# Service difficulty reports: N459UP

A list on [N459UP](https://openairdocs.org/aircraft/N459UP.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 · 266 reports

- [SDR IPXA2026072758829](https://openairdocs.org/sdr/IPXA2026072758829.md): Engine · failed · Jul 25, 2026 · N459UP · Boeing 75724APF · Engine (Turbine/Turboprop)
  > EMERGENCY DECLARED, IN FLIGHT SHUT DOWN DURING CLIMB THRU FL220, LTT ENG FAILED WITHOUT WARNING. AIRSPEED WAS APPROX 310 KTS. N2 ROTATION NORMAL AFTER SHUTDOWN. NO OTHER PROBLEMS THROUGHOUT FLIGHT ATTEMPTED TO START THE NR 1 ENGINE. ENGINE OIL PRESSURE INDICA
- [SDR IPXA2025112636097](https://openairdocs.org/sdr/IPXA2025112636097.md): Flap System · inoperative · Nov 25, 2025 · N459UP · Boeing 75724APF · Trailing Edge Flap Control System
  > TE FLAPS DISAGREE POSITIONING FLAPS 1 ON LANDING C/W FIM 27-51 FT 814. MSG CLEARED NO FUALTS NOTED. OPS CK REF AMM 27-51-00. NO MSG. OK TO CONTINUE.
- [SDR IPXA2025103173256](https://openairdocs.org/sdr/IPXA2025103173256.md): Stringer · corroded · Oct 9, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > WHILE WORKING CORROSION AT AFT CARGO COMP. FOUND CORROSION BETWEEN STRINGER 29R AND FUSELAGE SKIN AT STA 1560-1580. INSTALLED (1EA) REPAIR STRINGER SECTION AND (1EA) FILLER AT LOWER FUSELAGE SKIN BEWTEEN STA 1560-1580 AND STGR-29R I.A.W. B757-200PF SRM 53-00-0
- [SDR IPXA2025102833199](https://openairdocs.org/sdr/IPXA2025102833199.md): Floor Support · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO BELOW ACCESS PANEL 241XHF HAS CORROSION, FLL-026, INSTALLED FLOOR SUPPORT 144N5005-3 UNDER FLOOR PANEL 241XHF IAW SRM 51-40-02-OG-0.
- [SDR IPXA2025103131819](https://openairdocs.org/sdr/IPXA2025103131819.md): Strap · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 252XFF FROM STA 1400 TO STA 1420, RBL 45.5 HAS CORROSION ON SUPPORT CEILING PANEL, FLL-012, ATA 53. NSTALLED 1EA CAPSTRIP ONTO FABRICATED STABILIZER STRAP BELOW ACCESS PANEL 252XFF BETWEEN STA 1400 AND STA 1420 R
- [SDR IPXA2025102930140](https://openairdocs.org/sdr/IPXA2025102930140.md): Angle · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STRUCTURES, MAIN DECK CARGO AFT SHEAR WEB, FROM STA 1681 TO 1720, LBL 54.9 TO RBL 54.9 UNDER METALLIC FLOOR (ACCESS BY CARGO BAY) HAS CORROSION, FLL-005, ATA 53. LOCATED AND DRILLED FABRICATED ANGLE 146N5221-5SAAU IAW B757-200PF SRM 51-40-05-OG-0. OK TO INSTAL
- [SDR IPXA2025103132465](https://openairdocs.org/sdr/IPXA2025103132465.md): Strap · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 251XBF FROM STA 1220 TO STA 1240, LBL 24.75 HAS CORROSION, FLL-018, ATA 53. FABRICATED STABILIZER STRAP MAIN CABIN PANEL 251XBF IAW 757-200 SRM 53-60-51/BAC1493/SAMPLE REVIEWED
- [SDR IPXA2025103034768](https://openairdocs.org/sdr/IPXA2025103034768.md): Structure · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Structure
  > MAIN DECK CABIN BELOW FLOOR PANEL 241XKF HAS CORROSION, FLL-023, ATA 53. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95488-REQ1 AND VT-SAA EA 757-5310-01-B0583, REV IR.
- [SDR IPXA2025102633251](https://openairdocs.org/sdr/IPXA2025102633251.md): Seat Track · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK CARGO BELOW ACCESS PANEL 242XGF SEAT TRACK HAS CORROSION, FLL-028. OPEN
- [SDR IPXA2025102133199](https://openairdocs.org/sdr/IPXA2025102133199.md): Floor Support · corroded · Oct 7, 2025 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > STRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 241XHF HAS CORROSION, FLL-026, ATA 53.
- [SDR IPXA2025102198394](https://openairdocs.org/sdr/IPXA2025102198394.md): Strap · corroded · Oct 5, 2025 · N459UP · Boeing 75724APF · APU Cowling/Containment
  > APU INLET DOOR SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. INSTALLED 4EA NEW REPAIR PARTS, DOUBLER (-1), STRAP (-2), FILLER (-3), FILLER (-4), 1 EA EXISITING OUTER STRAP AND APPLIED FILET SEAL AT APU INLET DOOR SUPPORT STRUCTURE, AFT SIDE, STA. 1825
- [SDR IPXA2025103160829](https://openairdocs.org/sdr/IPXA2025103160829.md): Stringer · corroded · Oct 2, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > STRUCTURES, AFT LOWER FUSELAGE FROM STA 1480 TO STA 1500, S-30, HAS PROTUBERANT DENT, FLL-018, ATA 53. INSTALLED FABRICATED STRINGER SECTION, NEW HAT SECTION AND REINSTALLED SPLICE AT STGR-30. IAW B757-200PF SRM 53-00-03-2R-1 REPAIR 1 AND SRM 51-40-02-0G-0..
- [SDR IPXA2025103060968](https://openairdocs.org/sdr/IPXA2025103060968.md): Skin · corroded · Oct 2, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE FROM STA 1480 TO STA 1500, S-27R TO S-28R, HAS PROTUBERANT DENT, FLL-018, ATA 53. REINSTALLED RH FLOOR PANEL AT AFT CARGO COMP STA 1440 TO STA 1520 IAW B757-200PF SRM 51-40-02-0G-0. ACCOMPLISHED REPAIR PER B757-200PF SRM 53-00-03-2R REPAIR 1
- [SDR IPXA2025102661012](https://openairdocs.org/sdr/IPXA2025102661012.md): Skin · corroded · Oct 2, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE FROM BS 1560 - 1580, S29R, HAS PROTRUDING DENT, FLL-018, ACCOMPLISH REPAIR PER SRM 53-00-01-2R REPAIR 28 REV. 124 REQUIREMENTS.
- [SDR IPXA2025102254371](https://openairdocs.org/sdr/IPXA2025102254371.md): Strap · corroded · Oct 2, 2025 · N459UP · Boeing 75724APF · Fuselage Main, Structure
  > TAILCONE. APU INLET DOOR CUTOUT HAS CORROSION ON THE FWD EDGE.REMOVED FWD STRAP LOWER MIDDLE ANGLE AND FWD LOWER ANGLE AT APU INLET DOOR STRUCTURE IAW SRM 51-40-02-0G-0. SEVERE CORROSION ON REMOVED PARTS FWD STRAP PN, UPPER MIDDLE ANGLE, UPPER FWD ANGLE LOWER
- [SDR IPXA2025051420889](https://openairdocs.org/sdr/IPXA2025051420889.md): Evas Unit · failed · May 11, 2025 · N459UP · Boeing 75724APF · Emergency Equipment
  > CAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00
- [SDR IPXA2025051220889](https://openairdocs.org/sdr/IPXA2025051220889.md): Evas Unit · no test · May 11, 2025 · N459UP · Boeing 75724APF · Emergency Equipment
  > CAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00.
- [SDR IPXA2024123020240](https://openairdocs.org/sdr/IPXA2024123020240.md): Landing Gear · warning message · Dec 27, 2024 · N459UP · Boeing 75724APF · Landing Gear Position and Warning
  > AFTER SELECTING GEAR DOWN THE GEAR DISAGREE MSG ILLUMINATED. PERFORMED QRH AND LANDED NORMALLY. IT WAS THE RIGHT MAIN GEAR THAT DID NOT EXTEND USING NORMAL METHOD. RH GEAR TILT ACTUATOR HYD PRESSURE LINE REPLACED ON BARCODE T3F18E005U09V. CW WITH GEAR SWING NU
- [SDR IPXA202412270001](https://openairdocs.org/sdr/IPXA202412270001.md): Landing Gear · faulted · Dec 27, 2024 · N459UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > AFTER SELECTING GEAR DOWN THE GEAR DISAGREE MSG ILLUMINATED. PERFORMED QRH AND LANDED NORMALLY. IT WAS THE RIGHT MAIN GEAR THAT DID NOT EXTEND USING NORMAL METHOD.
- [SDR IPXA2024092433591](https://openairdocs.org/sdr/IPXA2024092433591.md): Window · warning message · Sep 11, 2024 · N459UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > ON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED. FINISHED REMOVAL OF L/H #2 WINDOW IAW B757 AMM 56-11-02-004-010. INSTALLED L/H #2 WINDOW IAW B757 AMM 56-11-02-404-020. OPS AND LEAK CHECK PASS. DMP REVERSED. THIS CLEARS 2823959. INSTALLATION AND OPS CK OF L
- [SDR IPXA2024091133591](https://openairdocs.org/sdr/IPXA2024091133591.md): Warning Message · illuminated · Sep 11, 2024 · N459UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > SDR FILED OPEN, ON PREFLIGHT L SIDE WINDOW EICAS MESSAGE DISPLAYED STARTED REMOVAL OF #2 WINDOW IAW B757 AMM 56-11-02-004-010 UP TO STEP 5(G) 2).
- [SDR IPXA2023120134182](https://openairdocs.org/sdr/IPXA2023120134182.md): Relief Valve · malfunctioned · Nov 30, 2023 · N459UP · Boeing 75724APF · Cabin Pressure Control System
  > AT 37000FT CABIN ALT AUTO 2 CABIN ALT AUTO 1 MASTER WARNING CABIN AUTO INOP ALL APPEARED. UNABLE TO CONTROL CABIN INITIATED DECENT MANUAL CONTROL BECAME EFFECTIVE BELOW 24000 CONTINUED DECENT TO 10000 FOUND LOWER POSITIVE PRESSURE RELIEF VALVE UNSEATED AND DEB
- [SDR IPXA2023112859902](https://openairdocs.org/sdr/IPXA2023112859902.md): Strake · corroded · Nov 12, 2023 · N459UP · Boeing 75724APF · Horizontal Stabilizer Structure
  > FAULT: LH HORIZONTAL LOWER STRAKELET HAS EVIDENCE OF CORROISON DOT: 107-002. INTALLED STRAKAKELET IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023120543755](https://openairdocs.org/sdr/IPXA2023120543755.md): Tee Angle · corroded · Nov 11, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *** SUPPLEMENTAL SDR *** FAULT: R/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. FAULT WROTE UP FOR OTHER A/C, PLEASE REFER TO T3F18E00CTLT
- [SDR IPXA2023120543694](https://openairdocs.org/sdr/IPXA2023120543694.md): Tee Angle · corroded · Nov 11, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. FAULT CREATED FOR OTHER A/C (N456UP), PLEASE REFER TO T3F18E003CTKV
- [SDR IPXA2023120543467](https://openairdocs.org/sdr/IPXA2023120543467.md): Tee Angle · corroded · Nov 11, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > *** SUPPLEMENTAL SDR *** FAULT: R/H WTB, T-CHORD, STA 1240, FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 T0 RBL 63 FAULT WRITTEN FOR WRONG AIRCRAFT (N456UP), PLEASE SEE T3F18E003CTKR
- [SDR IPXA2023111343755](https://openairdocs.org/sdr/IPXA2023111343755.md): Unknown · unknown · Nov 11, 2023 · N459UP · Boeing 75724APF · Aerodynamic Fairings
  > R/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD STA 1220 IAW SRM 51-40-02-0G. VERIFIED T-CHORD AT STA. 1220 REMOVED.
- [SDR IPXA2023111343694](https://openairdocs.org/sdr/IPXA2023111343694.md): Unknown · unknown · Nov 11, 2023 · N459UP · Boeing 75724APF · Aerodynamic Fairings
  > *** SDR FILED OPEN *** FAULT: R/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. REMOVED T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G. REMOVED STRAP FROM T-CHORD AT RBL 63.0 BETWEEN FS 1180 TO FS 1240 IAW B757 SRM 51-40-02-0G APPR
- [SDR IPXA2023111343467](https://openairdocs.org/sdr/IPXA2023111343467.md): Unknown · unknown · Nov 11, 2023 · N459UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > R/H WTB, T-CHORD, STA 1240, FOUND EXFOLIATED CORROSION, BETWEEN RBL 57.50 T0 RBL 63 PERFORMED CUT OUT AT T-CHORD FROM BL0 TO RBL63 STA 1240 I.A.W SRM 51-70-12-OG AND SRM 51-10-02. VERIFIED T-CHORD AT STA 1240 FROM BL-0 TO RBL-63 HAS BEEN CUT OUT.
- [SDR IPXA2023112740899](https://openairdocs.org/sdr/IPXA2023112740899.md): Skin · corroded · Nov 10, 2023 · N459UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > *MAJOR REPAIR* FAULT: EVIDENCE OF CORROSION INSIDE #2 PYLON SKIN FWD OF PANEL 443CR. DOT 140-13. ACCOMPLISH EO-88765-REQ1 AND EA 757-5450-27-A3442. SUBTASK UP TO REP REVIEW, JOB COMPLETE, AUDIT COMPLETE. REVIEWED.
- [SDR IPXA2023112533548](https://openairdocs.org/sdr/IPXA2023112533548.md): Tee Angle · corroded · Nov 10, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT:LOWER FUSELAGE WEBS BETWEEN BOTH AIR CONDITIONING ACCESS DOOR WITH SURFACE CORROSION.DOT119-065. INSTALLED T-CHORD IN LOWER FUSELAGE BTWN BOTH AIR CONDITIONING IAW SRM 51-40-02-0G.- JOB COMPLETED.
- [SDR IPXA2023112718179](https://openairdocs.org/sdr/IPXA2023112718179.md): Tee Angle · corroded · Nov 9, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT:WING TO BODY LH STRUCTURE HAS CORROSION AT T CHORD STA 1.040.DOT119-060. INSTALLED NEW T-CHORD IN WING TO BODY LH STRUCTURE STA.1040 IAW SRM 51-40-02-0G.- REVIEWED
- [SDR IPXA2023112316833](https://openairdocs.org/sdr/IPXA2023112316833.md): Web · corroded · Nov 9, 2023 · N459UP · Boeing 75724APF · Aerodynamic Fairings
  > FAULT:WING TO BODY FAIRING STA 1.200 WEB RH HAS CORROSION.DOT119-048. INSTALLED NEW WEB AT STA 1200 RH WTB IAW SRM 51-40-02-0G. REVIEWED.
- [SDR IPXA2023112989044](https://openairdocs.org/sdr/IPXA2023112989044.md): Tee Angle · corroded · Nov 8, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: L/H WTB T-CHORD AT STA. 1200 HAS EXFOLIATING CORROSION. INSTALLED NEW T-CHORD AT FS 1200 LH IAW B757 SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023112867666](https://openairdocs.org/sdr/IPXA2023112867666.md): Tee Angle · corroded · Nov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: R/H WTB T-CHORD STA 1037, FOUND EXFOLIATED CORROSION AT NUT PLATE HOLES. INSTALLED T-CHORD AT STA 1037RH WTB IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023112767770](https://openairdocs.org/sdr/IPXA2023112767770.md): Tee Angle · corroded · Nov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: R/H WTB, INTERCOSTAL, FOUND EXFOLIATE CORROSION, BETWEEN STA 1037 TO STA 1060. INSTALLED T-CHORD IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023111967834](https://openairdocs.org/sdr/IPXA2023111967834.md): Tee Angle · corroded · Nov 7, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > R/H WTB, T-CHORD STA 1220, AT RBL 63 FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2025022649962](https://openairdocs.org/sdr/IPXA2025022649962.md): Skin · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge Flaps
  > WING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PLEASE REF BARCODE T3F18E0039JV1 FOR CORRECTIVE ACTION AND INSTALLATION OF NEW FLAP.
- [SDR IPXA2025022651282](https://openairdocs.org/sdr/IPXA2025022651282.md): Skin · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge Flaps
  > WING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 INSTALLED RH IB TRAILING EDGE MAIN FLAP PER AMM 27-51-02-424-021. COMPLETED INSTALLATION AS OUTLINED IN AMM 27-51-12.
- [SDR IPXA2023112049962](https://openairdocs.org/sdr/IPXA2023112049962.md): Skin · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge Flaps
  > *SDR FILED OPEN* FAULT:WING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PARTS ON ORDER IN BARCODE T3F18E0039JV1. 3 MECHANICS REQUIRED FOR 4 SHIFTS ESTIMATED, CRANE REQUIRED, HANGER RECOMMENDED. WORK WITH BARCODE T2F18E0039JV1.
- [SDR IPXA2023112051282](https://openairdocs.org/sdr/IPXA2023112051282.md): Skin · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Trailing Edge Flaps
  > *SDR FILED OPEN* FAULT:WING RH I/B TRAILING EDGE FLAP SURFACE CORROSION AT LOWER SKIN. DOT119-031 PARTS ON ORDER. 3 MECHANICS REQUIRED FOR 4 SHIFTS ESTIMATED, CRANE REQUIRED, HANGER RECOMMENDED. WORK WITH BARCODE T2F18E0039HSE.
- [SDR IPXA2023112865059](https://openairdocs.org/sdr/IPXA2023112865059.md): Tee Angle · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: R/H WTB T-CHORD, RBL 57.50, FOUND EXFOLIATED CORROSION, BET STA 1180 TO STA 1240. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
- [SDR IPXA2023112759219](https://openairdocs.org/sdr/IPXA2023112759219.md): Tee Angle · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: LH AFT WTB STRUCTURE T-CHORD AT STA 1220, UNDER PANEL 195CL HAS CORROSION. INSTALLED NUT PLATE 17 E/A IAW SRM 51-40-02-0G. INSTALLED T-CHORD AT STA 1220 UNDER PANEL 145CL IAW SRM 51-40-02-0G.- REVIEWED
- [SDR IPXA2023112758827](https://openairdocs.org/sdr/IPXA2023112758827.md): Unknown · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Structure (General)
  > FAULT: WTB STRUCTURE UNDER PANEL 198MR, FROM STA 1180-1240 ON TH RH SIDE HAS SEVERAL AREAS WITH CORROSION. INSTALLED T-CHORD UNDER PANEL 198MRFROM STA.1180 TO 1240 ON THE RH SIDE IAW SRM 51-40-02-0G.- REVIEWED
- [SDR IPXA2023112265202](https://openairdocs.org/sdr/IPXA2023112265202.md): Tee Angle · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FULT: R/H WTB T-CHORD STA 1240, FOUND EXFOLIATED CORROSION, BET RBL 57.50 TO RBL 63.0 INSTALLED T-CHORD I.A.W. SRM 51-40-02-0G. INSTALLED 4 E/A SPLICES AT R/H WTB T-CHORD STA 1240 I.A.W. SRM 51-40-02-0G. JOB COMPLETED
- [SDR IPXA2023111958867](https://openairdocs.org/sdr/IPXA2023111958867.md): Tee Angle · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: RH WTB STRUCTURE UNDER PANEL 198AR, STA 1040-1060 HAS CORROSION. INSTALLED T- CHORD STA. 1040 TO STA.1060 IAW SRM 51-40-02-0G. REVIEWED
- [SDR IPXA2023111959108](https://openairdocs.org/sdr/IPXA2023111959108.md): Tee Angle · corroded · Nov 6, 2023 · N459UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: RH WTB STRUCTURE T-CHORD AT STA 1060 HAS CORROSION. INSTALLED T-CHORD I.A.W. B757-200 S.R.M. 51-40-02-OG. REVIEWED
- [SDR IPXA2023120535508](https://openairdocs.org/sdr/IPXA2023120535508.md): Floor Panel · broken · Nov 4, 2023 · N459UP · Boeing 75724APF · Fuselage Floor Panel
  > MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 INSTALLED FLOOR PANEL 232XVF I.A.W. AMM 53-01-024-023.
- [SDR IPXA2023112732706](https://openairdocs.org/sdr/IPXA2023112732706.md): Skin Panel · dented · Nov 4, 2023 · N459UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > *MAJOR REPAIR* FAULT:#2 PYLON I/B HAS DENT AT OUTTER SKIN BETWEEN NAC STA 105.66 AND NAC STA 169.8. DOT119-009. ACCOMPLISH EO-88785-REQ1 AND EA 757-5450-27-A3452. JOB COMPLETED. REVIEWED
- [SDR IPXA2023111735508](https://openairdocs.org/sdr/IPXA2023111735508.md): Floor Panel · broken · Nov 4, 2023 · N459UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT:MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 VERIFIED INSTALLATION OF FLOOR PANEL 232XVF

Next page: https://openairdocs.org/aircraft/N459UP/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 = 'N459UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N459UP/reports

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