# Service difficulty reports: N466UP

A list on [N466UP](https://openairdocs.org/aircraft/N466UP.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 4 · 193 reports

- [SDR IPXA2026040311723](https://openairdocs.org/sdr/IPXA2026040311723.md): Overheat Sys · false activation · Apr 2, 2026 · N466UP · Boeing 75724APF · Overheat Detection
  > EMERGENCY DECLARED, EQUIP OVRHT MSG @ FL 390. DID QRH CHECKLIST YET MSG REMAINED. WENT AWAY @ 1200" AGL. ALSO REF 21-58-00-710-802-011 STEP D. AND STEP E. NO OVER HEAT NOTED. INSTALLED FWD AIR FILTER REF AMM 21-58-21-201 OPS CHECK GOOD SEE ATTACHED PICTURE F
- [SDR IPXA2026030541774](https://openairdocs.org/sdr/IPXA2026030541774.md): Adc · inoperative · Mar 5, 2026 · N466UP · Boeing 75724APF · Air Data Computer
  > AIR TURN BACK - UNRELIABLE AIRSPEED DURING CLIMB OUT. R&R L/H ADC, OPS CHECK GOOD IAW 757 AMM 34-12-01. WORK DONE BY CAT QUALIFIED MECHANIC.
- [SDR IPXA2025083196619](https://openairdocs.org/sdr/IPXA2025083196619.md): Floorbeam · corroded · Aug 15, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MDC BETWEEN STA 1100 AND LBL 62 CROSSBEAN WITH CORROSION. ACCOMPLISHED REPAIR PER EO-94866-REQ1 AND VT-MAE 757-5340-27-A4101, REV-.
- [SDR IPXA2025090270617](https://openairdocs.org/sdr/IPXA2025090270617.md): Strap · corroded · Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT, BS 800-820 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION AND (1EA) NUTPLATE LOOSE. STRAP INSTALLED ACCORDING TO IAW SRM 51-40-02. INSTALLED ANGLES (4 EA) ON FWD CARGO COMPT, STA 800-820 CEILING DECOMPRESSION PANEL, IAW B757-200PF, SRM 51-
- [SDR IPXA2025090271962](https://openairdocs.org/sdr/IPXA2025090271962.md): Tee Fitting · corroded · Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LOWER CENTER FUSELAGE, STA 1040-1060 LBL 40, LT PACK EXHAUST SUPPORT INTERCOSTAL TEE FITTING HAS EXFOLIATION. INSTALLED 1 NEW TEE FITTING IAW SRM-51-40-02.
- [SDR IPXA2025082770574](https://openairdocs.org/sdr/IPXA2025082770574.md): Support · corroded · Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FWD CARGO COMPT, BS 580 - 600 CEILING DECOMPRESSION PANEL SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT PANEL IN FWD CARGO COMPT BS 580 - 600 CEILING DECOMPRESSION IAW B757-200 SRM 51-40-02-0G SRM 51-70-13-0G-0.
- [SDR IPXA2025090270230](https://openairdocs.org/sdr/IPXA2025090270230.md): Tee Fitting · corroded · Aug 14, 2025 · N466UP · Boeing 75724APF · Aerodynamic Fairings
  > LEFT AFT BODY FAIRING BS 1220, LBL 65, TEE FITTING HAD CORROSION. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02-0G.
- [SDR IPXA2025090276350](https://openairdocs.org/sdr/IPXA2025090276350.md): Skin · ground damage · Aug 14, 2025 · N466UP · Boeing 75724APF · Wing, Plate/Skin
  > FAULT-COMP-Z500- LH WING, SLAT 4 AREA, FIXED L/E SKIN, BY I/B MAIN TRACK, HAS COMPOSITE BROKEN. INSTALLED NEW PANEL ASSY-UPPER SKIN OTBD FIXED L/E. IAW B757-200PF, SRM 51-40-02. REVIEWED
- [SDR IPXA2025082957732](https://openairdocs.org/sdr/IPXA2025082957732.md): Strap · corroded · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1220 -1240 LBL 40 HAS EXFOLIATION CORROSION. INSTALLED AFT CARGO COMPARTMENT CEILING 153AC IAW B757-200 AMM 25-50-01-404-008.
- [SDR IPXA2025082757796](https://openairdocs.org/sdr/IPXA2025082757796.md): Strap · corroded · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1580 LBL 40 HAS CORROSION. INSTALLED CEILING PANEL 161DC AFT CARGO PIT L/H STA 1520-1600 IAW B757-200 SRM 51-40-02.
- [SDR IPXA2025082857775](https://openairdocs.org/sdr/IPXA2025082857775.md): Strap · corroded · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT CEILING DECOMPRESSION PANEL SUPPORT AT STA 1400-1420 RBL 45 HAS EXFOLIATION CORROSION. INSTALLED CEILING PANEL 154EC IAW B757-200 AMM 25-50-01-404-008.
- [SDR IPXA2025082756968](https://openairdocs.org/sdr/IPXA2025082756968.md): Tee Fitting · corroded · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > FUSELAGE LOWER STA 1260 BL 0 TO RBL 50 TEE FITTING HAS SURFACE CORROSION. INSTALLED TEE FITTING AND ANGLES ON STA 1260 BL 0 TO RBL 50, IAW SRM 51-40-02, SRM 51-70-12-0G-0.
- [SDR IPXA2025082944844](https://openairdocs.org/sdr/IPXA2025082944844.md): Support Bracket · cracked · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RH WW, FWD CUTOUT, STA. APPROX 1060, BRACKET #6 (I/B TO O/B) HAS A CRACK. INSTALLED NEW BRACKET AT RH WW, FWD CUTOUT, STA. APPROX 1060 IAW B757-200PF SRM 51-40-02.
- [SDR IPXA2025082741605](https://openairdocs.org/sdr/IPXA2025082741605.md): Support Channel · cracked · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > RIGHT MLG WW FWD SEAL RETAINER ATTACHMENT FRAME CRACKED AT OTBD END. INSTALLED NEW SUPPORT CHANNEL AT RT MLG WW IAW SRM 51-40-02.
- [SDR IPXA2025082350589](https://openairdocs.org/sdr/IPXA2025082350589.md): Tee Angle · corroded · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > AFT BODY FAIRINGS RH SIDE AT STA 1180 TO 1240 AND RBL 62 T-CHORD EXFOLIATED. INSTALLED T-CHORD FROM STA 1180-1240 R/H IAW B757-200-SRM-51-40-02-OG.
- [SDR IPXA2025082143477](https://openairdocs.org/sdr/IPXA2025082143477.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XBF HAS EDGES DAMAGED. FABRICATION OF PANEL 242XBF IAW MAIN CARGO COMPARTMENT FLOOR PANAL REPLACEMENT (SREO-9692-RE001).
- [SDR IPXA2025082143382](https://openairdocs.org/sdr/IPXA2025082143382.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XDF HAS EDGE ANT EXTERNAL SURFACE DAMAGED. FABRICATION OF PANEL 242XBF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO-9692-REQ001).
- [SDR IPXA2025082143354](https://openairdocs.org/sdr/IPXA2025082143354.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XAF HAS EDGES DAMAGED. FABRICATION OF PANAL 242XAF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO -9692-REQ001).
- [SDR IPXA2025082143295](https://openairdocs.org/sdr/IPXA2025082143295.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XHF INNER SURFACE HAS SPOTS DAMAGED. FABRICATION OF PANEL 242XHF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO-9692-REQ001).
- [SDR IPXA2025082143203](https://openairdocs.org/sdr/IPXA2025082143203.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR PANEL, ACCESS PANEL 242XJF EXTERNAL SURFACE HAS SPOTS DAMAGED IN 4 PLACES. FABRICATION OF PANEL 242XJF IAW MAIN CARGO COMPARTMENT FLOOR PANAL REPLACEMENT..
- [SDR IPXA2025082143158](https://openairdocs.org/sdr/IPXA2025082143158.md): Floor Panel · damaged · Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor Panel
  > MAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XFF HAS EDGE DAMAGE. FABRICATION OF PANEL 242XJF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO-9692-REQ001).
- [SDR IPXA2025090435309](https://openairdocs.org/sdr/IPXA2025090435309.md): Panel · cracked · Aug 12, 2025 · N466UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > NUMBER 2 PYLON VENT PANEL 443CR HAS A CRACK IN UPPER FWD CORNER. ACCOMPLISHED DVI IAW EO B757-5450-82780-A STEP 4(I). FASTENERS ARE IN SERVICEABLE CONDITION.
- [SDR IPXA2025090236564](https://openairdocs.org/sdr/IPXA2025090236564.md): Tee Angle · corroded · Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > BODY FAIRINGS AREA T-COURD AT STA 900 WITH CORROSION. NSTALLED NEW T-CHORD AND SPLICES AT STA 900, IAW B757-200PF SRM 51-70-12-0G-0 PAG 7 FIGURE 1.
- [SDR IPXA2025082226871](https://openairdocs.org/sdr/IPXA2025082226871.md): Skin · corroded · Aug 12, 2025 · N466UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > PYLON NR 1 OTBD AFT INNER SKIN CORROSION BETWEEN PANELS 433BL AND 433CL. ACCOMPLISHED REPAIR PER EO-94789-REQ1 AND VT-MAE EA 757-5450-27-A4098, REV- WITH NO DEVIATIONS.
- [SDR IPXA2025090233389](https://openairdocs.org/sdr/IPXA2025090233389.md): Bracket · corroded · Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > AFT CARGO BULKHEAD LOWER STRUCTURE OF MDC BETWEEN BS 1700 TO 1720 HAVE 5 BRACKETS OF THE NUTPLATE WITH CORROSION. INSTALLED 5EA BRACKETS AT AFT CARGO BULKHEAD LOWER STRUCTURE OF MDC BETWEEN BS 1700 TO 1720 IAW SRM 51-40-02.
- [SDR IPXA2025082337065](https://openairdocs.org/sdr/IPXA2025082337065.md): Tee Fitting · corroded · Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > LEFT LOWER FUSELAGE, STA 1200-1260 LBL 70 T-CHORD HAS (2EA) AREAS WITH DELAMINATION. INSTALLED NEW T-CHORD IN LH LOWER FUSELAGE STA 1200-1260 LBL 70 T-CHORD IAW B757-200 SRM 51-40-02-0G
- [SDR IPXA2025082135811](https://openairdocs.org/sdr/IPXA2025082135811.md): Stiffener · corroded · Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > CORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.
- [SDR IPXA2025090214639](https://openairdocs.org/sdr/IPXA2025090214639.md): Web · corroded · Aug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON WEB LOWER SECTION STA 1180 TO STA 1240 R/H. INSTALLED WEB LOWER SECTION STA 1180 TO STA 1240 R/H IAW B757-200 SRM 51-40-02. FASTENERS INSTALLED.
- [SDR IPXA2025083014616](https://openairdocs.org/sdr/IPXA2025083014616.md): Tee Angle · corroded · Aug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON TEE ANGLE UPPER SECTION STA 1220 RT. INSTALLED TEE ANGLE UPPER BS 1220 RT SIDE UPPER SECTION IAW B757-200 SRM 51-40-02.
- [SDR IPXA2025082315088](https://openairdocs.org/sdr/IPXA2025082315088.md): Tee Fitting · corroded · Aug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON VERTICA LT-CHORD STA 1220 RT. INSTALLED NEW T-CHORD IN STA 1200 R/H IAW B757-200 SRM 51-40-02-0G
- [SDR IPXA2025083098755](https://openairdocs.org/sdr/IPXA2025083098755.md): Angle · corroded · Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER CORNER ANGLE STA 1785.45 STR 6R HAS CORROSION. INSTALLED LOWER CORNER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025083098735](https://openairdocs.org/sdr/IPXA2025083098735.md): Angle · corroded · Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER CORNER ANGLE STA 1785.45 STR 3R HAS CORROSION. INSTALLED UPPER CORNER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025083000877](https://openairdocs.org/sdr/IPXA2025083000877.md): Strap · corroded · Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, APU INLET DOOR AFT STRAP AT STA 1825 HAS EVIDENCE CORROSION. INSTALLED ALL REPAIR PARTS (3EA STRAPS AND 2EA FILLERS), 2 FITTINGS AND 4 ANGLES IAW B757-200PF SRM 51-40-02-0G-0 FOR ACCOMPLISH TO SRM 53-80-15-2R-1 REPAIR 1 DETAIL II.
- [SDR IPXA2025082798800](https://openairdocs.org/sdr/IPXA2025082798800.md): Angle · corroded · Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER ANGLE FROM STA 1785.45 TO STA 1826 AT STR 3R HAS CORROSION. INSTALLED UPPER ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2025090298768](https://openairdocs.org/sdr/IPXA2025090298768.md): Angle · corroded · Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER ANGLE BS 1785.45 TO 1826, S6R HAD CORROSION. INSTALLED LOWER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2025082785917](https://openairdocs.org/sdr/IPXA2025082785917.md): Strap · corroded · Aug 9, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR FWD STRAP AT STA 1787.45 FROM STG 3R TO STG 6R HAS EXFOLIATION, CORROSION. INSTALLED FWD STRAP IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2024071750251](https://openairdocs.org/sdr/IPXA2024071750251.md): Window · leaking · Jul 17, 2024 · N466UP · Boeing 75724APF · Flight Compartment Windows
  > WATER DRIPPING FROM WINDOW INTO 02 MASK BETWEEN L1 AND L2. ADJUSTED THE LINK ARM TO PUSH WINDOW OUTBOARD TO MAKE CONTACT WITH SEAL. REF AMM 56-11-02-825-013.
- [SDR IPXA2024051065942](https://openairdocs.org/sdr/IPXA2024051065942.md): Windshield · leaking · May 8, 2024 · N466UP · Boeing 75724APF · Flight Compartment Windows
  > LOUD SQUEAL FROM L1 WINDOW STARTED AT FL 380 NEAR DAYTONA BEACH. FL 210 6 PSI SQUEAL WENT AWAY. R/R L1 WINDSHIELD ASSY PER AMM 56-11-01.
- [SDR IPXA2023090377830](https://openairdocs.org/sdr/IPXA2023090377830.md): Shear Tie · dented · Aug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting Structure
  > *** MAJOR REPAIR *** FAULT: AFT CARGO PIT STA 1500 AND STR 26 LH - STR 25 LH FRAME HAS A DENT. INSTALLED STRINGER CLIP (2E/A) AT AFT CARGO PIT STA 1500 IAW SRM 53-00-07-2R-5. VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB COMPLETE
- [SDR IPXA2023090298791](https://openairdocs.org/sdr/IPXA2023090298791.md): Shear Tie · dented · Aug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Structure (General)
  > *** MAJOR REPAIR *** FAULT: AFT CARGO COMPT, FRAME, STA 1580 R/H, AT S-26R HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R. VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB
- [SDR IPXA2023083177842](https://openairdocs.org/sdr/IPXA2023083177842.md): Shear Tie · dented · Aug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting Structure
  > AFT CARGO PIT STA 1500 AND STR 26 RH FRAME HAS A DENT. ACCOMPLISHED REINFORCING ANGLE REPAIR IAW PER 757-200PF SRM REV 117.00 CHAPTER 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R. VERIFIED FINAL INSTALLATION OF FRAME REPAIR. JOB COMPLETE
- [SDR IPXA2023083177808](https://openairdocs.org/sdr/IPXA2023083177808.md): Frame · dented · Aug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Main, Frame
  > AFT CARGO PIT STA 1480 AND STR 26 LH FRAME HAS A DENT VERIFIED FINAL INSTALLATION OF FRAME REPAIR.JOB COMPLETE. IAW B757-200PF REV 117.00 SRM 53-00-07-2R-5, TABLE #3, FOR ZONE #1. MAJOR REPAIR.
- [SDR IPXA2023090760281](https://openairdocs.org/sdr/IPXA2023090760281.md): Stringer · corroded · Aug 20, 2023 · N466UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR. LOWER FUSELAGE SKIN AT STA.1440, STRINGER 29L HAS A BULDGE BETWEEN STRINGER ATTACH RIVETS. DOT 8-001. APPLIED CIC AT NEW STRINGER I.A.W. AMM 51-00-59. VERIFIED ALL WORK COMPLETE.
- [SDR IPXA2023090660307](https://openairdocs.org/sdr/IPXA2023090660307.md): Shear Tie · corroded · Aug 20, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting Structure
  > FAULT- AFT FUSELAGE SKIN BETWEEN STA. 1680-1700, S-27L HAS BULDGING BETWEEN TWO STRINGER RIVETS. DOT 8-002. VERIFIED JOB COMPLETE.
- [SDR IPXA2022042881548](https://openairdocs.org/sdr/IPXA2022042881548.md): Bracket · broken · Apr 28, 2022 · N466UP · Boeing 75724APF · Passenger/Crew Doors
  > L1 DOOR PROXIMITY SENSOR SUPPORT BRACKET BROKEN OFF. (DAMAGED BY LOADING).SECURED PROX SENSOR PER EO B757-5210-83581-A. LINK TO M779933. CREW ENTRY DOOR INDICATION SYSTEM OPS CHECKED GOOD IAW AMM 52-71-1.
- [SDR IPXA2021092974395](https://openairdocs.org/sdr/IPXA2021092974395.md): Skin · none · Sep 29, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:SEG4#2 ENGINE PYLON. OUTBD INTERNAL STRUCTURE HAS BULDGING CORRISION.SKIN REPLACED IAW SRM 51-40-02-0G.
- [SDR IPXA2021092974396](https://openairdocs.org/sdr/IPXA2021092974396.md): Floorbeam · corroded · Sep 29, 2021 · N466UP · Boeing 75724APF · Standard Practices/Structures
  > INSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 45.5 STA 1200 SHOWING SIGNS OF CORROSION.REPAIR PER EA# 757-5360-27-A2671 REV-.
- [SDR IPXA2021092574274](https://openairdocs.org/sdr/IPXA2021092574274.md): Skin · corroded · Sep 25, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG4#2 ENGINE PYLON, INBD SKIN, INTERIOR, AT APPROX. NAC STA 169.8 INBD SIDE HAS CORROSIONAFTER REMOVED CORROSION IN THE AREA FOUND TO BE IN LIMITS PER SRM 54-50-01 FIG 01 SHEET 4 DETAIL V
- [SDR IPXA2021092474227](https://openairdocs.org/sdr/IPXA2021092474227.md): Skin · corroded · Sep 24, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:SEG4#1 ENGINE INBD PYLON FRAME FOR DOOR PANEL 433GR HAS CORROSION ON INSIDE LOWERREMOVE AND REPLACE SKIN
- [SDR IPXA2021092374183](https://openairdocs.org/sdr/IPXA2021092374183.md): Floorbeam · corroded · Sep 23, 2021 · N466UP · Boeing 75724APF · Standard Practices/Structures
  > INSPECTION TYPE:SEG4MAIN CABIN FLOOR BEAM BETWEEN 24.75 RBL - 24.75 LBL STA 110 SHOWING SIGNS OF CORROSIONREPAIRED PER EA# 757-5340-27-A2673 REV-

Next page: https://openairdocs.org/aircraft/N466UP/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 = 'N466UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N466UP/reports

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