# Service difficulty reports: N469UP

A list on [N469UP](https://openairdocs.org/aircraft/N469UP.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 · 207 reports

- [SDR IPXA2026010883023](https://openairdocs.org/sdr/IPXA2026010883023.md): Control Unit · faulted · Jan 7, 2026 · N469UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > AT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN AREA IS AFFECTED. REMOVED AND INSTALLED L2 WINDOW IAW AMM 56-11-02/401 UP TO AND INCLUDING STEP C.8.
- [SDR IPXA2026010783023](https://openairdocs.org/sdr/IPXA2026010783023.md): Window · delaminated · Jan 7, 2026 · N469UP · Boeing 75724APF · Flight Compartment Windows
  > AT CRUISE FLT AT FL380. L SIDE WINDOW HAD STARTED TO DELAMINATE THE HEATING ELEMENT. FOLLOWED QRH CHECKLIST & WINDOW WAS EXTREMELY HOT TO TOUCH AND APPROX 5IN AREA IS AFFECTED. UPON INSPECTION OF L2 WINDOW, REF AMM 56-11-00-206-068, FOUND BROWN COLORING, GROUP
- [SDR IPXA2025122247034](https://openairdocs.org/sdr/IPXA2025122247034.md): Engine · vibration · Dec 19, 2025 · N469UP · Boeing 75724APF · Engine (Turbine/Turboprop)
  > DIVERSION, NR 2 ENG HIGH N1 VIBRATION ON CLIMB AT 36,000. KEPT OUT OF YELLOW BAND BELOW 67% N1 POWER SETTING. POWERPLANT ENGINEERING REVIEWED ECM/OCM DATA. CLE LINE MAINTENANCE REPORTED THAT ICE WAS FOUND ON THE SPINNER AND FAN BLADES. POWERPLANT ENGINEERING
- [SDR IPXA2025111093190](https://openairdocs.org/sdr/IPXA2025111093190.md): Elec Connector · damaged · Nov 10, 2025 · N469UP · Boeing 75724APF · Air Intake Anti/De-Ice System
  > AIR TURN BACK DUE TO RIGHT ENG TAI INOP LIGHT & EICAS MSG. ENG. A/I CHECKLIST WAS RUN W/NO RELIEF. ICING CONDITIONS AT DESTINATION THIS OCCURRED ON CLIMB-OUT. REPLACED CONNECTOR D1318 FOR ENG ANTI-ICE VALVE IRW B757 SWPM 20-60-03. REVERSED DMP 30-21-1-1. PERF
- [SDR IPXA2025081246933](https://openairdocs.org/sdr/IPXA2025081246933.md): Latch · inoperative · Aug 1, 2025 · N469UP · Boeing 75724APF · Fixed Inner Doors
  > CREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS. INSTALLED CREW ENTRY DOOR UPR LATCH, IAW CMM 52-11-08 AND AMM 20-11-00-912-001.
- [SDR IPXA202508046933](https://openairdocs.org/sdr/IPXA202508046933.md): Latch · out of limits · Aug 1, 2025 · N469UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR UPPER LATCH IS OUT OF LIMITS VERIFIED STEP 6. INSTALLATION OF CREW ENTRY DOOR UPPER LATCH.REMOVED CREW ENTRY DOOR UPPER LATCH, IAW B757-200 AMM 20-11-00-912-001.INSTALLED CREW ENTRY DOOR UPR LATCH, IAW B757-200 CMM 52-11-08 AND AMM 20-11-00-912
- [SDR IPXA2025080310676](https://openairdocs.org/sdr/IPXA2025080310676.md): Frame · cracked · Jul 30, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Frame
  > DURING OK TO INSTALL, FOUND AT STA 1200, BTW RBL 5 TO RBL 24, INTERCOSTAL DELAMINATED AND WITH CRACK. INSTALLED 1 EA INTERCOSTAL IAW SRM 51-40-02-0G.
- [SDR IPXA2025080308094](https://openairdocs.org/sdr/IPXA2025080308094.md): Floorbeam · corroded · Jul 24, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN DECK FLOORBEAM BELOW FLOOR PANEL 242XGF AT BS 1100 RBL 24.75, HAS EXFOLIATED CORROSION, DOT 78-20, FABRICATED 01 EA REPAIR UPPER CHORD SECTION PER E.A.# 757-5340-27-A4084 STEP 8, LETTER A AND B. ACCOMPLISH CATEGORY B REPAIR IN ACCORDANCE WITH EO-94658-REQ
- [SDR IPXA2025080303268](https://openairdocs.org/sdr/IPXA2025080303268.md): Tee Angle · corroded · Jul 24, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AT STA 1040 TO 1060 LEFT, UNDER THE RAM AIR DOOR ACTUATOR, T-CHORD HAS EXFOLITATION CORROSION ON UPPER FLANGE, DOT 8-018.RECEIVED NEW INTERCOSTAL FROM TRAVELER # T25/1825274, BATCH #0004248846. RESTORED SURFACE IN NEW INTERCOSTAL IAW AMM 51-21-15 ALODINE PAI
- [SDR IPXA2025080383490](https://openairdocs.org/sdr/IPXA2025080383490.md): Skin · corroded · Jul 23, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > CORROSION FOUND AT SKIN AREA STA 1885.20 S-17L JUST ABOVE APU LEFT DOOR. PERFORMED EO-94659-REQ1 AND VT-MAE EA 757-5380-27-A4073, REV -.
- [SDR IPXA2025080708252](https://openairdocs.org/sdr/IPXA2025080708252.md): Tee Angle · corroded · Jul 23, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AT STA 1200 LOWER T-CHORD SUUPORT CLIP HAS CORROSION ON INNER FLANGE. DOT 8-015.CLEANED INTRECOSTAL AT STA 1200 NO CORROSION NOTED FOUND TO BE PAINT DAMAGED ONLY IAW B757-200 SOPM 20-30-03 ACETONEQT P/N ACETONEQT BATCH#0004346929 1QT, MAROON HAND PAD P/N 02-00
- [SDR IPXA2025072588319](https://openairdocs.org/sdr/IPXA2025072588319.md): Paint · damaged · Jul 23, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INTRECOSTAL AT BS 1090, RBL 50 HAS SURFACE CORROSION ON INNER SURFACES. CLEANED INTRECOSTAL AT BS 1190, NO CORROSION NOTED FOUND TO BE PAINT DAMAGED ONLY IAW B757-200 SOPM 20-30-03 ACETONEQT P/N ACETONEQT BATCH#0004346929 1QT, MAROON HAND PAD. TREATED AND PRI
- [SDR IPXA2025080560795](https://openairdocs.org/sdr/IPXA2025080560795.md): Skin · corroded · Jul 22, 2025 · N469UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 PYLON INBD SIDE, FWD INNER SKIN HAS CORROSION AROUND CUTOUT OF PANEL 443GL. INSTALLED PYLON #2 I/B FWD FAIRING IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080265076](https://openairdocs.org/sdr/IPXA2025080265076.md): Tee Angle · corroded · Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > TEE CHORD BS 900 RBL 0 HAVE CORROSION. INSTALLED TEE CHORD AND 8 PLATES, IAW SRM 51-70-12-0G-0, SRM 51-40-02.
- [SDR IPXA2025080366377](https://openairdocs.org/sdr/IPXA2025080366377.md): Skin · dented · Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN BETWEEN STA 560 TO 580 AND S-27R TO S-28R HAS A DENT. ACCOMPLISH REPAIR PER EO-94639-REQ1 AND VT-MAE EA 757-5330-27-A4080, REV-.
- [SDR IPXA2025080361106](https://openairdocs.org/sdr/IPXA2025080361106.md): Skin · corroded · Jul 22, 2025 · N469UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON INBD SIDE, AFT INNER SKIN HAS CORROSION BETWEEN PANELS 443HL AND 443JL AT LOWER AREA. ACCOMPLISH REPAIR PER EO-94655-REQ1 AND VT-MAE EA 757-5450-27-A4075, REV-.
- [SDR IPXA2025080706343](https://openairdocs.org/sdr/IPXA2025080706343.md): Support Bracket · corroded · Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > BETWEEN T-CHORD 860 AND LOWER SKIN OF FUSELAGE, LOWER SUPPORT BRACKET HAS CORROSION.REMOVED CORROSION T-CHORD 860 RBL 0 IAW B757-200PF SRM 51-10-02.TREATED AND PRIMED AREA IAW B757-200PF SRM 51-20-01.APPLIED TOP COAT AT AREA IAW B757-200PF AMM 51-21-15-370-801
- [SDR IPXA2025080766917](https://openairdocs.org/sdr/IPXA2025080766917.md): Support Angle · corroded · Jul 22, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE CORROSION PANEL 192 DR UPPER SUPPORT R/H SIDE. CLEANED AREA AT PANEL 192 DR UPPER SUPPORT R/H SIDE IAW SOPM 20-30-03.TREATED AND PRIMED AREA IAW SRM 51-20-01.APPLIED TOP COAT AT AREA IAW AMM 51-21-15-370-801.
- [SDR IPXA2025080234385](https://openairdocs.org/sdr/IPXA2025080234385.md): Strap · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR FWD STRAP AT STA 1787.45 FROM STR 3R TO STR 6R HAS EXFOLIATION. INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025080534561](https://openairdocs.org/sdr/IPXA2025080534561.md): Skin · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > APU INLET DOOR AFT STRAP AT STA 1826 FROM STR 3R TO STR 6R HAS EXFOLIATION CORROSION. ACCOMPLISH REPAIR PER EO-94632-REQ1 AND VT-MAE EA 757-5380-27-A4072, REV-,
- [SDR IPXA2025080234761](https://openairdocs.org/sdr/IPXA2025080234761.md): Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED NEW UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080234656](https://openairdocs.org/sdr/IPXA2025080234656.md): Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1826 AT STR 6R HAS EXFOLIATION CORROSION. INSTALLED 1EA LOWER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025080337337](https://openairdocs.org/sdr/IPXA2025080337337.md): Tee Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON T-CHORD UPPER R/H SECTION STA 1200. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.063''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.5, W:1.4, DEPTH: 0.018'', REMAINING MAT.: 0.045'', %DAMAGE:28.6%. REMOVED UPPER R
- [SDR IPXA2025080700384](https://openairdocs.org/sdr/IPXA2025080700384.md): Stiffener · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON CHANNEL UPPER L/H STA 1120. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.050''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.2, DEPTH: 0.007'', REMAINING MAT.: 0.043'', %DAMAGE:14%. REMOVED STIFFENER STA 1220
- [SDR IPXA2025080237575](https://openairdocs.org/sdr/IPXA2025080237575.md): Tee Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR R/H STA 1220 RBL50..REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.2, W:1.1, DEPTH: 0.020'', REMAINING MAT.: 0.051'', %DAMAGE:28.1%. LOCATED
- [SDR IPXA2025080737989](https://openairdocs.org/sdr/IPXA2025080737989.md): Tee Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON T-CHORD L/H STA 1180 TO 1240 LBL50.DOT 5846-12. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.080''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:1.9, W:1.4, DEPTH: 0.006'', REMAINING MAT.: 0.074'', %DAMAGE:7.5%. TREAT
- [SDR IPXA2025080738248](https://openairdocs.org/sdr/IPXA2025080738248.md): Tee Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON T-CHORD NEAR TO RAM AIR LT STA 1220 LBL50. REMOVED CORROSION ON T-CHORD ORIGINAL MEASURES THICKNESS: 0.071''. AFTER BLENDED FOUND FOLLOWING MEASUREMENTS: L:2.1, W:1.4, DEPTH: 0.031'', REMAINING MAT.: 0.040'' PERCENT, DAMAGE:43.7 PERCE
- [SDR IPXA2025080239097](https://openairdocs.org/sdr/IPXA2025080239097.md): Support Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S3R HAS CORROSION. REMOVED UPPER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED ONE S3R CORNER SUPPORT ANGLE (P/N: 148N3141-6) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SR
- [SDR IPXA2025080239271](https://openairdocs.org/sdr/IPXA2025080239271.md): Angle · corroded · Jul 21, 2025 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER CORNER ANGLE AT BS 1787.45 STR 6R HAS CORROSION.REMOVED LOWER CORNER ANGLE WITH CORROSION IAW B757-200 SRM 51-40-02-0G.REMOVED AND REPLACED 1 EACH S-6R CORNER SUPPORT ANGLE (P/N: 148N3141-5) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200P
- [SDR IPXA2025081314120](https://openairdocs.org/sdr/IPXA2025081314120.md): Cam · damaged · Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR LOWER LATCH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHED JOB IN SREO-14721-REQ001 ((APPX A) CREW ENTRY DOOR UPPER AND LOWER LATCH CAMS REWORK INSTRUCTIONS (SREO))
- [SDR IPXA202507214120](https://openairdocs.org/sdr/IPXA202507214120.md): Cam · gouged · Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR LOWER LATACH CAM HAS A GOUGE ON OUTER SIDE.
- [SDR IPXA2025072113981](https://openairdocs.org/sdr/IPXA2025072113981.md): Cam · gouged · Jul 19, 2025 · N469UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR UPPER LATACH CAM HAS A GOUGE ON OUTER SIDE. ACCOMPLISHMENT OF SREO-14721-REQ001.
- [SDR IPXA2025071153206](https://openairdocs.org/sdr/IPXA2025071153206.md): Indicator · inoperative · Jul 3, 2025 · N469UP · Boeing 75724APF · Fuel Quantity Indicator
  > AIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP REMOVED AND REPLACED ON R/H WING TANK: FUEL PROBES: #1, #2, #3, #4, #5, #7, #8, #9, #10, #11 AND 12, AND PERFORMED LEAK CHECK ON THOSE FUEL ACCESS PANEL, WHERE FUEL PROBES INSTALLED BY A UPS VENDOR. ACCO
- [SDR IPXA2025070753206](https://openairdocs.org/sdr/IPXA2025070753206.md): Indicator · inoperative · Jul 3, 2025 · N469UP · Boeing 75724APF · Fuel Indicating System
  > AIR TURN BACK DUE TO RIGHT SIDE FUEL QTY INDICATION INOP ACCOMPLISHED DRY CAPACITANCE TEST PER AMM 28-41-00-735-080-002.<BR>RM TU 10 AND 11 CAPACITANCES WITHIN LIMITS.
- [SDR IPXA2025040792925](https://openairdocs.org/sdr/IPXA2025040792925.md): Indicator · inoperative · Apr 2, 2025 · N469UP · Boeing 75724APF · Fuel Quantity Indicator
  > **SUPPLEMENTAL SDR** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT. DEFUELED LH MAIN TANK AND PERFORMED FQIS DRY CAPACITANCE TEST PER FIM 28-41 AND FOUND VALUES WITHIN LIMITS. PERFORMED FQIS BITE TEST PER FIM 28-41 AND FOUND NO FAULTS AT TH
- [SDR IPXA2025040792867](https://openairdocs.org/sdr/IPXA2025040792867.md): Indicator · inoperative · Apr 2, 2025 · N469UP · Boeing 75724APF · Fuel Quantity Indicator
  > **SUPPLEMENTAL SDR** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUT TECH SUSPECTED POSSIBLE RH MAIN TANK HARNESS, REFERENCE BARCODE T3F18E006DBEX FOR RH MAIN TANK HARNESS REPLACEMENT. AFTER REPLACEMENT PERFORMED FQIS DRY CAPACITANCE TEST PER FIM 28-41
- [SDR IPXA2025040292925](https://openairdocs.org/sdr/IPXA2025040292925.md): Indicator · inoperative · Apr 2, 2025 · N469UP · Boeing 75724APF · Fuel Quantity Indicator
  > **SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT LEFT MAIN FUEL QTY AND TOTAL FUEL QTY BLANKED OUT.
- [SDR IPXA2025040292867](https://openairdocs.org/sdr/IPXA2025040292867.md): Indicator · failed · Apr 2, 2025 · N469UP · Boeing 75724APF · Fuel Quantity Indicator
  > **SDR FILED OPEN** **DIVERSION** DURING CLIMBOUT RT MAIN FUEL QTY GAUGE BLANKED OUT
- [SDR IPXA2025030526691](https://openairdocs.org/sdr/IPXA2025030526691.md): Light · inoperative · Feb 24, 2025 · N469UP · Boeing 75724APF · Emergency Lighting
  > *SUPPLEMENTAL SDR* INTERIOR EMERGENCY LIGHT INOP ACCOMPLISHED OPS CK OF INTERIOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CK GOOD. THIS CLEARS ITEM. PLACARD REMOVED
- [SDR IPXA2025022426691](https://openairdocs.org/sdr/IPXA2025022426691.md): Light · inoperative · Feb 24, 2025 · N469UP · Boeing 75724APF · Emergency Lighting
  > **SDR FILED OPEN**INTERIOR EMERGENCY LIGHT INOP DEFERRED PER MEL 33-51-1-1. NO DMP, PLACARED INSTALLED.
- [SDR IPXA2024052305539](https://openairdocs.org/sdr/IPXA2024052305539.md): Processor · failed · May 22, 2024 · N469UP · Boeing 75724APF · Fuel Indicating System
  > *** ATB *** ON CLIMB OUT LEFT MAIN TANK FUEL BLANK, INDICATION CAME BACK 90 MINUTES INTO FLIGHT R/R FQIS PROCESSOR IAW AMM 28-41-08. OPS CHECK GOOD.
- [SDR IPXA2024032045317](https://openairdocs.org/sdr/IPXA2024032045317.md): Engine · slow · Mar 14, 2024 · N469UP · Boeing 75724APF · Engine (Turbine/Turboprop)
  > LEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED
- [SDR IPXA2024031545317](https://openairdocs.org/sdr/IPXA2024031545317.md): Governor · slow · Mar 14, 2024 · N469UP · Boeing 75724APF · Turbine Governor
  > LEFT ENGINE SLOW TO SPOOL WHEN POWER PUSHED UP ON TAKEOFF AND IN THE AIR. SLOW ENOUGH TO YAW AIRCRAFT IN THE AIR. ONCE CAUGHT UP ALL PARAMETERS APPEAR NORMAL + MATCH RIGHT ENGINE. REMOVED AND REPLACED LH ENG FUEL FLOW GOVERNOR REF B757 AMM 73-21-01. PERFORMED
- [SDR IPXA2024040259120](https://openairdocs.org/sdr/IPXA2024040259120.md): Panel · damaged · Mar 2, 2024 · N469UP · Boeing 75724APF · Rudder Structure
  > DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DEFERED PER EO-89694 CORRECTIVE ACTION. SPEED TAPE APPLIED TO THE AREA. ITEM CLOSED AND FAULT TRANSFERRED TO BARCODE T3F18E0047VUR FOR REPAIR AND DEADLINE EXTENSION.
- [SDR IPXA2024030459120](https://openairdocs.org/sdr/IPXA2024030459120.md): Hinge · damaged · Mar 2, 2024 · N469UP · Boeing 75724APF · Rudder Structure
  > *SDR FILED OPEN* DAMAGE RUDDER HINGE PANEL VERY MOST TOP PANEL DAMAGED BONDED PANEL REMOVED. WAITING ON NEW PANEL
- [SDR IPXA2023120557614](https://openairdocs.org/sdr/IPXA2023120557614.md): Door Sill · damaged · Nov 18, 2023 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *** SUPPLEMENTAL SDR *** AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. INSTALLLED AFT LWR SILL PLATE AS REQUIRED REF AMM 20-00-00
- [SDR IPXA2023112057614](https://openairdocs.org/sdr/IPXA2023112057614.md): Unknown · unknown · Nov 18, 2023 · N469UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* *MAJOR REPAIR* AFT LOWER CARGO COMP. HAS DAMAGE TO INNER SILL PROTECTOR AND UNDERLYING FITTINGS. REMOVED CLOSEOUT ZEE ANGLE FROM STA 1380 TO STA 1440 TO GAIN ACCESS TO THE TEE CHORD SPLICE REPAIR. REF SRM 51-40-02
- [SDR IPXA61502](https://openairdocs.org/sdr/IPXA61502.md): Unknown · unknown · Sep 15, 2023 · N469UP · Boeing 75724APF · Landing Gear System
  > *SDR FILED OPEN* GEAR DISAGREE EICAS WITH NO RIGHT MAIN GEAR DOWN
- [SDR IPXA2023090693849](https://openairdocs.org/sdr/IPXA2023090693849.md): Skin · cracked · Aug 22, 2023 · N469UP · Boeing 75724APF · Wing, Plate/Skin
  > LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END REPAIR ACCOMPLISHED ON FAULT: T3F18E002792J. INSTALLED REPAIR PARTS I.A.W. B757-200 S.R.M. 51-40-02-OG REVIEWED T3F18E002792J.
- [SDR IPXA202308230001](https://openairdocs.org/sdr/IPXA202308230001.md): Unknown · unknown · Aug 22, 2023 · N469UP · Boeing 75724APF · Wing Structure
  > *** SDR FILED OPEN *** FAULT: LEFT WING FIXED LEADING EDGE HAS CRACK BEHIND SLAT#4 OUTBOARD END

Next page: https://openairdocs.org/aircraft/N469UP/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 = 'N469UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N469UP/reports

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