXA2022071884261.md): Doubler · cracked · Jul 7, 2022 · N250UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 667.76 TO 673.76.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 667.76 TO 673.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022071884260](https://openairdocs.org/sdr/IPXA2022071884260.md): Doubler · cracked · Jul 7, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS.660.71 TO 667.76.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 660.71 TO 667.76 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022071584191](https://openairdocs.org/sdr/IPXA2022071584191.md): Doubler · cracked · Jul 7, 2022 · N250UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:3CL/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 906.58 TO 912.02.REPAIRED CRACKED L/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 906.58 TO 912.02 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022071584192](https://openairdocs.org/sdr/IPXA2022071584192.md): Doubler · cracked · Jul 6, 2022 · N250UP · Doug MD11F · Wing, Attach Fittings
  > INSPECTION TYPE:3CR/H WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN STA. XOS. 648.299 TO 653.0.REPAIRED CRACKED R/H WING FIXED L/E BEADED DOUBLER BETWEEN STA. XOS. 648.299 TO 653.0 IAW SRM 57-40-02 REPAIR 15 FIG. 205. (MAJOR)
- [SDR IPXA2022072184422](https://openairdocs.org/sdr/IPXA2022072184422.md): Floor Panel · corroded · May 18, 2022 · N250UP · Doug MD11F · Fuselage Main, Structure
  > INSPECTION TYPE:3CRCB FLOOR PANEL P/N WSP0789-502 WITH CORROSION AT STA X=-47.5 TO X=-75.250.REMOVED, REPLACED FLOOR PANEL IAW SRM 51-31-01 (MINOR)
- [SDR IPXA2022020478651](https://openairdocs.org/sdr/IPXA2022020478651.md): None · will not arm · Feb 4, 2022 · N250UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:NAL1 DOOR WILL NOT ARMLUBRICATING THE L1 DOOR SLIDE ARM HANDLE & OPS CHK NML PER AMM 52-61-15.
- [SDR IPXA2021071971846](https://openairdocs.org/sdr/IPXA2021071971846.md): Door Track · broken · Jul 18, 2021 · N250UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AFITTING ON L1 DOOR TRACK AFT LOWER SIDE BROKEN THAT HOLDS AFT LOWER CABLETT REPAIRS FABRICATED NEW BRACKET FROM BOEING AWG ABA 7864 REV IR ON CERT.# MX10417. DRILLED ALODINED & PRIMED[CS1195530 7-18-21] PERFORMED PENETRANT FLUORECENT INSP PE
- [SDR IPXA2021071771784](https://openairdocs.org/sdr/IPXA2021071771784.md): Pulley · inoperative · Jul 17, 2021 · N250UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE:N/AL1 DOOR LOWER AFT PULLEY RREQUIRES CABLE PULLEY GUIDE TO BE DRILLED AND RIVETED ONDRILLED AND INSTALLED PULLEY GUIDE ON NEW ASSY AS REQUIRED - REF SRM-51-35-01
- [SDR IPXA2021071371607](https://openairdocs.org/sdr/IPXA2021071371607.md): Tensioner · inoperative · Jul 12, 2021 · N250UP · Doug MD11F · Passenger/Crew Doors
  > L1 DOOR AFT LOWER CABLE TENSIONER BROKEN. DOOR C/B PULLED AND COLLARED. PLACED L1 PASSENGER DOOR DRIVE CABLE LOWER AFT ON DEFERRAL I/A/W MEL 52-10-2-2-1 DMP COMPLIED WITH DEFERRAL #M750006 C/B'S CLOSED. PARTS REQ #359273. ESR: 53-42-03-10REPLACED L1 PASSENGER
- [SDR IPXA2021070771372](https://openairdocs.org/sdr/IPXA2021070771372.md): Battery · faulted · Jul 6, 2021 · N250UP · Doug MD11F · Emergency Lighting
  > EMBER BAT 1 LO EIS ALERT. DEFERRED ITEM USING MEL 33-50-4 ACCOMPLISHED DMP. PULLED & COLLARED 5 CB'S & DISCONNECTED.DMP 33-50-4 REVERSED. REPLACED EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51-01-401. THIS CLEARS DEFERRAL M749412, PLACARD REMOVED.
- [SDR IPXA2021021065541](https://openairdocs.org/sdr/IPXA2021021065541.md): Unknown · smoke · Feb 10, 2021 · N250UP · Doug MD11F · Air Distribution System
  > INSPECTION TYPE:NA**ATB-EMERGENCY DECLARED-LANDED SAFE & TAXIED UNDER OWN POWER - NO EMERG EQUIP USED - AC TAKEN OOS** ON DEPARTURE PASSING 18000FB VISIBLE HAZY SMOKE WAS ENTERING FLIGHTDECK EMERGENCY DECLARED AOM CHECK LIST ACCOMPLISHED WHICH CLEARED THE SMOK
- [SDR IPXA2020100761053](https://openairdocs.org/sdr/IPXA2020100761053.md): Door · stuck · Oct 6, 2020 · N250UP · Doug MD11F · Passenger/Crew Doors
  > INSPECTION TYPE: NA ENTRY DOOR 1L SLIDE PANEL STUCK IN OPEN POSTION. PERFORMED OPERATIONAL CHECK OF 1L FWD PASSENGER/CREW DOOR, IAW MD11 AMM 52 10 01 700 801. DOOR OPERATES FULLY OPENED AND CLOSED WITH NO PANELS STICKING/OBSTRUCTIONS.
- [SDR IPXA2020092560625](https://openairdocs.org/sdr/IPXA2020092560625.md): Fairing · cracked · Sep 25, 2020 · N250UP · Doug MD11F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE: 2C NR 2 ENG PYLON FAIRING 488FL CRACKED. REPAIRED NR 2 ENG PYLON FAIRING, IAW VT-SAA EA NR 011-5450-01-A8576 I/R AND UPS EO NR MD11-5480-77944-A. MINOR.
- [SDR IPXA2020092560620](https://openairdocs.org/sdr/IPXA2020092560620.md): Floorbeam · cracked · Sep 25, 2020 · N250UP · Doug MD11F · Fuselage Main, Floor Beam
  > INSPECTION TYPE: 2C CENTER CARGO FLOOR SUPPORT ANGLE CRACK AT STA 1721. REPAIRED CENTER CARGO FLOOR SUPPORT ANGLE AT STA 1721, IAW SRM 51-35-01, VT-SAA EA NR 011-5300-01-A8572 I/R AND UPS EO NR MD11-5300-77923-A. (MINOR)
- [SDR IPXA2020092560613](https://openairdocs.org/sdr/IPXA2020092560613.md): Hinge Bracket · corroded · Sep 25, 2020 · N250UP · Doug MD11F · Wing, Control Surface Attach Fittings
  > INSPECTION TYPE: 2C RT WING TRAILING EDGE INBOARD FLAP OUTBOARD HINGE BRACKET ASSY HAS CORROSION. REPAIRED RT WING TRAILING EDGE INBOARD FLAP OUTBOARD HINGE BRACKET ASSY, IAW VT-SAA EA NR 011-5700-01-A8557 I/R AND UPS EO NR MD11-5740-77940-A. (MINOR)
- [SDR IPXA2020092560612](https://openairdocs.org/sdr/IPXA2020092560612.md): Angle · broken · Sep 25, 2020 · N250UP · Doug MD11F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE: 2C NR 2 PYLON ACCESS FAIRING 458AR FWD LT RIB 'T' ANGLE BROKEN OUT. REMOVED AND REPLACED NR 2 PYLON ACCESS FAIRING 'T' ANGLE, IAW VT-SAA EA NR 011-5450-01-A8566 I/R AND UPS EO NR MD11-5450-77890-A. (MINOR)
- [SDR IPXA202009160264](https://openairdocs.org/sdr/IPXA202009160264.md): Intercostal · cracked · Sep 15, 2020 · N250UP · Doug MD11F · Air Conditioning Doors
  > INSPECTION TYPE: 2C LT NR 2 A/C BAY DOOR CENTER INTERCOSTAL CRACKED. REMOVED AND INSTALLED CRACKED NR 2 A/C BAY DOOR INTERCOSTAL, IAW SRM 51-35-01 AND SRM 51-33-01 (MINOR).
- [SDR IPXA2020092360560](https://openairdocs.org/sdr/IPXA2020092360560.md): Rib · corroded · Sep 12, 2020 · N250UP · Doug MD11F · Elevator, Spar/Rib
  > INSPECTION TYPE: 2C LT OUTBOARD ELEVATOR NR 3 RIB FROM INBOARD HAS CORROSION. REMOVED AND REPLACED CORRODED LT OUTBOARD ELEVATOR NR 3 RIB FROM INBOARD, IAW MD-11 SRM 51-31-01 AND 51-33-01. (MINOR)
- [SDR IPXA2020092360559](https://openairdocs.org/sdr/IPXA2020092360559.md): Bushing · migrated · Sep 11, 2020 · N250UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE: 2C RT OUTBOARD ELEVATOR NR 5 MOUNT FITTING OUTBOARD BUSHING IS MIGRATED. REPAIRED RT OUTBOARD ELEVATOR NR 5 MOUNT FITTING OUTBOARD BUSHING BORE, IAW VT-SAA EA 011-5510-01-A8561 REV IR AND UPS EO MD11-5520-77918-A. (MINOR)
- [SDR IPXA2020092860717](https://openairdocs.org/sdr/IPXA2020092860717.md): Skin · damaged · Sep 10, 2020 · N250UP · Doug MD11F · Horizontal Stabilizer, Plate/Skin
  > INSPECTION TYPE: 2C RT HORIZ STAB LEADING EDGE ASSY HAS A DRILL START AND CORROSION IN FASTENER HOLE. REPAIRED RT HORIZ STAB LEADING EDGE ASSY, IAW VT-SAA EA 011-5510-01-A8565 REV I/R AND UPS EO MD11-5510-77934-A. MINOR.
- [SDR IPXA2020092460590](https://openairdocs.org/sdr/IPXA2020092460590.md): Floor Support · corroded · Sep 10, 2020 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C FLOOR PANEL SUPPORT IS CORRODED BETWEEN STA 392-440 AND X= -8.5 TO X= -27.5. REMOVED, FABRICATED, AND REPLACED FLOOR SUPPORT, IAW DWG WSP0668 AND SRM 51-33-01. (MINOR)
- [SDR IPXA2020092360558](https://openairdocs.org/sdr/IPXA2020092360558.md): Fitting · migrated · Sep 10, 2020 · N250UP · Doug MD11F · Elevator Structure
  > INSPECTION TYPE: 2C LT OUTBOARD ELEVATOR NR 6 MOUNT FITTING OUTBOARD BUSHING IS MIGRATED. REPAIRED LT OUTBOARD ELEVATOR NR 6 MOUNT FITTING OUTBOARD BUSHING BORE, IAW VT-SAA EA 011-5510-01-A8560 REV IR AND UPS EO MD11-5520-77927-A. (MINOR)
- [SDR IPXA2020092860728](https://openairdocs.org/sdr/IPXA2020092860728.md): Channel · corroded · Sep 9, 2020 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C CENTER CARGO LOADING SYSTEM CHANNEL HAS CORROSION BETWEEN STA 1571 TO 1611 AND X= -33. REPAIRED CORRODED CENTER CARGO LOADING SYSTEN CHANNEL BETWEEN STA 1571 TO 1611 AND X= -33, IAW UPS EO MD11-2550-77908-A. MAJOR.
- [SDR IPXA2020092460582](https://openairdocs.org/sdr/IPXA2020092460582.md): Intercostal · cracked · Sep 9, 2020 · N250UP · Doug MD11F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: 2C LOWER FWD CARGO BETWEEN STA 6-30 TO 6-50 & ABOVE L43L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL, IAW DWG ACA7049 AND SRM 51-33-01.

Next page: https://openairdocs.org/aircraft/N250UP/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 = 'N250UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N250UP/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
