N326UP
Service difficulty reports · 146
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 = 'N326UP' 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 = 'N326UP' 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 IPXA2026072007978Window · crackedCAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM! REPLACED LT SLIDING FLIGHT DECK WINDOW IAW AMM 56-11-02. PRESSURIZED AIRCRAFT WITH NO LEAKS NOTED. WINDOW HEAT OPS TEST SUCCESSFUL. CAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOMSDR IPXA2026071707978Window · crackedCAPTAINS L2 WINDOW FOUND CRACKED FROM TOP TO BOTTOM!SDR IPXA2026060105255Window · crackedL SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH. PERFORMED RII INSPECTION PER GMM 04-02 AND AMM 56-11-10 VERIFIED PROPER INSTALL AND TORQUE OF ELECTRICAL CONNECTORS R+R LH NO. 3 WINDOW PER AMM 56-11-10/401. WINDOW HEAT CHECK OPS TESSDR IPXA2026052900055Window · crackedLEFT SIDE WINDOW EICAS. INNER PANE CRACKED. WINDOW HEAT SWITCH OFF IAW QRH.SDR IPXA2026052906642Window · failedL3 WINDOW BURNED AT TEMP CONTROL SENSORS. CREW REPORTED BURNING SMELL PRIOR TO WINDOW CRACKING. REF BARCODE [T3F18E008X3R6] FOR WINDOW REPLACEMENT. R+R RIGHT FORWARD AND LEFT SIDE WINDOW HEAT CONTROL UNIT, WHCU M192 PER AMM 30-41-02/401. OPS CHECK GOOD.SDR IPXA2026021059426Skin Panel · corrodedMAJOR REPAIR, CORROSION FUSELAGE SKIN STA 1410 BETWEEN S-38R AND S-39R. (REPAIR. ACCOMPLISHED THE REPAIR I.A.W SRM 53-00-01 REPAIR 29 REV. 94 AND EGAT EI NO.F2026A53M-286 REV.1 AND UPS EO-96454-REQ1 REV1.SDR IPXA2026020707464Skin Panel · crackedMAJOR REPAIR, FOUND CRACK ON THE NO.1 FWD ENTRY DOOR LH AFT LOWER CORNER SKIN. ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 94 AND EGAT WORK SHEET NO: 60075 AND UPS EO-87307-REQ7 REV2.SDR IPXA2026020977464Skin · crackedMAJOR REPAIR. FOUND A CRACK ON THE NR1 FWD ENTRY DOOR LT AFT LOWER CORNER SKIN. INSTALLED ENTRY DOOR SCUFF PLATE IAW AMM 53-13-01-424-005, REV 147. INSTALLED ENTRY DOOR DOORWAY LINING IAW AMM 52-12-02-404-025, REV 147.SDR IPXA2025063074896Light · inoperativeCOCKPIT EMERGANCY LIGHT EXIT INOP REMOVED AND REPLACED EMERGANCY BATTERY CHARGER ASSY PER MM 33-51-07. OPS CK GOODSDR IPXA2024102127737Cover · detachedEXIT LIGHT COVER FOR LIGHT OVER CREW DOOR HANDLE FELL OFF WILL NOT STAY ATTACHED. C/W EO-91789-REQ1SDR IPXA2024101927838Charger · inoperativeMAIN ENTRY DOOR EMERGENCY LIGHT WILL NOT ILLUMINATE AFTER ATTACHING COVER REMOVED AND REPLACED EMERGENCY BATTERY CHARGER ASSEMBLY IAW AMM 33-51-07. OPS CHECK GOOD.SDR IPXA2024030705540Window · leakingR2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. PERFORMED R2 WINDOW ADJUSTMENT PER AMM 56-11-02-825-122, STEP 2.J(1)(H). APPLIED FILLET SEALANT TO LOWER AFT CORNER OF R2 SEAL PER AMM 56-11-11-404-006.G(SDR IPXA2024030605540Window · leaking*** SDR FILED OPEN *** R2 WINDOW HAS LOUD SQUEAL WHICH STARTED ON CLIMB THROUGH DESCENT, AND IN CRUISE. EVIDENCE OF AIR LEAKAGE. C/W RIISDR IPXA2024012302696Angle · brokenFAULT - FOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 141T8310 SH. 4 REV. H. REVIEWEDSDR IPXA2024012301393Scuff Plate · crackedFAULT - FOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE). 1.I.A.W AMM 53-13-01-424-005 REV.141 INSTALLED THE SCUFF PLATE. 2.ACCOMPLISHED THE EXCESSIVE CABIN PRESSURE LEAKAGE TEST I.A.W AMM 05-51-24-782-001 REV.141, NO LEAKAGE WAS FOUND. 3.JOBSDR IPXA2024011202696Unknown · unknownFOUND THREE OF CLIPS WITH BROKEN ON CREW ENTRY DOOR LOWER SILL (REPLACE)SDR IPXA2024011201393Unknown · unknownFOUND THE SCREW ENTRY DOOR SCUFF PLATE WITH CRACK DAMAGE (REPLACE) OK TO WORKSDR IPXA2024012382386Pawl · wornFAULT - FOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE). I.A.W AMM 52-11-26-004-001 REV.141 AND AMM 52-11-26-404-003 REV.141 REPLACED PAWL, OPERATION CHECK NORMAL. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWEDSDR IPXA2024012382163Cap · crackedFAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR). REMOVE THE DAMAGE AREA (L:0.2", W:0.1 , 5" FROM AFTER EDGE AT LOWER EDGE) AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURE AT 200°F FOR 220 MINUTES KEEP A MINIMUM VACUUM OF 22 IN/HG I.A.W. UPSSDR IPXA2024012382059Web · cracked*SUPPLEMENTAL SDR* FAULT - CRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR). ACCOMPLISHED REPAIR I.A.W UPS EO-89236-REQ1 REV.1. JOB COMPLETED. C/W REVIEWSDR IPXA2024012282141Spar · brokenFAULT - BROKEN PLATE, LH WING T/E REAR SPAR LOWER SURFACE NEAR WS 698 (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 113T1663 SH. 2 REV. D. 3. JOB COMPLETED. REVIEWEDSDR IPXA2024011182059Unknown · unknownCRACK WEB, LH WING LE STRUCTURE INTERNAL WEB NEAR LES 594 (REPAIR) OK TO WORKSDR IPXA2024011182386Unknown · unknownFOUND CREW ENTRY DOOR EXTERNAL HANDLE PAWL WORN. (REPLACE) OK TO WORKSDR IPXA2024011182163Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK EDGE, LH WING OUTBD FLAP INBD SIDE END CAP (REPAIR) OK TO WORKSDR IPXA2024012360713Skin · damagedFAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE). 1.REMOVED DAMAGE PARTS I.A.W. SRM 51-40-02-0G REV.88 2.INSTALLED NEW PARTS I.A.W. SRM 51-40-02-0G REV.88 AND BOEING DWG NO 114T2800 SH.5 REV.G 3.JOB COMPLETED. REVIEWEDSDR IPXA2024012355631Skin · eroded*SUPPLEMENTAL SDR* FAULT - EROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA(LENGTH:0.5", WIDTH:0.3",DEPTH:1 PLY , 0.7" FROM TRAILING EDGE , 1" FROM OUTBOARD EDGE).BOND THE REPAIR PLIES WITH FISDR IPXA2024011060713Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - SPLICE, RH WING OUTBD FXD LE NOSE SKIN, OSS 694.55. (REPLACE)SDR IPXA2024011055631Unknown · unknownEROSION, LH WING NO.4 SLAT OUTBD CLOSURE PNL (REPAIR) OK TO WORKSDR IPXA2024011635744Angle · crackedFAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETESDR IPXA2024012337994Bumper · deformedFAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE). I.A.W AMM 52-12-02-004-001 REV.141 AND AMM 52-12-02-404-025 REV.141 REPLACED BUMPER. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWEDSDR IPXA2024012335573Seal · brokenFAULT - FOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE). I.A.W AMM 52-09-01-024-018 REV. 141 AND AMM 52-09-01-424-019 REV.141 REPLACED DOORWAY LINING SEAL. PARTS INFO ATTACHED AND JOB COMPLETED, CONDITION CHECK NORMAL. REVIEWEDSDR IPXA2024011735666Angle · crackedFAULT - CRACK - ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL 49.3.(REPLACE). REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-05 REV. 88. PERFORMED THE HEAT TREATMENT FROM 7075-O-063 CLAD TO T62 CONDITION. I.A.W. WORK SHEET NO.:40034 WORK INSTRUCTIONS STEP 3 ASDR IPXA2024011635775Angle · cracked*SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV. SDR IPXA2024011635793Angle · crackedFAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REV. C. 3. JOB COMPLETESDR IPXA2024011635810Angle · cracked*SUPPLEMENTAL SDR* FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE). 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 146T5650 SH. 5 REVSDR IPXA2024011037994Unknown · unknown*** SDR FILED OPEN *** FAULT - FOUND FWD ENTRY DOORWAY LINING BUMPER DEFORM (REPLACE) OK TO WORKSDR IPXA2024011035573Unknown · unknownFOUND ENTRY DOORWAY AFT LINING SEAL BROKEN (REPLACE) OK TO WORKSDR IPXA2024010935666Unknown · unknownCRACKED ANGLE, MAIN EQUIPMENT CENTER LEFT SIDE AT STA 246 LBL (REPLACE) OK TO WORKSDR IPXA2024010935810Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT RIGHT SIDE STA 1578 RBL 60 OUTBOARD SIDE (REPLACE) OK TO WORKSDR IPXA2024010935744Unknown · unknownCRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60 INBOARD SIDE (REPLACE) OK TO WORKSDR IPXA2024010935793Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - ANGLE BULK CARGO COMPARTMENT LEFT SIDE STA 1578 LBL 60 OUTBOARD SIDE (REPLACE) OK TO WORKSDR IPXA2024010935775Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - ANGLE, BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60 INBOARD SIDE (REPLACE) OK TO WORKSDR IPXA2024012322914Beam · crackedFAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV. 88. AND BOEING SERVICE BULLETIN 767-54-0SDR IPXA2024012322940Beam · crackedFAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE). 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88. 2. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV. 88. AND BOEING SERVICE BULLETIN 767-54-0SDR IPXA2024010822914Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)SDR IPXA2024010822940Unknown · unknownCRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING L/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)SDR IPXA2022110787881Lock · inoperativeINSPECTION TYPE:NACREW ENTRY DOOR SECURE LOCK STICKING.LUBED EXTERIOR APPR LATCH IN MECHANISM. DOOR OPERATES AS ADVERTISED.Ï¿½52-12-00-715-119SDR IPXA2022082785667None · noneINSPECTION TYPE:NA**ATB**AT APPROXIMIMATELY 3000FT, ON DEPARTURE "TAT PROBE" EICAS MESSAGE AND FAILURE.REPLACED TAT PROBE PER AMM 34-12-02-404-008, BUT SAME CONDITION. REPLACED CURRENT SENSING RELAY PER WDM 30-33-11 SHEET1, TAT PROBE HEAT SYSTEM OPERATION TESTSDR IPXA2022080985047Light · inoperativeINSPECTION TYPE:N/ADURING PDC FOUND EMG LIGHTS INOP.R/R EMG BATT PACK IAW AMM 33-51-07. OPS CHECK SAT.SDR IPXA2022072584563Eicas · fault messageINSPECTION TYPE:ETOP** ETOPS FILED OPEN**GOT A "R PACK TEMP" EICAS MSG ON SHORT FINAL. RAN QRH AND INOP LIGHT EXTINGUISHED. DEFERRED R PACK TEMP CONTROL AUTO MODE IAW MEL 21-51-3-1 - PLACARD INSTALLED; PARTS ON REQ 406077. SUGGEST REPLACING C/P AND SENSORD - 2
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