# Service difficulty reports: N394UP

A list on [N394UP](https://openairdocs.org/aircraft/N394UP.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 2 · 74 reports

- [SDR IPXA2026052458954](https://openairdocs.org/sdr/IPXA2026052458954.md): Channel · corroded · May 13, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > - CORROSION - CHANNEL, R/H MAIN L/G SHOCK STRUT DOOR AFT LOWER CORNER INBD SIDE. INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND DWG 113T8201 SH 4 REV: C
- [SDR IPXA2026052436510](https://openairdocs.org/sdr/IPXA2026052436510.md): Filler · corroded · May 12, 2026 · N394UP · Boeing 767381 · Cargo/Baggage Doors
  > FAULT - CORROSION - FILLER, AFT CGO DOOR FWD LOWER HOOK SUPPORT STRUCTURE, DOOR STA 175, BEAM NO. 10 (REPLACE) INSTALL NEW RADIUS FILLER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 140T2610 SH 1 REV: B
- [SDR IPXA2026052037295](https://openairdocs.org/sdr/IPXA2026052037295.md): Fairing · debonded · May 12, 2026 · N394UP · Boeing 767381 · Aerodynamic Fairings
  > - DISBOND - PNL, AFT WING TO BODY FAIRING L/H PNL NO: 195PL. I.A.W AMM 53-66-01-404-003 REV.148 INSTALL PNL NO.195PL.
- [SDR IPXA2026052439460](https://openairdocs.org/sdr/IPXA2026052439460.md): Web · corroded · May 12, 2026 · N394UP · Boeing 767381 · Wing Miscellaneous Structure
  > CORROSION - WEB, L/H WING FIXED T/E REAR SPAR STA WS248 FUEL JETTISON TRANSFER VALVE FIXED POINT. I.A.W AMM 28-31-04-404-004 REV 148 INSTALLED THE ACTUATOR OF THE TRANSFER VALVE.
- [SDR IPXA2026052439830](https://openairdocs.org/sdr/IPXA2026052439830.md): Bushing · worn · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon Structure
  > WORN - BUSHING, NR 2 ENG R/H CORE COWL R/H SIDE PRESSURE RELIFE DOOR UPPER AND LOWER SIDE, TOTAL: 2EA..INSTALL NEW BUSHING I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026052237060](https://openairdocs.org/sdr/IPXA2026052237060.md): Depressor · broken · May 12, 2026 · N394UP · Boeing 767381 · Fuselage Main, Structure
  > FOUND M/D CGO DOOR AFT CUTOUT DISPRESSOR SEAL BROKEN (2EA). DUE TO TYPO FOUND IN CORRECTIVE ACTION 6, CORRECT REFERENCE SHOULD BE:<BR>INSTALLED THE DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV.148, TORQUED THE SCREW TO 25 IN-LB.
- [SDR IPXA2026052137024](https://openairdocs.org/sdr/IPXA2026052137024.md): Skin · debonded · May 12, 2026 · N394UP · Boeing 767381 · Trailing Edge Flaps
  > DEBONDED SKIN, RT WING OUTBD FLAP TE WEDGE. (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA,PER 767 NDT MANUAL PART 1 51-01-01 REV:143 RESULT:NO DEFECT WAS FOUND
- [SDR IPXA2026052036566](https://openairdocs.org/sdr/IPXA2026052036566.md): Strut · cracked · May 12, 2026 · N394UP · Boeing 767381 · Wing Main, Frame Structure
  > CRACKED, UPPER AND LOWER CHORD, RT WING OUTBD FXD LE CAVITY RIB, OSS 531.71. INSTALLED NEW CHORD IAW SRM 51-40-02-0G REV.55 AND DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 1, REV G.
- [SDR IPXA2026052039321](https://openairdocs.org/sdr/IPXA2026052039321.md): Seal · broken · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > BROKEN - SPRING, NR 2 PYLON AFT FAIRING PANEL NR 446CL. INSTALLED NEW SEAL IAW SRM 51-40-02-0G, REV 55 AND DWG 311T2570, SH 1, REV N.
- [SDR IPXA2026052039547](https://openairdocs.org/sdr/IPXA2026052039547.md): Fairing · cracked · May 12, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CRACKED FILLET FAIRING, NO. 2 ENG R/H T/R TRANSLATING COWL INNER SIDE BETWEEN NO. 5 AND NO. 6 BLOCKER DOOR. REMOVED DAMAGE FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55. INSTALLED NEW FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55 AND IPC 78-32-32 REV.96.
- [SDR IPXA2026052040024](https://openairdocs.org/sdr/IPXA2026052040024.md): Rub Strip · cracked · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > CRACKED RUB STRIP, NR 2 ENG RT CORE COWL INNER SIDE UPPER AREA. INSTALLED NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026052040363](https://openairdocs.org/sdr/IPXA2026052040363.md): Rub Strip · cracked · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > CRACKED RUB STRIP, NO. 2 ENG L/H CORE COWL INNER SIDE UPPER AREA. I.A.W. AMM 71-11-06-714-013-H00 REV.148 INSTALLED THE CORE COWL. CONDITION CHECKED NORMAL AND JOB COMPLETED. INSTALL NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURES
- [SDR IPXA2026051740055](https://openairdocs.org/sdr/IPXA2026051740055.md): Bracket · chafed · May 12, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG RT T/R COWL LOWER FWD CLOSURE PANEL T/E. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND ST ENGINEERING IPC 78-32-22 REV 96.
- [SDR IPXA2026051739573](https://openairdocs.org/sdr/IPXA2026051739573.md): Bracket · chafed · May 12, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG LT T/R COWL LOWER FWD CLOSURE DOOR T/E. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND ST ENGINEERING IPC 78-32-21, REV.96.
- [SDR IPXA2026051939604](https://openairdocs.org/sdr/IPXA2026051939604.md): Adapter · gouged · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon Miscellaneous Structure
  > GOUGEED BRACKET, NR 2 ENG LT CORE COWL HOLD-OPEN ROD RECIVER. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026051939610](https://openairdocs.org/sdr/IPXA2026051939610.md): Bracket · gouged · May 12, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon Miscellaneous Structure
  > GOUGED BRACKET, NR 2 ENG RT CORE COWL HOLD-OPEN ROD RECEIVER. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-24 REV. 50
- [SDR IPXA2026051739973](https://openairdocs.org/sdr/IPXA2026051739973.md): Duct · chafed · May 12, 2026 · N394UP · Boeing 767381 · Engine Collector/Tailpipe/Nozzle
  > CHAFED DUCT, NR 2 ENG RT CORE COWL INNER EXHAUST DUCT L/E AREA. REPAIRED DAMAGE AREA IAW ROHR SB 71-032 REV NR 2.
- [SDR IPXA2026052424954](https://openairdocs.org/sdr/IPXA2026052424954.md): Channel · corroded · May 11, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > CORRODED CHANNEL L/H MAIN L/G SHOCK STRUT FAIRING DOOR AFT LOWER CORNER. (REPLACE) Â INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 113T8201 SH 4 REV: C
- [SDR IPXA2026052022086](https://openairdocs.org/sdr/IPXA2026052022086.md): Seal · broken · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > BROKEN SEAL, NR 1 PYLON FAIRING PNL 436CL SPRING SEAL AREA. INSTALL NEW SEAL I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 311T2570 SH 1 REV: N.
- [SDR IPXA2026052024998](https://openairdocs.org/sdr/IPXA2026052024998.md): Spring · broken · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > BROKEN- SPRING, NR 2 PYLON AFT FAIRING PANEL NO. 446CR. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 311T2570, SH 1, REV N.
- [SDR IPXA2026051721345](https://openairdocs.org/sdr/IPXA2026051721345.md): Longeron · chafed · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > CHAFED LONGERON, NR 1 ENG LT CORE COWL EXTERNAL AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026051721898](https://openairdocs.org/sdr/IPXA2026051721898.md): Rub Strip · corroded · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon Miscellaneous Structure
  > CORRODED RUB STRIP, NR 1 ENG, LT CORE COWL EXTERNAL L/E RUB STRIP, 8:00 - 9:00 POS. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.
- [SDR IPXA2026051721983](https://openairdocs.org/sdr/IPXA2026051721983.md): Bracket · chafed · May 11, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG, RT T/R FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-22, REV 96.
- [SDR IPXA2026051722065](https://openairdocs.org/sdr/IPXA2026051722065.md): Bracket · chafed · May 11, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 LT T/R FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-21, REV 96.
- [SDR IPXA2026051722098](https://openairdocs.org/sdr/IPXA2026051722098.md): Angle · cracked · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD OTBD SIDE SUPPORT ANGLE. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:313T2303 SH 131 REV.- AND BOEING DWG NO: 313T2303 SH. 136 REV. -.
- [SDR IPXA2026051722233](https://openairdocs.org/sdr/IPXA2026051722233.md): Longeron · chafed · May 11, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > CHAFED LONGERON NR 1 ENG RT CORE COWL INNER SKIN AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV. 50.
- [SDR IPXA2026051924905](https://openairdocs.org/sdr/IPXA2026051924905.md): Guard · broken · May 11, 2026 · N394UP · Boeing 767381 · Leading Edge Slat Control System
  > FOUND LEFT WING INBOARD SLAT TORQUE TUBE GUARD BROKEN AT WBL 121.0. I.A.W AMM 20-11-00-910-802 REV 148 REPLACE LEFT WING INBOARD SLAT TORQUE TUBE GUARD AT WBL 121.0.
- [SDR IPXA2026052012733](https://openairdocs.org/sdr/IPXA2026052012733.md): Angle · cracked · May 10, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.A
- [SDR IPXA2026052012537](https://openairdocs.org/sdr/IPXA2026052012537.md): Channel · chafed · May 10, 2026 · N394UP · Boeing 767381 · Engine Thrust Reverser
  > CHAFED CHANNEL, NR 1 ENG R/H T/R AFT LWR FAIRING L/E AREA. INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND ST ENGINEERING IPC 78-32-02 REV.96
- [SDR IPXA2026052012545](https://openairdocs.org/sdr/IPXA2026052012545.md): Former · cracked · May 10, 2026 · N394UP · Boeing 767381 · Wing, Fuselage Attach Fittings
  > CRACKED FORMER, RT WING OUTBD FXD LE NOSE SKIN, OSS 456.98. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG 114T2202 SH 1 REV D AND UPS SREO-57209-REQ001 REV2
- [SDR IPXA2026052012498](https://openairdocs.org/sdr/IPXA2026052012498.md): Angle · cracked · May 10, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACKED AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV.55 AND BOEING DWG 657T1332 SH 5 REV.A.
- [SDR IPXA2026051912479](https://openairdocs.org/sdr/IPXA2026051912479.md): Fireshield · chafed · May 10, 2026 · N394UP · Boeing 767381 · Nacelle/Pylon, Main Frame
  > CHAFED FIRESHIELD, NR 1 ENG FAIRING PANEL 436BL INNER PLATE AREA. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 55, & DWG 311T2570, SH 1, REV N.
- [SDR IPXA2026052480150](https://openairdocs.org/sdr/IPXA2026052480150.md): Skin · cracked · May 8, 2026 · N394UP · Boeing 767381 · Passenger/Crew Doors
  > DURING PERFORM EO-87307-JIC1 FOUND L1 DOOR AFT DOOR CORNER HOLE CRACK. (REPAIR) ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 55 AND EGAT WORK SHEET NO: 60372 AND UPS EO-87307-REQ7 REV2.
- [SDR IPXA2026052080887](https://openairdocs.org/sdr/IPXA2026052080887.md): Angle · cracked · May 8, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.A
- [SDR IPXA2026052081117](https://openairdocs.org/sdr/IPXA2026052081117.md): Angle · cracked · May 8, 2026 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > FOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.A
- [SDR IPXA202605081013](https://openairdocs.org/sdr/IPXA202605081013.md): Pawl · worn · May 8, 2026 · N394UP · Boeing 767381 · Passenger/Crew Doors
  > THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. OPEN
- [SDR IPXA2024052191404](https://openairdocs.org/sdr/IPXA2024052191404.md): Skin Panel · corroded · May 3, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > **SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, L/H WING INBD INSPAR SKIN WBL 97 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90375-REQ1 REV.1 AND BOEING DWG NO. 112T4000 SH 9 REV. B AND NO. 112T4000 SH 8 REV. JOB COMPLETED. PAPER CHECK OK.
- [SDR IPXA2024052191453](https://openairdocs.org/sdr/IPXA2024052191453.md): Skin · corroded · May 3, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > CORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90935-REQ1 REV.1. REVIEW COMPLETED
- [SDR IPXA2024052096856](https://openairdocs.org/sdr/IPXA2024052096856.md): Support · corroded · May 3, 2024 · N394UP · Boeing 767381 · Fuselage Miscellaneous Structure
  > CORROSION - CLIP, L/H ENVIRONMENTAL CONTROL BAY LOWER RIB SUPPORT, STA 924, LBL 19 (REPLACE) INSTALLED FABRICATED PART I.A.W SRM 51-40-02-0G REV. 49. AND BOEING DWG NO: 149T7370 SH.1 REV. F.
- [SDR IPXA2024052199027](https://openairdocs.org/sdr/IPXA2024052199027.md): None · none · May 3, 2024 · N394UP · Boeing 767381 · Standard Practices/Structures
  > (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.
- [SDR IPXA2024052091487](https://openairdocs.org/sdr/IPXA2024052091487.md): Skin Panel · corroded · May 3, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > *** SUPPLEMENTAL SDR *** FAULT - EXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) ACCOMPLISH REPAIR I.A.W EO-90394-REQ1 REV. 1. JOB COMPLETED.
- [SDR IPXA2024051791453](https://openairdocs.org/sdr/IPXA2024051791453.md): Skin · corroded · May 3, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > **SDR FILED OPEN**FAULT - CORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) REVIEW COMPLETED
- [SDR IPXA2024051691487](https://openairdocs.org/sdr/IPXA2024051691487.md): Skin Panel · corroded · May 3, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > EXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) REVIEW COMPLETE
- [SDR IPXA2024050399027](https://openairdocs.org/sdr/IPXA2024050399027.md): None · none · May 3, 2024 · N394UP · Boeing 767381 · Standard Practices/Structures
  > OPEN, FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.
- [SDR IPXA2024052076482](https://openairdocs.org/sdr/IPXA2024052076482.md): Skin Panel · corroded · May 2, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > CORROSION - SKIN, L/H WING OUTBD VORTEX GENERATORS AREA, WS720 TO WS772. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90376-REQ1 REV.1 AND BOEING DWG NO. 112T3000 SH 16 REV. -.
- [SDR IPXA2024052074092](https://openairdocs.org/sdr/IPXA2024052074092.md): Fitting · corroded · May 2, 2024 · N394UP · Boeing 767381 · Fuselage Main, Attach Fittings
  > FOUND BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM FITTING DAMAGED AT STA 1593 LBL 54.5. (REPLACE) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANELS AND CONDITION CHECK NORMAL
- [SDR IPXA2024052074066](https://openairdocs.org/sdr/IPXA2024052074066.md): Fitting · corroded · May 2, 2024 · N394UP · Boeing 767381 · Fuselage Main, Attach Fittings
  > FOUND BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM FITTING DAMAGED, AT STA 1593 LBL 55. (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 49. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 49. AND BOEING DWG NO. 657T1332 SH. 7 REV. A. AND 657T133
- [SDR IPXA2024052073956](https://openairdocs.org/sdr/IPXA2024052073956.md): Skin Panel · corroded · May 2, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > *** SUPPLEMENTAL SDR *** FAULT - CORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90393-REQ1 REV.1 AND SRM 51-40-04-0G REV. 49 AND BOEING DWG NO. 112T4323 SH5 REV. C; NO. 112T5000 SH
- [SDR IPXA2024051673956](https://openairdocs.org/sdr/IPXA2024051673956.md): Skin Panel · corroded · May 2, 2024 · N394UP · Boeing 767381 · Wing, Plate/Skin
  > CORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISH REPAIR PER EO-90393-REQ1 AND EGAT EI F2024A57M-1171, REV. 4 (REF. T3F18E004H051) PRIOR TO FURTHER FLIGHT.
- [SDR IPXA2024051639459](https://openairdocs.org/sdr/IPXA2024051639459.md): Bulkhead · cracked · Apr 30, 2024 · N394UP · Boeing 767381 · Fuselage Main, Bulkhead
  > FOUND NOSE W/W AFT BULKHEAD LH BL25 CHORD CRACK (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 51-70-12-OG-0 REV.49 AND EGAT WORK SHEET NO.40374. JOB COMPLETED.

Next page: https://openairdocs.org/aircraft/N394UP/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 = 'N394UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N394UP/reports

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