N466UP

Service difficulty reports · 193

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026040311723Overheat Sys · false activationEMERGENCY 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 FApr 2, 2026 · N466UP · Boeing 75724APF · Overheat DetectionSDR IPXA2026030541774Adc · inoperativeAIR 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.Mar 5, 2026 · N466UP · Boeing 75724APF · Air Data ComputerSDR IPXA2025083196619Floorbeam · corrodedMDC BETWEEN STA 1100 AND LBL 62 CROSSBEAN WITH CORROSION. ACCOMPLISHED REPAIR PER EO-94866-REQ1 AND VT-MAE 757-5340-27-A4101, REV-.Aug 15, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2025090270617Strap · corrodedFWD 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-Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025090271962Tee Fitting · corrodedLOWER 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.Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082770574Support · corrodedFWD 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.Aug 14, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025090270230Tee Fitting · corrodedLEFT AFT BODY FAIRING BS 1220, LBL 65, TEE FITTING HAD CORROSION. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02-0G.Aug 14, 2025 · N466UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2025090276350Skin · ground damageFAULT-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. REVIEWEDAug 14, 2025 · N466UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2025082957732Strap · corrodedAFT 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082757796Strap · corrodedAFT 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082857775Strap · corrodedAFT 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082756968Tee Fitting · corrodedFUSELAGE 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025082944844Support Bracket · crackedRH 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082741605Support Channel · crackedRIGHT MLG WW FWD SEAL RETAINER ATTACHMENT FRAME CRACKED AT OTBD END. INSTALLED NEW SUPPORT CHANNEL AT RT MLG WW IAW SRM 51-40-02.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082350589Tee Angle · corrodedAFT 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.Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2025082143477Floor Panel · damagedMAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XBF HAS EDGES DAMAGED. FABRICATION OF PANEL 242XBF IAW MAIN CARGO COMPARTMENT FLOOR PANAL REPLACEMENT (SREO-9692-RE001).Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025082143382Floor Panel · damagedMAJOR 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).Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025082143354Floor Panel · damagedMAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XAF HAS EDGES DAMAGED. FABRICATION OF PANAL 242XAF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO -9692-REQ001).Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025082143295Floor Panel · damagedMAJOR 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).Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025082143203Floor Panel · damagedMAJOR 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..Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025082143158Floor Panel · damagedMAJOR REPAIR, MDC FLOOR, ACCESS PANEL 242XFF HAS EDGE DAMAGE. FABRICATION OF PANEL 242XJF IAW MAIN CARGO COMPARTMENT FLOOR PANEL REPLACEMENT (SREO-9692-REQ001).Aug 13, 2025 · N466UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2025090435309Panel · crackedNUMBER 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.Aug 12, 2025 · N466UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2025090236564Tee Angle · corrodedBODY 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.Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082226871Skin · corrodedPYLON 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.Aug 12, 2025 · N466UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2025090233389Bracket · corrodedAFT 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.Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082337065Tee Fitting · corrodedLEFT 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 51-40-02-0GAug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082135811Stiffener · corrodedCORROSION BETWEEN BS 1120 - 1140, LT CHANNEL UNDER PANEL 197EL. INSTALLED A NEW STIFFENER BETWEEN BS 1120-1140 LEFT.Aug 12, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025090214639Web · corrodedEVIDENCE 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.Aug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025083014616Tee Angle · corrodedEVIDENCE 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.Aug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082315088Tee Fitting · corrodedEVIDENCE OF CORROSION ON VERTICA LT-CHORD STA 1220 RT. INSTALLED NEW T-CHORD IN STA 1200 R/H IAW B757-200 SRM 51-40-02-0GAug 11, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025083098755Angle · corrodedAPU INLET DOOR LOWER CORNER ANGLE STA 1785.45 STR 6R HAS CORROSION. INSTALLED LOWER CORNER ANGLE IAW SRM 51-40-02-0G-0.Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025083098735Angle · corrodedAPU INLET DOOR UPPER CORNER ANGLE STA 1785.45 STR 3R HAS CORROSION. INSTALLED UPPER CORNER ANGLE IAW SRM 51-40-02-0G-0.Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025083000877Strap · corrodedMAJOR 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.Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082798800Angle · corrodedAPU 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.Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025090298768Angle · corrodedAPU INLET DOOR LOWER ANGLE BS 1785.45 TO 1826, S6R HAD CORROSION. INSTALLED LOWER ANGLE IAW SRM 51-40-02-0G-0.Aug 10, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025082785917Strap · corrodedAPU 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.Aug 9, 2025 · N466UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024071750251Window · leakingWATER 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.Jul 17, 2024 · N466UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2024051065942Windshield · leakingLOUD 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.May 8, 2024 · N466UP · Boeing 75724APF · Flight Compartment WindowsSDR IPXA2023090377830Shear Tie · dented*** 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 COMPLETEAug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2023090298791Shear Tie · dented*** 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.JOBAug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Structure (General)SDR IPXA2023083177842Shear Tie · dentedAFT 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 COMPLETEAug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2023083177808Frame · dentedAFT 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.Aug 22, 2023 · N466UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2023090760281Stringer · corrodedMAJOR 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.Aug 20, 2023 · N466UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2023090660307Shear Tie · corrodedFAULT- AFT FUSELAGE SKIN BETWEEN STA. 1680-1700, S-27L HAS BULDGING BETWEEN TWO STRINGER RIVETS. DOT 8-002. VERIFIED JOB COMPLETE.Aug 20, 2023 · N466UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2022042881548Bracket · brokenL1 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.Apr 28, 2022 · N466UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2021092974395Skin · noneINSPECTION TYPE:SEG4#2 ENGINE PYLON. OUTBD INTERNAL STRUCTURE HAS BULDGING CORRISION.SKIN REPLACED IAW SRM 51-40-02-0G.Sep 29, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2021092974396Floorbeam · corrodedINSPECTION 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-.Sep 29, 2021 · N466UP · Boeing 75724APF · Standard Practices/StructuresSDR IPXA2021092574274Skin · corrodedINSPECTION 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 VSep 25, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon StructureSDR IPXA2021092474227Skin · corrodedINSPECTION TYPE:SEG4#1 ENGINE INBD PYLON FRAME FOR DOOR PANEL 433GR HAS CORROSION ON INSIDE LOWERREMOVE AND REPLACE SKINSep 24, 2021 · N466UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2021092374183Floorbeam · corrodedINSPECTION 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-Sep 23, 2021 · N466UP · Boeing 75724APF · Standard Practices/Structures
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