# Service difficulty reports: N458UP

A list on [N458UP](https://openairdocs.org/aircraft/N458UP.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 · 215 reports

- [SDR IPXA2026091821733](https://openairdocs.org/sdr/IPXA2026091821733.md): Evas Unit · unsecure · Sep 18, 2026 · N458UP · Boeing 75724APF · Emergency Equipment
  > DURING PREFLIGHT FOUND EVAS CONTAINER NOT SECURED/HANGING TO THE SIDE. PLACED CAPT EVAS UNIT ON DEFERRAL IAW MEL 25-60-1. DMP C/W (UNIT REMOVED SERVICEABLE AND STOWED IN PFM) PLACARD INSTALLED.
- [SDR IPXA2026022092281](https://openairdocs.org/sdr/IPXA2026022092281.md): Seat Track · corroded · Feb 2, 2026 · N458UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > STR--UPON VERIFICATION OF REMOVAD FROZEN BOLT AT FWD SIDE OF SEAT TRACK SECTION IN MAIN CABIN STA 880 LBL 20 FOUND CORROSION--ATA 53 MARKED 007-02 REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALLED REPAI
- [SDR IPXA2026012743275](https://openairdocs.org/sdr/IPXA2026012743275.md): Floor Support · corroded · Jan 23, 2026 · N458UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00 REMOVED DAMAGED FLOOR SUPPORT ANGLE FROM APPROX STA 1715 OUTBOARD L/H SIDE JUST FWD OF AFT PRESSURE BULKHEAD REF. B757-200PF SRM 5
- [SDR IPXA2026012343275](https://openairdocs.org/sdr/IPXA2026012343275.md): Floor Support · corroded · Jan 23, 2026 · N458UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AGING ACFT INSP - FLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00
- [SDR IPXA2026022401372](https://openairdocs.org/sdr/IPXA2026022401372.md): Angle · corroded · Jan 21, 2026 · N458UP · Boeing 75724APF · Horizontal Stabilizer Structure
  > STR, ATA 55: R/H HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS BLOW OUT WITH CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORRODED. RL013 INSTALLED BONDING STRAP P/N BACJ40E20-20 BATCH 0004458634, BONDING BRACKET (ANGLE) AND WEB
- [SDR IPXA2026022402462](https://openairdocs.org/sdr/IPXA2026022402462.md): Angle · corroded · Jan 21, 2026 · N458UP · Boeing 75724APF · Horizontal Stabilizer, Spar/Rib
  > LEFT HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS HAVE CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORRODED. RL029 INSTALLED 1EA ANGLE, 1EA WEB AND 1EA BONDING STRAP AT LH HORIZONTAL STABILIZER STAB STA 360 IAW 757-200PF SRM 5
- [SDR IPXA2026022323794](https://openairdocs.org/sdr/IPXA2026022323794.md): Strap · corroded · Jan 15, 2026 · N458UP · Boeing 75724APF · APU Cowling/Containment
  > CORROSION FOUND ON APU INLET SURROUND STRUCTURE FWD STRAP O/B END. ATA 53,STR INSTALLED 4EA STRAP ANGLES AT APU INLET SURROUND STRUCTURE FWD IAW B757-200PF-SRM 51-40-02-0G-0
- [SDR IPXA2025090211532](https://openairdocs.org/sdr/IPXA2025090211532.md): Hose · failed · Aug 28, 2025 · N458UP · Boeing 75724APF · Hydraulic System, Main
  > LEFT HYD QTY ANNUNCIATED ON FINAL APPROACH. S HORTLY AFTER LT SYS PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED, QRH PROCEDURE AND RETURNED FOR LANDING. QTY DEPLETED BEFORE LT ENG. SERVICING HOSE WAS REPLACED AND LEAKED CHECK IAW AMM 29-18-01. BOTH HOSES
- [SDR IPXA2025082811532](https://openairdocs.org/sdr/IPXA2025082811532.md): Hydraulic System · leaking · Aug 28, 2025 · N458UP · Boeing 75724APF · Hydraulic System, Main
  > EMERGENCY DECLARED, LT HYD QTY (EICAS C) ANNUNCIATED ON FINAL APPROACH. SHORTLY AFTER LEFT SYSTEM PRESSURE WAS LOST, AFTER GO AROUND ACCOMPLISHED QRH PROCEDURE AND RETURNED FOR LANDING. QTY DEPLETED BEFORE L ENG PERFORMED OPS AND LEAK CHECK OF LT ENGINE DRIVE
- [SDR IPXA2025082287433](https://openairdocs.org/sdr/IPXA2025082287433.md): Flap System · malfunctioned · Aug 21, 2025 · N458UP · Boeing 75724APF · Trailing Edge Flap Control System
  > EMERGENCY DECLARED ON APPROACH, WHEN CONFIG., TE FLAP DISAGREE EICAS MSG. FLAPS @ BETWEEN 0 AND 1 REMOVED AND REPLACED RT FLAP TRANSMITTER PER AMM 27-58-03/401. PERFORMED ADJUSTMENT/TEST PER AMM 27-58-01/501. FLAPS/SLATS OPERATE NORMAL. ACFT OK FOR SERVICE.
- [SDR IPXA2025062483756](https://openairdocs.org/sdr/IPXA2025062483756.md): Door · binding · Jun 24, 2025 · N458UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR DIFFICUILT TO UNLOCK PERFORMED ADJUSTMENT OF CREW ENTRY DOOR IAW AMM 52-12-00, OPS CHECK GOOD AT THIS TIME.
- [SDR IPXA2025062552431](https://openairdocs.org/sdr/IPXA2025062552431.md): Attach Bracket · debonded · Jun 11, 2025 · N458UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > F/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE. REPLACED F/O'S EMERGENCY ESCAPE ROPE DOOR REFERENCE IPC 25-14-01-02, ITEM 850 & 705.
- [SDR IPXA2025061152431](https://openairdocs.org/sdr/IPXA2025061152431.md): Attach Bracket · debonded · Jun 11, 2025 · N458UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > F/O'S ESCAPE ROPE DOOR ATTACH BRACKETS DISBONDED FROM PANEL, PANEL IS LOOSE DEFERRED F/OS ESCAPE ROPE DOOR PANEL IAW SREO-84962-REQ001 ACOMPLISHED STEPS TO REMOVE AND STOW PANEL AND INSPECT AREA AND ROPE FOR SECURITY IAW SREO-84962-REQ001
- [SDR IPXA2025042864245](https://openairdocs.org/sdr/IPXA2025042864245.md): Life Vest · missing · Apr 26, 2025 · N458UP · Boeing 75724APF · Life Jacket
  > FO'S LIFE JACKET MISSING. REPLACED FO'S LIFE JACKET IAW AMM 25-64-00/201
- [SDR IPXA2024021912973](https://openairdocs.org/sdr/IPXA2024021912973.md): Tee Angle · corroded · Feb 5, 2024 · N458UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: AFT FUSELAGE, WING TO BODY FAIRING T CHORD SUPPORT AT STA 1220 L/H HAS CORROSION. INSTALLED NEW T-CHORD AT STA 1220 L/H IAW SRM 51-40-02-0G-0. JOB COMPLETE
- [SDR IPXA2024021805797](https://openairdocs.org/sdr/IPXA2024021805797.md): Tee Angle · corroded · Feb 4, 2024 · N458UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT: AFT FUSELAGE WTB FAIRING T CHORD SUPPOR AT STA 1240 R/H HAS CORROSION INSTALLED T-CORD SUPPORT AT STA 1240 R/H IAW B757-200 SRM 51-70-12-0G-0, FIG 1. AUDIT COMPLETE.
- [SDR IPXA2024022889259](https://openairdocs.org/sdr/IPXA2024022889259.md): Support · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED INSTALLED NEW "T" CHORD AT STA 1220 R/H IAW SRM 52-40-02
- [SDR IPXA2024022092776](https://openairdocs.org/sdr/IPXA2024022092776.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > NR 1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. ALL WORK ACCOMPLISHED PER EO EO-89461-REQ AND VT MAE 757-5450-27-A3512 REV.
- [SDR IPXA2024022292675](https://openairdocs.org/sdr/IPXA2024022292675.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT- #2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. WORK ACCOMPLISHED PER UPS EO: EO-89467-REQ 1 AND VTMAE EA 757-5450-27-A3518 REV-
- [SDR IPXA2024022192899](https://openairdocs.org/sdr/IPXA2024022192899.md): Doubler · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR. #2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISHED WORKED PER UPS EO-89493-REQ 1 AND VT MAE EA 757-5450-27-A3519 REV. FAA 8100-9 APPROVAL ATTACHED.
- [SDR IPXA2024021992798](https://openairdocs.org/sdr/IPXA2024021992798.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR, NR 1 ENGINE INBD PYLON INNER SKIN, AFT OF THE SQUARE PANEL HAS EXFOLIATION CORROSION. DOT 8-014. VERIFIED WORKED PER UPS EO: EO 89460-REQ 1 AND VT MAE 757-5450-27-A3511 REV.
- [SDR IPXA2024021992675](https://openairdocs.org/sdr/IPXA2024021992675.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR, NR 2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. OK TO APPLY TOP-COAT APPROVED. OPEN
- [SDR IPXA2024021792899](https://openairdocs.org/sdr/IPXA2024021792899.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > MAJOR REPAIR, NR 2 ENGINE INBD PYLON INNER SKIN UNDER THE CIRCLE PANEL OPENING HAS CORROSION. DOT 8-021. ACCOMPLISH EO-89493-REQ1 AND EA 757-5450-27-A3519. OPEN
- [SDR IPXA2024021789430](https://openairdocs.org/sdr/IPXA2024021789430.md): Tee Angle · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT: WING TO BODY T CHORD SUPPORT STA 1200 R/H HAS CORROSION INSTALLED T CHORD SUPPORT STA 1200 IAW B757-200 SRM 51-40-02 REVIEWED
- [SDR IPXA2024021589259](https://openairdocs.org/sdr/IPXA2024021589259.md): Support · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Aerodynamic Fairings
  > *** SDR FILED OPEN *** FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED AUDIT COMPLETE
- [SDR IPXA2024021592776](https://openairdocs.org/sdr/IPXA2024021592776.md): Skin · corroded · Feb 3, 2024 · N458UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > FAULT- #1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. OK TO INSTALL DOUBLER"INSP ONLY"
- [SDR IPXA2024021773507](https://openairdocs.org/sdr/IPXA2024021773507.md): Frame · dented · Feb 2, 2024 · N458UP · Boeing 75724APF · Fuselage Main, Frame
  > *MAJOR REPAIR* FAULT: DENT FOUND AT AFT CARGO COMPARTMENT FRAME STA 1500 STR 27 R/H WORKED PER PRELIMINARY 1 AND 2 EA 757-5360-27-A3510 REV-. WORKED PER UPS EO: EO-89458-REQ 1. WORKED PER VTMAE EA 757-5360-27-A3510 REV-. FAA 8100-9 APPROVAL ATTACHED.
- [SDR IPXA2024021673097](https://openairdocs.org/sdr/IPXA2024021673097.md): Frame · dented · Feb 2, 2024 · N458UP · Boeing 75724APF · Fuselage Structure (General)
  > DENT FOUND AT AFT CARGO COMPARTMENT, STA 1300 STR 27 R/H INSTALLED REPAIR PARTS IAW B757 EA#:757-5360-27-A3513 AND INSTALLED TIE DOWN AND ANGLE AT STA:1300 IAW SRM 51-40-02. VERIFIED. R/H WORKED PER UPS EO: EO-89459-REQ 1 AND VTMAE EA 757-5360-27-A3513 REV-
- [SDR IPXA2024021960150](https://openairdocs.org/sdr/IPXA2024021960150.md): Tee Angle · corroded · Feb 1, 2024 · N458UP · Boeing 75724APF · Aerodynamic Fairings
  > EVIDENCE OF CORROSION BEHIND PANEL 198LR ON FUSELAGE. INSTALLED T CHORD BEHIND PANEL 189 IAW B757-200 SRM 51-40-02. INSTALLED PANEL 198LR IAW B757-200 SRM 51-40-02. AUDIT COMPLETE.
- [SDR IPXA2022101187064](https://openairdocs.org/sdr/IPXA2022101187064.md): Power Supply · inoperative · Oct 11, 2022 · N458UP · Boeing 75724APF · Emergency Lighting
  > BOTH INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP.REMOVED AND REPLACED BATTERY POWER SUPPLY. MM 33-51-07 AND BATTERY CHARGER. MM 33-51-07. OPS CHECKS GOOD. EFF SOURCE REF: IPC 33-51-11-01-021 CHARGER -33-51-11-01-045S BATTERY SUPPLY
- [SDR IPXA2022021478987](https://openairdocs.org/sdr/IPXA2022021478987.md): None · none · Feb 14, 2022 · N458UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:C-CKAFT CARGO COMPT. HAS EXISTING REPAIR AT STA 1320 I/B OF S-26R.REMOVED EXISTING REPAIR, FABRICATED STRINGER CLIPS AND COLD WORKED HOLES. REPAIRE IAW EA# 757-5360-27-A2810 REV; UPS EO B757-5310-82766-A.
- [SDR IPXA2022021579016](https://openairdocs.org/sdr/IPXA2022021579016.md): Frame · none · Feb 14, 2022 · N458UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG1AFT CARGO COMPTG, FOUND EXISTING FRAME REPAIR AT STA 1560 I/B SODE PF S-26LREPAIRED IAW VT MAE EA#757-5360-27-A2811 REV. UPS EO B757-5310-82763-A
- [SDR IPXA2021120976796](https://openairdocs.org/sdr/IPXA2021120976796.md): First Aid Kit · none · Dec 9, 2021 · N458UP · Boeing 75724APF · Emergency Equipment
  > INSPECTION TYPE:N/ASEAL BROKEN ON FIRST AID KITREPLACED FIRST AID KIT AS REQ PER GMM 08-02
- [SDR IPXA2020111062217](https://openairdocs.org/sdr/IPXA2020111062217.md): Glide Slope · failed · Nov 7, 2020 · N458UP · Boeing 75724APF · Landing and Taxi Aids
  > INSPECTION TYPE: NA DIVERSION, NO EMERGENCY DECLARED. AT 400' ON ILS APPROACH RUNWAY 14 JAX THE FOLLOWING OCCURED. AP DISENGAGED FLIGHT DIRECTOR G/S DEVIATION BAR DISAPPEARED G/S FLAG APPEARED FOR BOTH CAPT & F/O. PERFORMED ILS CHECK, IAW FIM 34-31-00-815-8
- [SDR IPXA2020092260525](https://openairdocs.org/sdr/IPXA2020092260525.md): Actuator · slow · Sep 21, 2020 · N458UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > EMERGENCY DECLARED. GEAR DISAGREE EICAS MSG ON AFTER TAKEOFF WITH GEAR IN UP POSITION. PLACED ON MEL 32-30-1 HGEAR PINS INSTALLED DMP ACCOMPLISHED. PERFORMED GEAR SWING AND FOUND NOSE GEAR SLOW TO RETRACT (26 SECONDS). REPLACED NOSE GEAR ACTUATOR, PER MM 3
- [SDR IPXA2020062435903](https://openairdocs.org/sdr/IPXA2020062435903.md): Sensor · out of adjust · Jun 21, 2020 · N458UP · Boeing 75724APF · Landing Gear Position and Warning
  > INSPECTION TYPE:SV, ATB - AFTER TAKE OFF, AFTER RETRACTION HAD A GEAR DISAGREE LIGHT, THE LANDING GEAR DISAGREE CHECKLIST RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. ADJUSTED THE NLG UP AND DOWN LOCK SENSORS IAW AMM 32-61-03-822-038. PERFORMED LANDIN
- [SDR IPXA2020051555278](https://openairdocs.org/sdr/IPXA2020051555278.md): Light · inoperative · May 13, 2020 · N458UP · Boeing 75724APF · Emergency Lighting
  > INSPECTION TYPE:N/AEMERGENCY LIGHT HAS FOUR INOP BULBSRELAMPED EMERGENCT LIGHT PER AMM 33-51-01-2 FOUR BULBS
- [SDR IPXA2020033053628](https://openairdocs.org/sdr/IPXA2020033053628.md): Slat · delaminated · Mar 11, 2020 · N458UP · Boeing 75724APF · Leading Edge Devices
  > INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2020033053627](https://openairdocs.org/sdr/IPXA2020033053627.md): Slat · delaminated · Mar 11, 2020 · N458UP · Boeing 75724APF · Leading Edge Devices
  > INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2020032753623](https://openairdocs.org/sdr/IPXA2020032753623.md): Slat · delaminated · Mar 11, 2020 · N458UP · Boeing 75724APF · Leading Edge Devices
  > INSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
- [SDR IPXA2019061243113](https://openairdocs.org/sdr/IPXA2019061243113.md): Structure · damaged · Jun 10, 2019 · N458UP · Boeing 75724APF · Rudder Structure
  > RUDDER T/E DMG 26.5 INCHES UP FROM BOTTOM EDGE ON THE L/H SIDE 2.0" ALONG AFT EDGE BY 2.0 FWD/AFT.REPAIRED PER EO B757-5540-72844-A.
- [SDR IPXA2019061243112](https://openairdocs.org/sdr/IPXA2019061243112.md): Structure · damaged · Jun 10, 2019 · N458UP · Boeing 75724APF · Rudder Structure
  > RUDDER T/E DMG 76" UP FROM BOTTOM EDGE. REMOVED DMG IS 1 PLY OF GRAPHITE 1.7" FWD/AFT BY 1.5" UP/DOWN LOCATED ON L/H SIDE.REPAIRED PER EO B757-5540-72844-A.
- [SDR IPXA2019050941939](https://openairdocs.org/sdr/IPXA2019050941939.md): Hydraulic Line · not reported · May 9, 2019 · N458UP · Boeing 75724APF · Hydraulic System, Main
  > INSPECTION TYPE:N/A AIR TURN BACK - LT HYDRAULIC SYSTEM LOSS OF QUANTITY AND PRESSURE. PASSING 8000 FT. LEFT HYD. QTY EICAS FOLLOWED BY L HYD ENG PUMP EICAS AND L HYD SYS PRESS. HYD QTY 0.0 ON STATUS PAGE. ATB ACCOMPLISHED WITH ALTERNATE FLAP EXT AND ALTERNAT
- [SDR IPXA2018032827932](https://openairdocs.org/sdr/IPXA2018032827932.md): Floor Panel · delaminated · Mar 27, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 251XMF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018040328140](https://openairdocs.org/sdr/IPXA2018040328140.md): Panel · delaminated · Mar 18, 2018 · N458UP · Boeing 75724APF · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE: SEG3, WHILE PERFORMING TAP TEST IAW S55-610-100-2, FOUND THREE AREAS OF DELAMINATION ON THE RT VERTICAL STAB LOWER FWD TORQUE BOX PANEL. REMOVED AND REPLACED THE PANEL IAW SRM 51-40-02-OG, AND AMM 51-21-10.
- [SDR IPXA2018032527805](https://openairdocs.org/sdr/IPXA2018032527805.md): Floor Panel · delaminated · Mar 18, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XEF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727899](https://openairdocs.org/sdr/IPXA2018032727899.md): Floor Panel · delaminated · Mar 15, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XFF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727896](https://openairdocs.org/sdr/IPXA2018032727896.md): Floor Panel · delaminated · Mar 15, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032727895](https://openairdocs.org/sdr/IPXA2018032727895.md): Floor Panel · delaminated · Mar 15, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
- [SDR IPXA2018032827929](https://openairdocs.org/sdr/IPXA2018032827929.md): Floor Panel · delaminated · Mar 15, 2018 · N458UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 252XTF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.

Next page: https://openairdocs.org/aircraft/N458UP/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 = 'N458UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N458UP/reports

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