N583UP
Service difficulty reports · 420
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 = 'N583UP' 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 = 'N583UP' 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 IPXA2024081466239Support Fitting · cracked**SDR FILED OPEN**FAULT - AGING A/C INSPECTION : FOUND NO.8 SPOILER SUPPORT FITTING COLLAR CRACK. (REPLACE) REVIEWEDSDR IPXA2024081364749Support Fitting · corroded**SDR FILED OPEN**FAULT - R/H WING STA OLES 1525.45 FRONT SPAR FIXED PNL SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVICEABLE TAG NOSDR IPXA2024081364774Link · corroded**SDR FILED OPEN**FAULT - R/H WING STA OLES 1483.95 , 1493.45 FRONT SPAR FIXED PNL 2EA SUPPORT FITTING ROD CORROSION (AGING A/C INSPECTION). (REPLACE) 1. I.A.W AMM 20-51-01-912-008 REV.111 REPLACED THE ROD.<BR>2. COND CHECK NORMAL.<BR><BR>IPC VERIFIED AND SERVSDR IPXA2024081166455Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT L/H UNDER FLOOR, STA 1140, MID SPAR (REPAIR) CHECK NORMAL.SDR IPXA2024081166354Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1100, S-20C (REPAIR) CHECK NORMAL.SDR IPXA2024081166332Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+11", S-24C~S-25C (REPAIR) CHECK NORMAL.SDR IPXA2024081166310Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1040 + 12", S-27C (REPAIR) CHECK NORMAL.SDR IPXA2024081166287Skin Panel · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN, MAIN DECK CARGO COMPARTMENT UNDER FLOOR, STA 1060+6" S-25C (REPAIR) CHECK NORMAL.SDR IPXA2024081265808Floorbeam · corroded*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 740 LBL 5 ~ 10 (REPAIR) CHECK NORMAL.SDR IPXA2024081265029Floorbeam · corroded*SDR FILED OPEN* FAULT - CORROSION - CHORD, MAIN DECK FLOOR BEAM UPPER CHORD, STA 640 LBL 100 (REPAIR) OK TO WORKSDR IPXA2024080666256Aileron · corroded*SDR FILED OPEN* FAULT - AGING A/C INSPECTION : FOUND LH WING OUTBD AILERON T/E & DISCHARGE CORROSION. (REPLACE) 1.REMOVE THE DAMAGED STRIPS. PREPARE THE BONDING SURFACES AND BOND THE NEW STRIPS WITH RESIN CURED AT 80°F FOR 10 HOURS WITH CONSTANT PRESSURE I.ASDR IPXA2024073165776Plate · corrodedCORRODED PLATE, MAIN DECK CARGO FLOOR PANEL SUPPORT PLATE, STA 1500 RBL 10 (REPAIR) INSTALL FABRICATE PART I.A.W. SRM 51-40-02-0G REV.101 AND BOEING DWG NO:65B38407 SH 1 REV.C. PAPER CHECK OK.SDR IPXA2024080448895Drag Fitting · crackedCRACK - DURING PERFORM EO-26756-JIC002 FOUND SKIN CRACK AT STA 980 S-38R. (REPAIR). REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.40581, SRM 53-20-01-2R-2 REV.101 AND UPS EO-91158-REQ1 REV1. JOB COMPLETED.SDR IPXA2024081730033Panel · crackedCRACK - SKIN, UPPER FACE OF L/H WING NO.5 V.C. FLAP FOLDING NOSE, NEAR INBD ARM LOWER FITTING. (REPAIR). ACCOMPLISHED UPS EO-91129-REQ1 REV1.SDR IPXA2024081130140Stringer · crackedCRACK - STRINGER, L/H WING NO.7 V.C FLAP INNER FACE STRINGER. (REPLACE). I.A.W AMM 27-81-02-404-010 REV.111 STEP E(6) TO E(33) ADJUST NO.7 V.C FLAP.SDR IPXA2024080513809Roller · damaged*SUPPLEMENTAL SDR* FAULT - FOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT AFT-LOWER SIDE. IAW AMM 20-11-28-964-010 REV. 111 REPLACE L1 ENTRY DOOR LATCH ROLLER AT AFT-LOWER SIDE. ALL PAPERWORK C/WSDR IPXA2024071513809Roller · damagedFOUND L1 ENTRY DOOR LATCH ROLLER DAMAGED AT AFT-LOWER SIDE. OPENSDR IPXA2024081904062Panel · debondedDISBOND RH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1007-4 (SHEET METAL RMV AND REINSTALL PNL). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W SRM 51-40-02-0G REV.101 AND UPS EO-90959-REQ1 REV1.SDR IPXA2024081904632Panel · debondedDISBOND, LH VERTICAL STABILIZER LOWER FORWARD TORQUE BOX PANEL DISBOND P/N: 186U1006-3 (REPLACE). REMOVED THE EXISTING FASTENERS I.A.W SRM 51-40-02-0G REV.101. ACCOMPLISHED JOB I.A.W UPS EO-90958-REQ1 REV1.SDR IPXA2024072973714Bracket · crackedCRACKED BRACKET, ATTACH FRONT SPAR OF L/H WING INBD L/E UPPER RIB ILES 338. (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.101. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B13921 SH 2 REV:H, 112U2001 SH 5 REV:B.SDR IPXA2024032545819Engine · power loss*IN FLIGHT SHUT DOWN* AT FL350, #4 ENGINE SHOWED REDUCED THRUST AND DID NOT RESPOND TO THRUST LEVEL INPUT. THERE WERE NO EICAS MSG€™S OR CAUTION INDICATIONS ON THE ENG PAGE. CREW ELECTED TO SHUT DOWN #4 ENGINE. R&R #4 ENGINE PS3 LINE NEAR 8 O€™CLOCK POSITIONSDR IPXA2025022695949Skin · dented*** SUPPLEMENTAL SDR *** LH WING LEADING EDGE FLAP #9 HAS DENT AROUND OUTBOARD HINGE. COMPLIED WITH EO-89401-REQ3SDR IPXA2024021395947Skin · dentedLH HAND WING LEADING EDGE FLAP #8 HAS 2 DENTS/WEAR MARKS WHERE IT APPEARS TO BE RUBBING STABILIZING BARS ON LEADING EDGE OF WING. FOUND NO DAMAGE TO STAB BARS RESTORED FINISHES. COMPLETED STEPS 1-4 AND 7 OF EO-89403-REQ1. C/W EO-89403-REQ1SDR IPXA2024020595949Skin · dented*SDR FILED OPEN* LH WING LEADING EDGE FLAP #9 HAS DENT AROUND OUTBOARD HINGE. ACCOMPLISHED UT IAW NDTSPM PART 4, 51-00-00, MINIMUM MATERIAL REMAINING .032€?. ACCOMPLISHED HFEC IAW NDTSPM PART 6, 51-00-00 NO CRACKS DETECTED€¦SDR IPXA2024020595947Skin · dented*SDR FILED OPEN* LH HAND WING LEADING EDGE FLAP #8 HAS 2 DENTS/WEAR MARKS WHERE IT APPEARS TO BE RUBBING STABILIZING BARS ON LEADING EDGE OF WING. FOUND DENT 13€? FROM OUTBD EDGE .6€? IN DIAMETER .020€? DEEP WITH .032€? MATERIAL REMAINING. FOUND SECOND DENSDR IPXA2024020798510Skin · damagedLEFT O/B MIDFLAP HAS THE LOWER SKIN PULLED AWAY FROM CORE AND IS DELAMINATED OUTBOARD OF #1 CANOE FAIRING.***SM39/LMX2***HGR*** FABRICATED, CLEANED AND INSTALLED CORE PLUG. STARTED 250 DEGREE CURE. REF: SRM 57-53-01-2R-1 REPAIR 1, AND SRM 51-70-07-0G-0. REPAIRSDR IPXA2023112298510Skin · damaged*SDR FILED OPEN* LEFT O/B MIDFLAP HAS THE LOWER SKIN PULLED AWAY FROM CORE AND IS DELAMINATED OUTBOARD OF #1 CANOE FAIRING.***SM39/LMX2***HGR*** FABRICATED, CLEANED AND INSTALLED CORE PLUG. STARTED 250 DEGREE CURE. REF: SRM 57-53-01-2R-1 REPAIR 1, AND SRM 51-7SDR IPXA2022091913190Support · corrodedFAULT - FOUND APU FIRE SHUTDOWN MODULE SUPPORT CORROSION AT RIGHT BODY GEAR WHEEL WELL, STA 1457 WL 91 AREA ACCOMPLISHED PERMANENT REINFORCING REPAIR PER USP EO-84739-REQ1SDR IPXA2022091968976Stiffener · corrodedFAULT - CORROSION - CHORD, VERTICAL STABILIZER AUXILIARY STRUCTURE FRONT SPAR, LE STA 6 B, STA 2280 ACCOMPLISHED PERMANENT REINFORCING REPAIR PER UPS EO-84712-REQ1SDR IPXA2023011367147Floorbeam · corrodedFAULT - CORROSION - MAIN DECK FLOOR BEAM, STA 2360, LBL - 47 (REPLACED)SDR IPXA2022092042019Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241AG DISBOND, STA 1220 - 1264, LBL 97 - 117 (REPAIR) REVIEWEDSDR IPXA2022092042007Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241DG DISBOND, STA 1260 - 1300, LBL 33 - 76 (REPAIR) REVIEWEDSDR IPXA2022092042041Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241XF DISBOND, STA 1220 - 1260, LBL 11 - 33 (REPAIR) REVIEWEDSDR IPXA2022092136862Channel · crackedFAULT - CRACK - FND UPPER DECK TENSION TIE FWD CHANNEL, AT R/H STA 840 (REPAIR), PLEASE SPECIFY THE REASON FOR "REJECT"SDR IPXA2022092136851Channel · crackedFAULT - CRACK, FND UPPER DECK TENSION TIE FWD CHANNEL, AT RH STA 820 (REPAIR) COMPLETED PAPER FINAL CHECKSDR IPXA2022092136857Channel · crackedFAULT - CRACK, FND UPPER DECK TENSION TIE FWD CHANNEL, AT L/H STA 840 (REPAIR) COMPLETED PAPER FINAL CHECK.SDR IPXA2022092136855Channel · crackedFAULT - CRACK, FND UPPER DECK TENSION TIE AFT CHANNEL, AT R/H STA 740 (REPAIR).SDR IPXA2022062257228Skin Panel · dentedR/H SIDE FUSELAGE SKIN DENT AFT OF THE AFT CARGO DOOR STR 37R 38R COMPLIED WITH ALL WORK STEPSSDR IPXA2021021465646Charger · inoperativeEMERGENCY LIGHT IN-OP MAIN DECK CREW ENTRY DOOR AFT POSITION . RELAMP NO HELP ASSY P/N 30-0407-3 . REF # 342045.ITEM DEFERRED PER MEL 33-51-1-0 .REPLACED BATTERY & CHARGER ASSY AT POS M5170 IAW AMM 33 51 04, OPS CHECK GOOD THIS CLEARS M 735652. AIPC 24-34-00 5SDR IPXA2020092960752Housing · brokenINSPECTION TYPE: C3 UPPER DECK EMERGENCY LIGHT BASE BROKEN AT STA 410 (L5730), IAW AMM 33-51-07-002-009, 33-51-07-402-015 REV 99.03. RPL UPPER DECK EMERGENCY LIGHT BASE AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY.SDR IPXA2020092960751Lens · damagedINSPECTION TYPE: C3 EMERGENCY LIGHT LENS DAMAGE AT UPPER DECK DOORWAY PATH (L05734), IAW AMM 33-51-07-002-009, 33-51-07-402-015 REV 99.03. RPL UPPER DECK EMERGENCY LIGHT ASSY AND PERFORMED EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY.SDR IPXA2020100460892Support · damagedINSPECTION TYPE: C3 ALTERNATE SURFACE FINISH AND OVERSIZED HOLES FOR SUPPORT (P/N : 65B38409-4) OF MAIN DECK OUTBOARD GUIDE RESTRAINT NEAR STA 2110 - 2200 RBL 98.58. REPAIR IAW BOEING SR 4-4884430222 AND UPS EO B747-5310-78041-A.SDR IPXA2020100460891Bracket · crackedINSPECTION TYPE: C3 CRACK WAS FOUND ON BRACKET (P/N : 146U1020-17) IN AFT CARGO COMPONENT AT STA 1920. REPAIR IAW BOEING SR 4-4868001341 AND UPS EO B747-5310-78008-A.SDR IPXA2020092660638Angle · corrodedINSPECTION TYPE: C3 CORROSION ON CLIP (P/N:65B07853-34) ON RT WING OUTBOARD LEADING EDGE CAVITY RIB ASSY NEAR OLES 1509.95. REPLACE NEW PART, IAW 747-400F SRM 51-40-02-0G, REV 89.00 AND BOEING DWG 65B07853 SH 3, REV A.SDR IPXA2020092660637Support · corrodedINSPECTION TYPE: C3 CORROSION ON FWD CARGO COMPARTMENT HANGER SUPPORT (P/N:453U1563-31) NEAR STA 986. REPLACE NEW PART, IAW 747-400F SRM 51-40-02-0G, REV 89.00, BOEING DWG 453U1563 SH 11 REV B DWG 453U1183 SH 1 REV B AND DWG 453U1183 SH 3 REV B.SDR IPXA2020071757880Window · arcedENROUTE, THE FO SMELLED AN ELECTRICAL ODOR AND NOTICED THE RIGHT SIDE WINDOW ARCING. TURNED THE RIGHT WINDOW HEAT OFF. RAN SMOKE, FIRE, FUMES, AND WINDOW DAMAGE CHECKLIST. CONTACTED MMOC AND DECIDED TO CONTINUE. REMOVED & REPLACED R2 WINDOW IAW AMM IAW 56-11SDR IPXA2020030652848Control Switch · faultyINSPECTION TYPE:NA**ATB, AC OOS ** RESULTED IN ATB ON CLIMBOUT PASSING =11000' WHILE ACCELERATING THROUGH 310 KTS WITH AUTOPILOT ENGAGED "STAB TRIM 2", "STAB TRIM 3" ADVISORY EICAS MSG ILLUMINATED ALONG WITH >AUTOPILOT CAUTION MSG. EMERGENCY DECLARED, JETTISSDR IPXA2020010350598Warning System · activated**AIR TURN BACK** DUE TO FLAPS PRIMARY AND FLAPS DRIVE EICAS USED.SDR IPXA2019010837642Skin · dentedINSPECTION TYPE:AOG DENTS ON FUSELAGE SKIN (P/N:65B04488-14) BETWEEN STA 1540 - STA 1560, S-44R TO S-46R. IN ADDITION, THE SHEAR TIE (P/N : 69B03680-1) HAS ALSO BEEN DAMAGED AT STA 1560, BETWEEN S-44R AND S-45R REPAIR IAW SRID : 3-4362758360 AND EO B747-5330-7SDR IPXA2018092874455Battery · inoperativeFOUND THE UPPER DECK EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY AND PERFORMED AN EMERGENCY LIGHT TEST, RESULT WAS SATISFACTORY IAW AMM 33-51-04-902-001-001 REV 93.01.
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