N581UP

Service difficulty reports · 309

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 = 'N581UP' 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 IPXA2026050139587Restraint · inoperativeFWD CARGO AFT MOST DOOR SILL ROLLOUT LOCK WON`T STAY UP LOCK 59. I.A.W AMM25-54-02-000-801 REV116 AND I.A.W AMM25-54-02-400-801 REV116 REPLACE DOOR SILL ROLLOUT WITH NEW PARTS.Apr 23, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, StructureSDR IPXA2026031630321Landing Gear · warning messageAFTER TAKEOFF AND GEAR RETRACTION "GEAR DISAGREE" EICAS MSG. RT MAIN FWD GEAR DOWN INDICATION VERIFIED WING GEAR SWING OPERATION SUCCESSFUL. NO LEAKS NOTED PERFORMED PSEU GRND TEST & PRI LAD GEAR SYS & ALT LAND GEAR SYS TESTS PASSED PER AMM 32-09-03-745-019.Mar 11, 2026 · N581UP · Boeing 7474R7F · Main Landing GearSDR IPXA2026031230321Warning Message · illuminatedAIR TURN BACK, AFTER TAKEOFF & GEAR RETRACTION GEAR DISAGREE EICAS MSG. RT MAIN FWD GEAR DOWN INDICATION AFTER TAKEOFF VISUALLY SAW AFTER GEAR RETRACTION THE RT WING GEAR DID NOT MOVE AND STOW. AFTER ACFT BLOCKED IN CMC REPORTS MSG NUMBERS 32707,32703,32667,32Mar 11, 2026 · N581UP · Boeing 7474R7F · Landing Gear Position and WarningSDR IPXA2026030523252Fitting · crackedFOUND RT SPOILER NR 7 INBD SIDE SUPPORT RIB FITTING CRACKED, WBL 255. IAW AMM 20-51-01-912-008, REV 115 INSTALLED THE SUPPORT ROD. CONDITION CHECKED NORMAL.Feb 15, 2026 · N581UP · Boeing 7474R7F · Wing Main, Frame StructureSDR IPXA2026030223147Web · crackedFOUND LT NR 5 SPOILER OTBD SIDE, SUPPORT WEB CRACKED, WBL 432. REMOVED THE DAMAGED WEB IAW SRM 51-40-02-0G, REV 105, INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 106, DWG 65B10865, SHT 2, REV N, & DWG 65B11629, SHT 2, REV E.Feb 15, 2026 · N581UP · Boeing 7474R7F · SpoilersSDR IPXA2026030223284Bracket · crackedFOUND MAIN DECK CARGO TRIM AIR DUCT SUPPORT BRACKET CRACKED, BS 1180 LT. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 106, INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 106, & DWG 214U2177, SHT 2, REV C.Feb 15, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous StructureSDR IPXA2026022146800Sidewall Support · brokenFOUND FWD CARGO SIDEWALL SUPPORT BROKEN AT BS 680, RT. REMOVED THE DAMAGE SIDEWALL SUPPORT IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW SIDEWALL SUPPORT IAW SRM 51-40-02-0G, REV 105, DWG 65B60587, SHT 1, REV C, DWG 65B01727, SHT 26, REV D, & DWG 65B01728,Feb 11, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous StructureSDR IPXA2026030611423Floor Support · corrodedMAJOR REPAIR, CORRODED SUPPORT, MAIN DECK FLOOR SUPPORT AT BS 1580, LBL 110. REMOVED MAIN DECK CARGO FLOOR PANEL IAW AMM 53-21-02-404-006, REV 115. INSTALLED MAIN DECK CARGO FLOOR PANEL.Feb 9, 2026 · N581UP · Boeing 7474R7F · Fuselage Structure (General)SDR IPXA2026030411397Bracket · crackedCRACKED NR 4 PYLON HYD RESERVOIR BLEED VALVE MOUNTING BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 105, & DWG 65B82300, SHT 4, REV B.Feb 9, 2026 · N581UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026030411388Floor Support · corrodedCORRODED MAIN DECK FLOOR SUPPORT AT BS 980, LBL 110. IAW AMM 53-21-02-004-001 REV 115, REMOVED MAIN DECK CARGO FLOOR PANEL AT BS 980, LBL 110, G.V.I CONDITION CHECK NORMAL. ACCOMPLISHED REPAIR IAW EO-96680-REQ1, REV 1 & EGAT EI F2026A53M-368, REV 1. MAJOR Feb 9, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous StructureSDR IPXA2026022111386Angle · crackedCRACKED ANGLE , FWD LOWER CARGO DOOR AFT ARM LINK ATTACH FITTING (AGING INSPECTION)(NO.5878) PAPER FINAL REVIEW COMPLETEDFeb 9, 2026 · N581UP · Boeing 7474R7F · Cargo/Baggage DoorsSDR IPXA2026022611384Support · crackedCRACKED BRACKET, RT AFT WING TO BODY FAIRING SUPPORT, BS 1480, RBL 100. REMOVED THE DAMAGE SUPPORT IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW SUPPORT IAW SRM 51-40-02-0G, REV 106, & DWG 65B15085, SHT 17, REV H.Feb 9, 2026 · N581UP · Boeing 7474R7F · Aerodynamic FairingsSDR IPXA2026022611393Support · crackedCRACKED BRACKET, LT AFT WING TO BODY FAIRING SUPPORT, BS 1480, LBL 100. REMOVED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW SUPPORT IAW SRM 51-40-02-0G, REV 106, & G DWG 65B15085, SHT 17, REV H.Feb 9, 2026 · N581UP · Boeing 7474R7F · Aerodynamic FairingsSDR IPXA2026031399855Skin · corrodedCORROSION, R/H WING OUTBD AILERON TE LOWER SURFACE AROUND DISCHARGER BASE, NR 1 FROM THE INBD (AGING INSPECTION) (NO.5862)(REPAIR) IAW AMM 20-51-01-912-008 REV.115 INSTALL R/H WING OUTBD AILERON TE LOWER PANEL P/N:65B02152-2 AND CONDITION CHECK NORMAL.Feb 8, 2026 · N581UP · Boeing 7474R7F · AileronsSDR IPXA2026030900041Link · brokenCORRODED LINK, LOWER SIDE OF LT WING OUTBD L/E CAVITY UPPER RIB LOWER LINK, OLES 1340 IAW AMM 20-51-01-912-008, REV. 115. REPLACED THE LINK.Feb 8, 2026 · N581UP · Boeing 7474R7F · Wing Main, Frame StructureSDR IPXA2026022499855Skin · corroded***SDR FILED OPEN*** FAULT-CORROSION, R/H WING OUTBD AILERON TE LOWER SURFACE AROUND DISCHARGER BASE, #1 FROM THE INBD (AGING INSPECTION) (NO.5862)(REPAIR) I.A.W AMM 20-51-01-912-008 REV.115 INSTALL R/H WING OUTBD AILERON TE LOWER PANEL P/N:65802152-2 AND CONDFeb 8, 2026 · N581UP · Boeing 7474R7F · AileronsSDR IPXA2026030296876Fitting · deformedDEFORMED FITTING , APU COMPARTMENT LT AFT AREA , BS 2775, S42L.. REMOVED THE DAMAGED FITTING IAW SRM 51-40-02-0G-0, REV 105, & INSTALLED THE FITTING IAW SRM 51-40-02-0G, REV 106, & DWG 65B02830, SHT 2, REV C.Feb 8, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous StructureSDR IPXA2026030196684Fitting · crackedCRACKED FITTING, RT APU NR 4 DOOR LOCK FITTING, BS 2742. REMOVED THE DAMAGED FITTING IAW SRM 51-40-02-0G-0, REV 105, & INSTALLED A NEW FITTING IAW SRM 51-40-02-0G, REV 106, AND DWG 65B02771, SHT 13, REV B.Feb 8, 2026 · N581UP · Boeing 7474R7F · Auxiliary Power Unit (APU) DoorsSDR IPXA2026022696780Support Fitting · wornWORN FITTING, RT APU DOOR UPPER CABLE SUPPORT FITTING, BS 2701. REMOVEED THE DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 105, & INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 106, DWG 69B70240, SHT 1, REV C, & DWG 287U4804, SHT 1, REV E.Feb 8, 2026 · N581UP · Boeing 7474R7F · Auxiliary Power Unit (APU) DoorsSDR IPXA2026022186459Longeron Fitting · crackedDURING PERFORM UPS EO-281410-JIC017 FOUND LOWER LONGERON SPLICE FITTING AFT SIDE CRACK AT STA 2598 S-11R. ACCOMPLISHED REPAIR I.A.W EO-96692-REQ1 REV1 AND EGAT EI F2026A53M-361 REV.2.Feb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/StringerSDR IPXA2026022186495Longeron Fitting · crackedCRACK - FITTING - DURING PERFORM UPS EO-28141-JIC017 FOUND LOWER LONGERON SPLICE FITTING AFT SIDE CRACK AT STA 2598 S-11L (REPLACE) RII COMPLETED STEP 19 PERFORM E.I. NO.F2026A53M-361 SEQUENCE:B PAGE 2 OF 10 STEP:12. VERIFY THE SERVICE DIFFICULTY REPORT ( SDR)Feb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/StringerSDR IPXA2026030286480Longeron Splice · crackedCRACKED FITTING, DURING PERFORMANCE OF EO-28141-JIC017, FOUND THE UPPER LONGERON SPLICE FITTING AFT SIDE CRACKED AT BS 2598, S11L. REMOVED THE DAMAGE LONGERON SPLICE IAW SRM 51-40-02-0G-0, REV 106, AND INSTALLED A NEW LONGERON SPLICE IAW SRM 51-40-02-0G-0, REFeb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/StringerSDR IPXA2026030287293Fitting · brokenBROKEN FITTING, LT WING INBD TE CAVITY UPPER RIB SUPPORT FITTING, WBL 432. REMOVED THE DAMAGED FITTING IAW SRM 51-40-02-0G, REV 106, & INSTALLED A NEW FITTING IAW SRM 51-40-02-0G, REV 106, & DWG 65B10865, SHT 2, REV N.Feb 7, 2026 · N581UP · Boeing 7474R7F · Wing Miscellaneous StructureSDR IPXA2026030969236Skin · crackedMAJOR REPAIR, DURING PERFORMANCE OF EO-27983-JIC001, FOUND SKIN CRACKED AT AFT CARGO DOOR CUTOUT FWD CORNER. ACCOMPLISHED REPAIR IAW EO-96736-REQ1, REV 1, AND EGAT EI F2026A53M-364 REV 1. AND SRM 53-60-01-2R-3, REV 106.Feb 6, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/SkinSDR IPXA2026030564510Skin · crackedCRACK LEFT WING LEADING EDGE UPPER FIXED PANEL. REPAIRED I.A.W AMM 27-81-03-402-019 REV.115 STEP 3.A TO 3.F. INSTALLED THE L2 PDU CHECK OKFeb 6, 2026 · N581UP · Boeing 7474R7F · Wing, Plate/SkinSDR IPXA2026030200832Support Bracket · damagedDAMAGED NR 4 ENGINE RT THRUST REVERSER INNER DRAIN TUBE SUPPORT BRACKET. REMOVED THE DAMAGED SUPPORT BRACKET IAW SRM 51-40-02-0G, REV 106, & INSTALLED A NEW SUPPORT BRACKET IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-52, REV 94.Feb 4, 2026 · N581UP · Boeing 7474R7F · Engine Thrust ReverserSDR IPXA2026020510969Battery · inoperativeFOUND THE L1 DOOR AREA EMERGENCY LIGHT INOPERATIVE. REPLACEED, OK TO WORKFeb 3, 2026 · N581UP · Boeing 7474R7F · Emergency LightingSDR IPXA2026020310969Light · inoperativeFOUND THE L1 DOOR AREA EMERGENCY LIGHT INOPERATIVE.Feb 3, 2026 · N581UP · Boeing 7474R7F · Emergency LightingSDR IPXA2025070185694Crash Axe · corrodedFOUND MAIN CARGO DECK CRASH AXE RUSTY. R&R MCD CRASH AXE IAW AMM 25-60-00.Jun 30, 2025 · N581UP · Boeing 7474R7F · Emergency EquipmentSDR IPXA2026030286670Skin · ground damageMAJOR REPAIR. DAMAGE TO FUSELAGE SKIN ABOVE AFT CARGO DOOR CONTROL PANEL AT LAP SEAM CAUSED BY CARGO LOADER RAIL. FINAL CHECKED OK.Mar 11, 2025 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/SkinSDR IPXA2024120228803Fire Detector · faulted€Œ DET FIRE/OVHT 4 €Œ ILLUM ON. T/O AFTER V-1 ALL INDICATIONS NORMAL AFTER T/O. REFERENCE BAR CODE T3F18E005NC5S FOR MAINTENANCE ACTIONS C/W ON THIS ISSUE. C/W INSPECTION OF #4 ENGINE FOR PNEUMATIC LEAKS , NO LEAKS NOTED, INSPECTED OVHT/ FIRE LOOPS FOR DAMNov 27, 2024 · N581UP · Boeing 7474R7F · Smoke DetectionSDR IPXA2024111588508Drain · clogged**DIVERSION**MASTER WARNING LIGHT AND BELL COME ON INTERMITTENTLY. BUT NO EICAS MESSAGE. FOUND CLOGGED DRAIN ABOVE FIRE/SMOKE CARD FILE. CLEARED DRAIN PER AMM 51-41-01. RERACKED CARDS IN FIRE/SMOKE CARD FILE PER AMM 26-10-01. PERFORMED FIRE OVHT GROUND TEST PENov 14, 2024 · N581UP · Boeing 7474R7F · Standard Practices/StructuresSDR IPXA2024061177533Evas Unit · malfunctionedFOUND CAPTAIN EVAS MOTOR KEEP RUN. R/R CAPTAIN EVAS ASSY IAW AMM25-69-00/401 AND OPS CHECK NORMAL IAW AMM25-69-00/601.Jun 10, 2024 · N581UP · Boeing 7474R7F · Emergency EquipmentSDR IPXA2024032089480Battery · inoperativeFOUND M5169 EMERGENCY LIGHT BATTERY INOP. REPLACED M5169 EMERGENCY LIGHT BATTERY AND PERFORMED INSTALLATION TEST I.A.W AMM 33-51-04-902-001-001 REV. 109. THE RESULT WAS SATISFACTORY.Mar 11, 2024 · N581UP · Boeing 7474R7F · Emergency LightingSDR IPXA2024031189480Battery · inoperative*SDR FILED OPEN* FAULT - FOUND M5169 EMERGENCY LIGHT BATTERY INOP. (REPLACE) OK TO WORKMar 11, 2024 · N581UP · Boeing 7474R7F · Emergency LightingSDR IPXA2024031420377Floorbeam · corrodedFAULT - CORROSION - CABIN FLOOR BEAM UPPER CHORD, STA 480 LBL 80 TO LBL 112. (REPAIR) I.A.W AMM 25-57-04-404-022 AND AMM 25-58-02-404-126 REV.109 INSTALL MAIN DECK CARGO HANDLING AND JOB COMPLETED. REPAIR DAMAGE AREA I.A.W EO-89671-REQ1 REV.1(T3F18E0043BRK ANDFeb 17, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, Floor BeamSDR IPXA2024030420404Seat Track · corroded*SDR FILED OPEN* *MAJOR REPAIR* FAULT - CORROSION - CABIN SEAT TRACK, STA 980 LBL 81. (REPAIR) I.A.W AMM 25-58-01-404-006 REV.109 INSTALL MAIN DECK CARGO HANDLING AND JOB COMPLETEDFeb 17, 2024 · N581UP · Boeing 7474R7F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2024030461498Intercostal · crackedCRACK, INTERCOSTAL, STA 1000, RBL 106 (REPLACE) REMOVE DAMAGE PART I.A.W SRM 51-40-02-0G REV.100. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.100 AND BOEING DWG NO:65B16038 SH.1 REV:D. I.A.W AMM 53-21-02-404-006 REV.109 INSTALL MAIN DECK CARGO FLOOR PANEL AND JFeb 14, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, BulkheadSDR IPXA2024031395384Duct · corrodedPACK 3 AIR INTAKE DUCT CONNECTION ANGLE CORROSION. (REPLACE) REMOVE DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.99. INSTALL NEW PARTS I.A.W SRM 51-40-02-0G REV.99 AND BOEING DWG NO:65B09715 SH.3 REV:G. JOB COMPLETEDFeb 4, 2024 · N581UP · Boeing 7474R7F · Cabin Cooling SystemSDR IPXA2024030495384Angle · corroded*SDR FILED OPEN* FAULT - PACK 3 AIR INTAKE DUCT CONNECTION ANGLE CORROSION. (REPLACE) OK TO WORKFeb 4, 2024 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous StructureSDR IPXA2024032684094Skin · dentedBULK CARGO DOOR OUTER SKIN ONE DENT, FWD EDGE 120 INCH TO BOTTOM EDGE. (EVALUATE) MEASURE DENT AREA DIMENSION LENGTH=1.12" WIDTH=0.27" DEPTH=0.0067" A/Y=40 IT WAS WITHIN ALLOWABLE DAMAGE LIMIT I.A.W SRM 52-30-01-1A-1 ALLOWABLE DAMAGE 1 FIGURE 101 TABLE 1 DETAIFeb 3, 2024 · N581UP · Boeing 7474R7F · Cargo/Baggage DoorsSDR IPXA2024020584094Skin · dented*SDR FILED OPEN* FAULT - BULK CARGO DOOR OUTER SKIN ONE DENT, FWD EDGE 120 INCH TO BOTTOM EDGE. (EVALUATE) OK TO WORKFeb 3, 2024 · N581UP · Boeing 7474R7F · Passenger/Crew DoorsSDR IPXA2024021968385Skin · debondedMAJOR REPAIR, DISBOND - SKIN PNL , RH WING NO.9 SPOILER UPPER SURFACE. INSTALL DOUBLER WITH FILM ADHESIVE AND CURED AT 250°F FOR 100 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 747-400F SRM 51-70-10-2R-0 PARAGRAPH 18 & 20 REV.99.Feb 2, 2024 · N581UP · Boeing 7474R7F · SpoilersSDR IPXA2024031445752Skin · corroded*** SUPPLEMENTAL SDR *** FAULT - CORROSION - SKIN , AFT FACE OF R/H WING GEAR W/W FWD BULKHEAD CENTER TANK FUEL PUMP CUTOUT , STA 1241. (REPAIR) REMOVED CORROSION AREA I.A.W SRM 51-10-02-0G-0 REV.99. I.A.W AMM 28-31-01-404-011-002 REV.109 INSTALL CENTER WING TFeb 1, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/SkinSDR IPXA2024030445752Spar · corroded*SDR FILED OPEN* FAULT - CORROSION - SKIN , AFT FACE OF R/H WING GEAR W/W FWD BULKHEAD CENTER TANK FUEL PUMP CUTOUT , STA 1241. (REPAIR) 1.PERFORM EO-89629-REQ1 REV.1(T3F18E0041K6N).<BR>2.JOB COMPLETED.Feb 1, 2024 · N581UP · Boeing 7474R7F · Wing SparSDR IPXA2024030425160Shear Tie · crackedFAULT - SHEAR TIE CRACK, LOCATE AT STA 1000 LBL 57.5. (REPLACE) PERFORM SHEAR TIE REPLACEMANT I.A.W EO-80332-JIC006 REV.2 AND EO-89697-REQ1 REV.1. JOB COMPLETED. REVIEWEDJan 25, 2024 · N581UP · Boeing 7474R7F · Fuselage Internal Mounting StructureSDR IPXA2024032081123Mount · crackedLARGE CRACK OUTBOARD SIDE ENGINE 1 AT MOUNT POINT ON WING. INSTALL NO.1 ENG PYLON TO WING FARING I.A.W SRM 51-40-02-0G REV.100 AND DWG NO.65B13507 SH1 TRV.G AND DWG NO.65B13639 SH2 REV.D.Jan 4, 2024 · N581UP · Boeing 7474R7F · Engine Mount SectionSDR IPXA2024010481123Unknown · unknown*** SDR FILED OPEN *** LARGE CRACK OUTBOARD SIDE ENGINE 1 AT MOUNT POINT ON WING. FAULT BE DEFERRED FOR 15 DAYS WITH REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED EVERY FLIGHT CYCLE PER EO-89091-REQ2 IN ACCORDANCE WITH DEFERRAL REFERENCE EO-89091.Jan 4, 2024 · N581UP · Boeing 7474R7F · Engine (Turbine/Turboprop)SDR IPXA2023121486591Flap System · warning message*AIR TURN BACK* ON TAKEOFF CLIMBING OUT OF 2000 SELECTED FLAPS 15 FROM 5 AND FLAPS PRIMARY CAUTION AND LE MULT DRIVE MESSAGES CAME UP. FLAPS RETRACTED NORMAL AND LE RETRACT SLOW (SEC MORE).EXTENSION NORMAL ON LANDING DISCOVERED FLAPS PRIMARY AND LE MULT DRIVE Dec 14, 2023 · N581UP · Boeing 7474R7F · Trailing Edge Flap Control SystemSDR IPXA2023100203895Spoiler · delaminatedRIGHT WING SPOILER DELAMINATED .. VERIFIED COMPLETION OF #11 SPOILER PANEL PER AMM 27-61-02Sep 30, 2023 · N581UP · Boeing 7474R7F · Spoilers
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