# Service difficulty reports: N581UP

A list on [N581UP](https://openairdocs.org/aircraft/N581UP.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 309 reports

- [SDR IPXA2026050139587](https://openairdocs.org/sdr/IPXA2026050139587.md): Restraint · inoperative · Apr 23, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Structure
  > FWD 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.
- [SDR IPXA2026031630321](https://openairdocs.org/sdr/IPXA2026031630321.md): Landing Gear · warning message · Mar 11, 2026 · N581UP · Boeing 7474R7F · Main Landing Gear
  > AFTER 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.
- [SDR IPXA2026031230321](https://openairdocs.org/sdr/IPXA2026031230321.md): Warning Message · illuminated · Mar 11, 2026 · N581UP · Boeing 7474R7F · Landing Gear Position and Warning
  > AIR 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 32707,32703,32667,32
- [SDR IPXA2026030523252](https://openairdocs.org/sdr/IPXA2026030523252.md): Fitting · cracked · Feb 15, 2026 · N581UP · Boeing 7474R7F · Wing Main, Frame Structure
  > FOUND 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.
- [SDR IPXA2026030223147](https://openairdocs.org/sdr/IPXA2026030223147.md): Web · cracked · Feb 15, 2026 · N581UP · Boeing 7474R7F · Spoilers
  > FOUND 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.
- [SDR IPXA2026030223284](https://openairdocs.org/sdr/IPXA2026030223284.md): Bracket · cracked · Feb 15, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > FOUND 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.
- [SDR IPXA2026022146800](https://openairdocs.org/sdr/IPXA2026022146800.md): Sidewall Support · broken · Feb 11, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > FOUND 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,
- [SDR IPXA2026030611423](https://openairdocs.org/sdr/IPXA2026030611423.md): Floor Support · corroded · Feb 9, 2026 · N581UP · Boeing 7474R7F · Fuselage Structure (General)
  > MAJOR 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.
- [SDR IPXA2026030411397](https://openairdocs.org/sdr/IPXA2026030411397.md): Bracket · cracked · Feb 9, 2026 · N581UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CRACKED 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.
- [SDR IPXA2026030411388](https://openairdocs.org/sdr/IPXA2026030411388.md): Floor Support · corroded · Feb 9, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > CORRODED 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
- [SDR IPXA2026022111386](https://openairdocs.org/sdr/IPXA2026022111386.md): Angle · cracked · Feb 9, 2026 · N581UP · Boeing 7474R7F · Cargo/Baggage Doors
  > CRACKED ANGLE, FWD LOWER CARGO DOOR AFT ARM LINK ATTACH FITTING (AGING INSPECTION)(NO.5878) PAPER FINAL REVIEW COMPLETED
- [SDR IPXA2026022611384](https://openairdocs.org/sdr/IPXA2026022611384.md): Support · cracked · Feb 9, 2026 · N581UP · Boeing 7474R7F · Aerodynamic Fairings
  > CRACKED 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.
- [SDR IPXA2026022611393](https://openairdocs.org/sdr/IPXA2026022611393.md): Support · cracked · Feb 9, 2026 · N581UP · Boeing 7474R7F · Aerodynamic Fairings
  > CRACKED 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.
- [SDR IPXA2026031399855](https://openairdocs.org/sdr/IPXA2026031399855.md): Skin · corroded · Feb 8, 2026 · N581UP · Boeing 7474R7F · Ailerons
  > CORROSION, 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.
- [SDR IPXA2026030900041](https://openairdocs.org/sdr/IPXA2026030900041.md): Link · broken · Feb 8, 2026 · N581UP · Boeing 7474R7F · Wing Main, Frame Structure
  > CORRODED 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.
- [SDR IPXA2026022499855](https://openairdocs.org/sdr/IPXA2026022499855.md): Skin · corroded · Feb 8, 2026 · N581UP · Boeing 7474R7F · Ailerons
  > ***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 COND
- [SDR IPXA2026030296876](https://openairdocs.org/sdr/IPXA2026030296876.md): Fitting · deformed · Feb 8, 2026 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > DEFORMED 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.
- [SDR IPXA2026030196684](https://openairdocs.org/sdr/IPXA2026030196684.md): Fitting · cracked · Feb 8, 2026 · N581UP · Boeing 7474R7F · Auxiliary Power Unit (APU) Doors
  > CRACKED 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.
- [SDR IPXA2026022696780](https://openairdocs.org/sdr/IPXA2026022696780.md): Support Fitting · worn · Feb 8, 2026 · N581UP · Boeing 7474R7F · Auxiliary Power Unit (APU) Doors
  > WORN 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.
- [SDR IPXA2026022186459](https://openairdocs.org/sdr/IPXA2026022186459.md): Longeron Fitting · cracked · Feb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/Stringer
  > DURING 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.
- [SDR IPXA2026022186495](https://openairdocs.org/sdr/IPXA2026022186495.md): Longeron Fitting · cracked · Feb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/Stringer
  > CRACK - 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)
- [SDR IPXA2026030286480](https://openairdocs.org/sdr/IPXA2026030286480.md): Longeron Splice · cracked · Feb 7, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Longeron/Stringer
  > CRACKED 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, RE
- [SDR IPXA2026030287293](https://openairdocs.org/sdr/IPXA2026030287293.md): Fitting · broken · Feb 7, 2026 · N581UP · Boeing 7474R7F · Wing Miscellaneous Structure
  > BROKEN 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.
- [SDR IPXA2026030969236](https://openairdocs.org/sdr/IPXA2026030969236.md): Skin · cracked · Feb 6, 2026 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > MAJOR 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.
- [SDR IPXA2026030564510](https://openairdocs.org/sdr/IPXA2026030564510.md): Skin · cracked · Feb 6, 2026 · N581UP · Boeing 7474R7F · Wing, Plate/Skin
  > CRACK 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 OK
- [SDR IPXA2026030200832](https://openairdocs.org/sdr/IPXA2026030200832.md): Support Bracket · damaged · Feb 4, 2026 · N581UP · Boeing 7474R7F · Engine Thrust Reverser
  > DAMAGED 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.
- [SDR IPXA2026020510969](https://openairdocs.org/sdr/IPXA2026020510969.md): Battery · inoperative · Feb 3, 2026 · N581UP · Boeing 7474R7F · Emergency Lighting
  > FOUND THE L1 DOOR AREA EMERGENCY LIGHT INOPERATIVE. REPLACEED, OK TO WORK
- [SDR IPXA2026020310969](https://openairdocs.org/sdr/IPXA2026020310969.md): Light · inoperative · Feb 3, 2026 · N581UP · Boeing 7474R7F · Emergency Lighting
  > FOUND THE L1 DOOR AREA EMERGENCY LIGHT INOPERATIVE.
- [SDR IPXA2025070185694](https://openairdocs.org/sdr/IPXA2025070185694.md): Crash Axe · corroded · Jun 30, 2025 · N581UP · Boeing 7474R7F · Emergency Equipment
  > FOUND MAIN CARGO DECK CRASH AXE RUSTY. R&R MCD CRASH AXE IAW AMM 25-60-00.
- [SDR IPXA2026030286670](https://openairdocs.org/sdr/IPXA2026030286670.md): Skin · ground damage · Mar 11, 2025 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. DAMAGE TO FUSELAGE SKIN ABOVE AFT CARGO DOOR CONTROL PANEL AT LAP SEAM CAUSED BY CARGO LOADER RAIL. FINAL CHECKED OK.
- [SDR IPXA2024120228803](https://openairdocs.org/sdr/IPXA2024120228803.md): Fire Detector · faulted · Nov 27, 2024 · N581UP · Boeing 7474R7F · Smoke Detection
  > €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 DAM
- [SDR IPXA2024111588508](https://openairdocs.org/sdr/IPXA2024111588508.md): Drain · clogged · Nov 14, 2024 · N581UP · Boeing 7474R7F · Standard Practices/Structures
  > **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 PE
- [SDR IPXA2024061177533](https://openairdocs.org/sdr/IPXA2024061177533.md): Evas Unit · malfunctioned · Jun 10, 2024 · N581UP · Boeing 7474R7F · Emergency Equipment
  > FOUND CAPTAIN EVAS MOTOR KEEP RUN. R/R CAPTAIN EVAS ASSY IAW AMM25-69-00/401 AND OPS CHECK NORMAL IAW AMM25-69-00/601.
- [SDR IPXA2024032089480](https://openairdocs.org/sdr/IPXA2024032089480.md): Battery · inoperative · Mar 11, 2024 · N581UP · Boeing 7474R7F · Emergency Lighting
  > FOUND 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.
- [SDR IPXA2024031189480](https://openairdocs.org/sdr/IPXA2024031189480.md): Battery · inoperative · Mar 11, 2024 · N581UP · Boeing 7474R7F · Emergency Lighting
  > *SDR FILED OPEN* FAULT - FOUND M5169 EMERGENCY LIGHT BATTERY INOP. (REPLACE) OK TO WORK
- [SDR IPXA2024031420377](https://openairdocs.org/sdr/IPXA2024031420377.md): Floorbeam · corroded · Feb 17, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, Floor Beam
  > FAULT - 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 AND
- [SDR IPXA2024030420404](https://openairdocs.org/sdr/IPXA2024030420404.md): Seat Track · corroded · Feb 17, 2024 · N581UP · Boeing 7474R7F · Fuselage, Seat/Cargo Attach Fittings
  > *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 COMPLETED
- [SDR IPXA2024030461498](https://openairdocs.org/sdr/IPXA2024030461498.md): Intercostal · cracked · Feb 14, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, Bulkhead
  > CRACK, 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 J
- [SDR IPXA2024031395384](https://openairdocs.org/sdr/IPXA2024031395384.md): Duct · corroded · Feb 4, 2024 · N581UP · Boeing 7474R7F · Cabin Cooling System
  > PACK 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 COMPLETED
- [SDR IPXA2024030495384](https://openairdocs.org/sdr/IPXA2024030495384.md): Angle · corroded · Feb 4, 2024 · N581UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > *SDR FILED OPEN* FAULT - PACK 3 AIR INTAKE DUCT CONNECTION ANGLE CORROSION. (REPLACE) OK TO WORK
- [SDR IPXA2024032684094](https://openairdocs.org/sdr/IPXA2024032684094.md): Skin · dented · Feb 3, 2024 · N581UP · Boeing 7474R7F · Cargo/Baggage Doors
  > BULK 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 DETAI
- [SDR IPXA2024020584094](https://openairdocs.org/sdr/IPXA2024020584094.md): Skin · dented · Feb 3, 2024 · N581UP · Boeing 7474R7F · Passenger/Crew Doors
  > *SDR FILED OPEN* FAULT - BULK CARGO DOOR OUTER SKIN ONE DENT, FWD EDGE 120 INCH TO BOTTOM EDGE. (EVALUATE) OK TO WORK
- [SDR IPXA2024021968385](https://openairdocs.org/sdr/IPXA2024021968385.md): Skin · debonded · Feb 2, 2024 · N581UP · Boeing 7474R7F · Spoilers
  > MAJOR 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.
- [SDR IPXA2024031445752](https://openairdocs.org/sdr/IPXA2024031445752.md): Skin · corroded · Feb 1, 2024 · N581UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > *** 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 T
- [SDR IPXA2024030445752](https://openairdocs.org/sdr/IPXA2024030445752.md): Spar · corroded · Feb 1, 2024 · N581UP · Boeing 7474R7F · Wing Spar
  > *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.
- [SDR IPXA2024030425160](https://openairdocs.org/sdr/IPXA2024030425160.md): Shear Tie · cracked · Jan 25, 2024 · N581UP · Boeing 7474R7F · Fuselage Internal Mounting Structure
  > FAULT - 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. REVIEWED
- [SDR IPXA2024032081123](https://openairdocs.org/sdr/IPXA2024032081123.md): Mount · cracked · Jan 4, 2024 · N581UP · Boeing 7474R7F · Engine Mount Section
  > LARGE 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.
- [SDR IPXA2024010481123](https://openairdocs.org/sdr/IPXA2024010481123.md): Unknown · unknown · Jan 4, 2024 · N581UP · Boeing 7474R7F · Engine (Turbine/Turboprop)
  > *** 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.
- [SDR IPXA2023121486591](https://openairdocs.org/sdr/IPXA2023121486591.md): Flap System · warning message · Dec 14, 2023 · N581UP · Boeing 7474R7F · Trailing Edge Flap Control System
  > *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
- [SDR IPXA2023100203895](https://openairdocs.org/sdr/IPXA2023100203895.md): Spoiler · delaminated · Sep 30, 2023 · N581UP · Boeing 7474R7F · Spoilers
  > RIGHT WING SPOILER DELAMINATED.. VERIFIED COMPLETION OF #11 SPOILER PANEL PER AMM 27-61-02

Next page: https://openairdocs.org/aircraft/N581UP/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N581UP/reports

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