N458UP
Service difficulty reports · 215
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 = 'N458UP' 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 = 'N458UP' 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 IPXA2026091821733Evas Unit · unsecureDURING 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 IPXA2026022092281Seat Track · corrodedSTR--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 REPAISDR IPXA2026012743275Floor Support · corrodedFLOOR 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 5SDR IPXA2026012343275Floor Support · corrodedAGING 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 51-00SDR IPXA2026022401372Angle · corrodedSTR, 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 WEBSDR IPXA2026022402462Angle · corrodedLEFT 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 5SDR IPXA2026022323794Strap · corrodedCORROSION 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-0SDR IPXA2025090211532Hose · failedLEFT 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 IPXA2025082811532Hydraulic System · leakingEMERGENCY 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 DRIVESDR IPXA2025082287433Flap System · malfunctionedEMERGENCY 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 IPXA2025062483756Door · bindingCREW ENTRY DOOR DIFFICUILT TO UNLOCK PERFORMED ADJUSTMENT OF CREW ENTRY DOOR IAW AMM 52-12-00, OPS CHECK GOOD AT THIS TIME.SDR IPXA2025062552431Attach Bracket · debondedF/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 IPXA2025061152431Attach Bracket · debondedF/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-REQ001SDR IPXA2025042864245Life Vest · missingFO'S LIFE JACKET MISSING. REPLACED FO'S LIFE JACKET IAW AMM 25-64-00/201SDR IPXA2024021912973Tee Angle · corrodedFAULT: 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 COMPLETESDR IPXA2024021805797Tee Angle · corrodedFAULT: 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 IPXA2024022889259Support · corrodedFAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED INSTALLED NEW "T" CHORD AT STA 1220 R/H IAW SRM 52-40-02SDR IPXA2024022092776Skin · corrodedNR 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 IPXA2024022292675Skin · corroded*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 IPXA2024022192899Doubler · corrodedMAJOR 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 IPXA2024021992798Skin · corrodedMAJOR 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 IPXA2024021992675Skin · corrodedMAJOR REPAIR, NR 2 ENGINE OUTBD PYLON, INNER SKIN FWD OF VENT PANEL HAS EXFOLIATION CORROSION. DOT 8-017. OK TO APPLY TOP-COAT APPROVED. OPENSDR IPXA2024021792899Skin · corrodedMAJOR 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. OPENSDR IPXA2024021789430Tee Angle · corrodedFAULT: 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 REVIEWEDSDR IPXA2024021589259Support · corroded*** SDR FILED OPEN *** FAULT: WING TO BODY T CHORD SUPPORT AT STA 1220 R/H IS CORRODED AUDIT COMPLETESDR IPXA2024021592776Skin · corrodedFAULT- #1 ENGINE OUTBD PYLON INNER SKIN, FWD OF VENT PANEL HAS EXFOLIATION CORROSION. OK TO INSTALL DOUBLER"INSP ONLY"SDR IPXA2024021773507Frame · dented*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 IPXA2024021673097Frame · dentedDENT 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 IPXA2024021960150Tee Angle · corrodedEVIDENCE 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 IPXA2022101187064Power Supply · inoperativeBOTH 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 SUPPLYSDR IPXA2022021478987None · noneINSPECTION 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 IPXA2022021579016Frame · noneINSPECTION 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-ASDR IPXA2021120976796First Aid Kit · noneINSPECTION TYPE:N/ASEAL BROKEN ON FIRST AID KITREPLACED FIRST AID KIT AS REQ PER GMM 08-02SDR IPXA2020111062217Glide Slope · failedINSPECTION 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 34-31-00-815-8SDR IPXA2020092260525Actuator · slowEMERGENCY 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 3SDR IPXA2020062435903Sensor · out of adjustINSPECTION 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 LANDINSDR IPXA2020051555278Light · inoperativeINSPECTION TYPE:N/AEMERGENCY LIGHT HAS FOUR INOP BULBSRELAMPED EMERGENCT LIGHT PER AMM 33-51-01-2 FOUR BULBSSDR IPXA2020033053628Slat · delaminatedINSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2SDR IPXA2020033053627Slat · delaminatedINSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2SDR IPXA2020032753623Slat · delaminatedINSPECTION TYPE:CP12#1 SLAT REMOVE FOR REPAIRREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2SDR IPXA2019061243113Structure · damagedRUDDER 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 IPXA2019061243112Structure · damagedRUDDER 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 IPXA2019050941939Hydraulic Line · not reportedINSPECTION 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 ALTERNATSDR IPXA2018032827932Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 251XMF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR IPXA2018040328140Panel · delaminatedINSPECTION 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 IPXA2018032527805Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XEF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR IPXA2018032727899Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XFF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR IPXA2018032727896Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 232XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR IPXA2018032727895Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 231XJF WAS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.SDR IPXA2018032827929Floor Panel · delaminatedINSPECTION TYPE: SEG3, MAIN DECK FLOOR PANEL 252XTF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.
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