N459UP
Service difficulty reports · 266
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 = 'N459UP' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA2026072758829Engine · failedEMERGENCY 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 INDICASDR IPXA2025112636097Flap System · inoperativeTE 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 IPXA2025103173256Stringer · corrodedWHILE 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 53-00-0SDR IPXA2025102833199Floor Support · corrodedMAIN 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 IPXA2025103131819Strap · corrodedSTRUCTURES, 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 RSDR IPXA2025102930140Angle · corrodedSTRUCTURES, 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 INSTALSDR IPXA2025103132465Strap · corrodedSTRUCTURES, 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 REVIEWEDSDR IPXA2025103034768Structure · corrodedMAIN 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 IPXA2025102633251Seat Track · corrodedMAIN DECK CARGO BELOW ACCESS PANEL 242XGF SEAT TRACK HAS CORROSION, FLL-028. OPENSDR IPXA2025102133199Floor Support · corrodedSTRUCTURES, MAIN DECK CARGO BELOW ACCESS PANEL 241XHF HAS CORROSION, FLL-026, ATA 53.SDR IPXA2025102198394Strap · corrodedAPU 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. 1825SDR IPXA2025103160829Stringer · corrodedSTRUCTURES, 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 IPXA2025103060968Skin · corrodedAFT 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 1SDR IPXA2025102661012Skin · corrodedAFT 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 IPXA2025102254371Strap · corrodedTAILCONE. 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 IPXA2025051420889Evas Unit · failedCAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00SDR IPXA2025051220889Evas Unit · no testCAPTAINS EVAS FAILED BLOWER CHECK R&R CAPTS EVAS REF AMM 25-69-00.SDR IPXA2024123020240Landing Gear · warning messageAFTER 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 NUSDR IPXA202412270001Landing Gear · faultedAFTER 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 IPXA2024092433591Window · warning messageON 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 LSDR IPXA2024091133591Warning Message · illuminatedSDR 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 IPXA2023120134182Relief Valve · malfunctionedAT 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 DEBSDR IPXA2023112859902Strake · corrodedFAULT: LH HORIZONTAL LOWER STRAKELET HAS EVIDENCE OF CORROISON DOT: 107-002. INTALLED STRAKAKELET IAW SRM 51-40-02. REVIEWEDSDR IPXA2023120543755Tee Angle · corroded*** SUPPLEMENTAL SDR *** FAULT: R/H WTB, T-CHORD STA 1220, FOUND EXFOLIATED CORROSION. FAULT WROTE UP FOR OTHER A/C, PLEASE REFER TO T3F18E00CTLTSDR IPXA2023120543694Tee Angle · corrodedR/H WTB, T-CHORD, RBL 63, FOUND EXFOLIATED CORROSION. FAULT CREATED FOR OTHER A/C (N456UP), PLEASE REFER TO T3F18E003CTKVSDR IPXA2023120543467Tee Angle · corroded*** 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 T3F18E003CTKRSDR IPXA2023111343755Unknown · unknownR/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 IPXA2023111343694Unknown · unknown*** 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 APPRSDR IPXA2023111343467Unknown · unknownR/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 IPXA2023112740899Skin · corroded*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 IPXA2023112533548Tee Angle · corrodedFAULT: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 IPXA2023112718179Tee Angle · corrodedFAULT: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.- REVIEWEDSDR IPXA2023112316833Web · corrodedFAULT: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 IPXA2023112989044Tee Angle · corrodedFAULT: 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. REVIEWEDSDR IPXA2023112867666Tee Angle · corrodedFAULT: 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. REVIEWEDSDR IPXA2023112767770Tee Angle · corrodedFAULT: R/H WTB, INTERCOSTAL, FOUND EXFOLIATE CORROSION, BETWEEN STA 1037 TO STA 1060. INSTALLED T-CHORD IAW SRM 51-40-02. REVIEWEDSDR IPXA2023111967834Tee Angle · corrodedR/H WTB, T-CHORD STA 1220, AT RBL 63 FOUND EXFOLIATED CORROSION. INSTALLED T-CHORD IAW SRM 51-40-02-0G. REVIEWEDSDR IPXA2025022649962Skin · corrodedWING RH I/B FLAP SURFACE CORROSION AT LOWER SURFACE. DOT119-029 PLEASE REF BARCODE T3F18E0039JV1 FOR CORRECTIVE ACTION AND INSTALLATION OF NEW FLAP.SDR IPXA2025022651282Skin · corrodedWING 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 IPXA2023112049962Skin · corroded*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 IPXA2023112051282Skin · corroded*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 IPXA2023112865059Tee Angle · corrodedFAULT: 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. REVIEWEDSDR IPXA2023112759219Tee Angle · corrodedFAULT: 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.- REVIEWEDSDR IPXA2023112758827Unknown · corrodedFAULT: 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.- REVIEWEDSDR IPXA2023112265202Tee Angle · corrodedFULT: 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 COMPLETEDSDR IPXA2023111958867Tee Angle · corrodedFAULT: 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. REVIEWEDSDR IPXA2023111959108Tee Angle · corrodedFAULT: 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. REVIEWEDSDR IPXA2023120535508Floor Panel · brokenMAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 INSTALLED FLOOR PANEL 232XVF I.A.W. AMM 53-01-024-023.SDR IPXA2023112732706Skin Panel · dented*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. REVIEWEDSDR IPXA2023111735508Floor Panel · brokenFAULT:MAIN CARGO COMPARTMENT FLOOR PANEL 232XVF BROKEN. DOT119-019 VERIFIED INSTALLATION OF FLOOR PANEL 232XVF
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