# Service difficulty reports: N371UP

A list on [N371UP](https://openairdocs.org/aircraft/N371UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR IPXA2026091808623](https://openairdocs.org/sdr/IPXA2026091808623.md): Switch · broken · Sep 18, 2026 · N371UP · Boeing 767300 · Emergency Lighting
  > ON SECURE FLIGHT CHECKLIST EMERGENCY LIGHTS SWITCH BRACKET BROKE OFF. SWITCH STILL SEEMS TO FUNCTION NORMALLY. C/W AMM 33-51-08. R/R EMERGENCY LIGHT SWITCH OPS CHECK GOOD.
- [SDR IPXA2026060263875](https://openairdocs.org/sdr/IPXA2026060263875.md): Slat System · warning message · Jun 2, 2026 · N371UP · Boeing 767300 · Leading Edge Slat Position Indicating System
  > EMERGENCY DECLARED, LE SLAT DISAGREE EICAS MESSAGE WHEN FLAPS SELECTED ON APPROACH TO 25. PERFORMED QRH PROCEDURE ACCOMPLISHED FIM FLAP/SLAT ELECTRONIC UNIT BITE PROCEDURE 27-51 FAULT TREE 809 NO FAULTS NOTED. RAN FLAPS THRU FULL RANGE 5 TIMES. NO FAULTS OR E
- [SDR IPXA2026051938822](https://openairdocs.org/sdr/IPXA2026051938822.md): Former · cracked · May 18, 2026 · N371UP · Boeing 767300 · Wing Main, Frame Structure
  > FORMER, RT WING OUTBD L/E CAVITY CURTAIN SUPPORT NEAR OSS 441. INSTALLED NEW FORMER I.A.W UPS SREO-54290-REQ1 REV.2 AND SRM 51-40-02-0G REV.95 AND BOEING DWG NO.114T2241 SH.4 REV-.
- [SDR IPXA2026052013581](https://openairdocs.org/sdr/IPXA2026052013581.md): Angle · cracked · May 16, 2026 · N371UP · Boeing 767300 · Nacelle/Pylon Miscellaneous Structure
  > CRACKED ANGLE NR 1 PYLON LOWER FAIRING NAC STA 376 FRAME AFT INBOARD. CONDITION CHECK NORMAL. INSTALLED NEW CLIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.313T2303 SH.161 REV.- AND DWG NO.313T2303 SH.166 REV.-
- [SDR IPXA2026052100698](https://openairdocs.org/sdr/IPXA2026052100698.md): Seal · broken · May 15, 2026 · N371UP · Boeing 767300 · Nacelle/Pylon, Main Frame
  > BROKEN SEAL, NR 2 PYLON RT FAIRING PANEL 446 CR. INSTALLED NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO.311T2570 SH.16 REV.-
- [SDR IPXA2026052001001](https://openairdocs.org/sdr/IPXA2026052001001.md): Bracket · chafed · May 15, 2026 · N371UP · Boeing 767300 · Nacelle/Pylon, Main Frame
  > CHAFING - BRACKET ASSY, NR 1 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.95. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND CMM IPL 71-13-23 REV.47.
- [SDR IPXA2026051900631](https://openairdocs.org/sdr/IPXA2026051900631.md): Former · cracked · May 15, 2026 · N371UP · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER, RT WING OUTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2161 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REV2.
- [SDR IPXA2026051800614](https://openairdocs.org/sdr/IPXA2026051800614.md): Former · cracked · May 15, 2026 · N371UP · Boeing 767300 · Wing Main, Frame Structure
  > CRACKED FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 565.9. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2162 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REV2.
- [SDR IPXA2026051800673](https://openairdocs.org/sdr/IPXA2026051800673.md): Former · cracked · May 15, 2026 · N371UP · Boeing 767300 · Wing Main, Frame Structure
  > CRACK - FORMER, FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM, OSS 499.6 (REPLACE) 1. REMOVE DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2161 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REV
- [SDR IPXA2026051880648](https://openairdocs.org/sdr/IPXA2026051880648.md): Bracket · cracked · May 14, 2026 · N371UP · Boeing 767300 · Wing, Attach Fittings
  > CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV.95. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND DWG 114T1240, SH 6, REV-.
- [SDR IPXA2026051880666](https://openairdocs.org/sdr/IPXA2026051880666.md): Hinge · worn · May 14, 2026 · N371UP · Boeing 767300 · Fuselage, Door Hinge
  > FOUND LEFT RAM INLET DOOR FWD HINGE WORN OUT. REPLACED CONDITION CHECK NORMAL. INSTALLED NEW HINGE I.A.W SRM 51-40-02-0G REV.95 AND AIPC 21-53-61-05A REV.142.
- [SDR IPXA2026052162489](https://openairdocs.org/sdr/IPXA2026052162489.md): Bumper · broken · May 13, 2026 · N371UP · Boeing 767300 · Passenger/Crew Doors
  > FOUND L1 ENTRY DOOR BUMPER BROKEN. REPLACED I.A.W DWG 411T2036 SHEET 1 REV.H AND PSDL 411T2240 SHEET DL REV.A REPLACE BUMPER.
- [SDR IPXA2026051765497](https://openairdocs.org/sdr/IPXA2026051765497.md): Floor Panel · damaged · May 13, 2026 · N371UP · Boeing 767300 · Fuselage Floor Panel
  > MAJOR REPAIR, FOUND MAIN DECK FLOOR PANEL DAMAGED 252UFF. REPAIRED IAW AMM 25-57-02-404-016, AMM 25-57-05-404-006, AMM 25-58-01-404-005, AND AMM 25-58-04-404-015, REV 148, INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL..I.A.W AMM 53-01-06-4
- [SDR IPXA2026051362489](https://openairdocs.org/sdr/IPXA2026051362489.md): Bumper · broken · May 13, 2026 · N371UP · Boeing 767300 · Passenger/Crew Doors
  > FOUND L1 ENTRY DOOR BUMPER BROKEN. (REPLACE)
- [SDR IPXA2026052501937](https://openairdocs.org/sdr/IPXA2026052501937.md): Skin · dented · Apr 21, 2026 · N371UP · Boeing 767300 · Trailing Edge Flaps
  > R/H OUTBOARD FLAP, BOTTOM INBOARD SIDE APPROX 15IN FROM INNER SIDE HAD 6 DENTS. REPAIR DENTS ON LOWER SURFACE OF LOWER PANEL ON R/H WING OUTBD T/E FLAP NEAR OTEF STA 25 I.A.W. UPS EO-97203-REQ3 REV.1 AND EGAT EI NO. F2026A57M-1046 REV.1
- [SDR IPXA2026052101937](https://openairdocs.org/sdr/IPXA2026052101937.md): Skin · dented · Apr 21, 2026 · N371UP · Boeing 767300 · Trailing Edge Flaps
  > RT OUTBOARD FLAP, BOTTOM INBOARD SIDE APPROX 15IN FROM INNER SIDE HAD 6 DENTS ACCOMPLETED RII ITEM CHECK FOR STEP 10.
- [SDR IPXA2024052677894](https://openairdocs.org/sdr/IPXA2024052677894.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > **SUPPLEMENTAL SDR** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE).I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-
- [SDR IPXA2024052677589](https://openairdocs.org/sdr/IPXA2024052677589.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > **SUPPLEMENTAL SDR** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE). I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04
- [SDR IPXA2024052977830](https://openairdocs.org/sdr/IPXA2024052977830.md): Former · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Wing Main, Frame Structure
  > - CRACK - FORMER, LH WING OUTBD FXD LE OSS 441.6 NOSE SKIN (REPLACE).REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 114T2241 SH. 4 REV. JOB COMPLETED. REVIEW COMPLETED
- [SDR IPXA2024052977775](https://openairdocs.org/sdr/IPXA2024052977775.md): Skin · punctured · May 21, 2024 · N371UP · Boeing 76734AF · Wing, Plate/Skin
  > - PUNCTURE - SKIN, LH WING OUTBD LE LWR FXD PNL 521RB (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (DIAMETER:2", DEPTH:3" PLIES", 9.5" FROM LEADING EDGE, 6" FROM RIGHT HAND). BONDED FIBERGLASS PREPREG REPAIR PLIES WITH FILM ADHESIVE
- [SDR IPXA2024052677570](https://openairdocs.org/sdr/IPXA2024052677570.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBD SIDE CRACKED I.A.W AMM 25-59-01-404-019 REV.142 INSTALL MAIN DECK CARGO DADO PANEL AND CONDITION CHECK NORMAL. REVIEW COMPLETED
- [SDR IPXA2024052277775](https://openairdocs.org/sdr/IPXA2024052277775.md): Skin · punctured · May 21, 2024 · N371UP · Boeing 76734AF · Wing, Plate/Skin
  > *** SDR FILED OPEN *** FAULT - PUNCTURE - SKIN, LH WING OUTBD LE LWR FXD PNL 521RB (REPAIR) OKAY TO WORK
- [SDR IPXA2024052277830](https://openairdocs.org/sdr/IPXA2024052277830.md): Former · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Wing Main, Frame Structure
  > CRACK - FORMER, LH WING OUTBD FXD LE OSS 441.6 NOSE SKIN (REPLACE) OKAY TO WORK OPEN
- [SDR IPXA2024052177894](https://openairdocs.org/sdr/IPXA2024052177894.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > SDR FILED OPEN - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE)
- [SDR IPXA2024052177589](https://openairdocs.org/sdr/IPXA2024052177589.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > SDR FILED OPEN - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE)
- [SDR IPXA2024052177570](https://openairdocs.org/sdr/IPXA2024052177570.md): Angle · cracked · May 21, 2024 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > SDR FILED OPEN - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 OUTBD SIDE (REPLACE)
- [SDR IPXA2024052962645](https://openairdocs.org/sdr/IPXA2024052962645.md): Drain · none · May 20, 2024 · N371UP · Boeing 76734AF · Standard Practices/Structures
  > **SUPPLEMENTAL SDR** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173-JIC001.
- [SDR IPXA2024052062645](https://openairdocs.org/sdr/IPXA2024052062645.md): None · none · May 20, 2024 · N371UP · Boeing 76734AF · Standard Practices/Structures
  > OPEN (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)
- [SDR IPXA2022072584559](https://openairdocs.org/sdr/IPXA2022072584559.md): Fire Loop · abnormal · Jul 25, 2022 · N371UP · Boeing 76734AF · Smoke Detection
  > INSPECTION TYPE:ETOP** ETOPS FILED OPEN**AT BLOCK IN: "L ENG FIRE LP 2" STATUS MSG ILLUMINATED. L ENG FIRE LP2 DEFERRED 26-11-1-1 CAT C.
- [SDR IPXA2022061183024](https://openairdocs.org/sdr/IPXA2022061183024.md): Floor Panel · damaged · Jun 11, 2022 · N371UP · Boeing 76734AF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1DAMAGE ON MAIN DECK CARGO FLOOR PANEL BETWEEN STA 654+22 - STA 680, AND BETWEEN RBL 54.75 - RBL 77.5FABRICATE REPLACEMENT FLOOR PANEL PER UPS EO NO.:B767-5320-83896-A

## 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 = 'N371UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N371UP/reports

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