# Service difficulty reports: N583UP

A list on [N583UP](https://openairdocs.org/aircraft/N583UP.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 9 · 419 reports

- [SDR IPXA2026073173712](https://openairdocs.org/sdr/IPXA2026073173712.md): Hinge · broken · Jul 9, 2026 · N583UP · Boeing 7474R7F · Leading Edge Devices
  > FOUND RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE HINGE BROKEN. OK TO INSTALL, CONDITION CHECK SATISFIED. IAW AMM 27-81-02-404-010 REV.117 ASSEMBLY RT WING NR 24 V.C FLAP INBD SIDE FOLDING NOSE & INBD SIDE HINGE. CONDITION CHECK NORMAL.
- [SDR IPXA2026071539478](https://openairdocs.org/sdr/IPXA2026071539478.md): Stringer · damaged · Jul 7, 2026 · N583UP · Boeing 7474R7F · Leading Edge Devices
  > FOUND LT WING NR 5 VC FLAP UPPER SIDE STRINGER DAMAGE. INSTALL NEW STRINGER IAW SRM 51-40-02-0G REV.107 AND DWG 65B15168, SH2, REV G.
- [SDR IPXA2026072984187](https://openairdocs.org/sdr/IPXA2026072984187.md): Fitting · corroded · Jul 3, 2026 · N583UP · Boeing 7474R7F · Main Landing Gear
  > FOUND THE CORROSION ON INBOARD LOWER FITTING CAP AT LT BODY GEAR. IAW AMM 32-13-01-404-022 REV. 117 AND EI NO. F2026A53M-1507 SEQUENCE A, PERFORMED INSTALL, LEAK CHECK OF HYDRAULIC HOSE CONNECTIONS, TEST AND SWING AT LEFT BODY LANDING GEAR. CONDITION CHECK NO
- [SDR IPXA2026072984213](https://openairdocs.org/sdr/IPXA2026072984213.md): Fitting · corroded · Jul 3, 2026 · N583UP · Boeing 7474R7F · Main Landing Gear
  > FOUND THE CORROSION ON INBD LOWER FITTING CAP AT RT BODY GEAR. IAW AMM 32-13-01-404-022 REV. 117 AND EI F2026A53M-1506 SEQUENCE A, PERFORMED INSTALL, LEAK CHECK OF HYDRAULIC HOSE CONNECTIONS, TEST AND SWING AT RIGHT BODY LANDING GEAR. CONDITION CHECKED NORM
- [SDR IPXA2026063066815](https://openairdocs.org/sdr/IPXA2026063066815.md): Strut · worn · Jun 26, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > FOUND RH WING OUTBD FLAP SUPPORT STRUT LOWER INSERT, COVE ATTACH WORN OUT, WBL 695. REVIEWED PER GMM-MTX 09.05.01.09. IAW CMM 57-52-55 601, REPAIR PARAGRAPH 1.F.(4), REV 212. REFER TO SRM 57-53-01-2R-1 AND SRM 51-70-07-0G-0 REV. 107 PERFORMED REPAIR.
- [SDR IPXA2026072970144](https://openairdocs.org/sdr/IPXA2026072970144.md): Splice Plate · cracked · Jun 26, 2026 · N583UP · Boeing 7474R7F · Wing Structure
  > DURING PERFORM EO-76733-JIC2 STEP 247, FOUND NR 2 FASTENER HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98163-REQ1 REV.1 AND EGAT EI F2026A57M-1371 REV 3.
- [SDR IPXA2026072970341](https://openairdocs.org/sdr/IPXA2026072970341.md): Skin · cracked · Jun 26, 2026 · N583UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > SKIN CRACKED AT BS 560, BELOW S26R. ACCOMPLISHED REPAIR I.A.W EO-98185-REQ1 REV.1 2
- [SDR IPXA2026072140524](https://openairdocs.org/sdr/IPXA2026072140524.md): Safety Net · frayed · Jun 25, 2026 · N583UP · Boeing 7474R7F · Emergency Equipment
  > FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. IAW AMM 52-32-00-410-801 REV.116 AND AMM 52-32-00-010-801 REV.116 REPLACED MAIN DECK SIDE CARGO DOOR SAFETY NET. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070540146](https://openairdocs.org/sdr/IPXA2026070540146.md): Seal · broken · Jun 25, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon, Main Frame
  > BROKEN SEAL, NR 3 PYLON 472HR PANEL. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED A NEW SEAL IAW SRM 51-40-02-0G, REV.107, AND DWG 65B90466, SH 2, REV D.
- [SDR IPXA2026062940524](https://openairdocs.org/sdr/IPXA2026062940524.md): Cargo Net · frayed · Jun 25, 2026 · N583UP · Boeing 7474R7F · Emergency Equipment
  > FOUND MAIN DECK SIDE CARGO DOOR SAFETY NET FRAYED. (REPLACE)
- [SDR IPXA2026070301653](https://openairdocs.org/sdr/IPXA2026070301653.md): Snubber · out of limits · Jun 23, 2026 · N583UP · Boeing 7474R7F · Passenger/Crew Doors
  > FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS. IAW AMM 52-11-10-004-001 REV.116 AND AMM 52-11-10-404-005 REV.116 REPLACED THE SNUBBER.
- [SDR IPXA2026062401653](https://openairdocs.org/sdr/IPXA2026062401653.md): Snubber · out of limits · Jun 23, 2026 · N583UP · Boeing 7474R7F · Passenger/Crew Doors
  > FOUND NR 1 MAIN ENTRY DOOR ROTARY SNUBBER OUT OF LIMITS.
- [SDR IPXA2026070183406](https://openairdocs.org/sdr/IPXA2026070183406.md): Skin · debonded · Jun 22, 2026 · N583UP · Boeing 7474R7F · Wing, Plate/Skin
  > DEBONDED SKIN, LOWER FACE OF LT WING NR 3 FLAP TRACK AFT FAIRING. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 107
- [SDR IPXA2026070183670](https://openairdocs.org/sdr/IPXA2026070183670.md): Door · chafed · Jun 22, 2026 · N583UP · Boeing 7474R7F · Engine Thrust Reverser
  > CHAFING- EDGE, NR 2 ENG RT T/R LOWER FORWARD DOOR AFT SIDE. INSTALLED NEW PARTS IAW SRM 51-40-02-0G REV.107 AND IPC 78-32-22 REV.96.
- [SDR IPXA2026062381206](https://openairdocs.org/sdr/IPXA2026062381206.md): Bracket · chafed · Jun 22, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFING - BRACKET, NR 1 ENG LT CORE COWL SUPPORT ROD SUPPORT FITTING. (REPLACE). INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47. REVIEWED TASK PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026071772387](https://openairdocs.org/sdr/IPXA2026071772387.md): Duct · cracked · Jun 21, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Structure
  > CRACKED DUCT, NR 1 ENG RT CORE COWL PRECOOLER EXHAUST DUCT. IAW AMM 71-11-06-004-001-J00, REV 117, AND AMM 71-11-06-404-006-J00, REV 117, REPLACED THE CORE COWL. COMPLETED THIS JOB AND CONDITION CHECK SATISFACTORY.
- [SDR IPXA2026063061139](https://openairdocs.org/sdr/IPXA2026063061139.md): Panel · eroded · Jun 20, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon, Plate/Skin
  > EROSION, L/E, NR 3 PYLON 471B PANEL. REMOVE THE ERODED MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( L: 3.5", W: 0.2", D: 1 PLY, AT L/E, 22" FROM INBD EDGE). APPLY ADHESIVE TO THE REPAIR AREA, CURED AT 80 F FOR 10 HOURS. I.A.W AMM 51-24-11-477-083 REV.11
- [SDR IPXA2026071961031](https://openairdocs.org/sdr/IPXA2026071961031.md): Bracket · cracked · Jun 20, 2026 · N583UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > CRACKED CLIP, RT BLG W/W FUILD TRANSFER ALT BRAKE SUPPORT ADJACENT KEEL BEAM AT STA 1394. (REPLACE) 1.REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.107 2.FABRICATE P/N(274U0001-5) PER BOEING DWG NO.274U0001 SH1 REV."C";PL REV."C" AND PSDL REV."-" AND ORIGIN
- [SDR IPXA2026063061135](https://openairdocs.org/sdr/IPXA2026063061135.md): Panel · eroded · Jun 20, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon, Plate/Skin
  > EROSION, L/E, NR 4 PYLON 481B PANEL. IAW SRM 54-51-70-1A-1 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW STEP: REMOVE THE ERODED MATERIALS AND CLEAN. APPLY ADHESIVE TO THE REPAIR AREA, CURED AT 80°F FOR 10 HOURS. CONDITION CHECK IS SATISFA
- [SDR IPXA2026062957241](https://openairdocs.org/sdr/IPXA2026062957241.md): Seal · damaged · Jun 20, 2026 · N583UP · Boeing 7474R7F · Leading Edge Devices
  > NR 26 V.C FLAP, OUTBOARD MOLDING SEAL DAMAGE. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.107 & CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026070240523](https://openairdocs.org/sdr/IPXA2026070240523.md): Support Bracket · cracked · Jun 19, 2026 · N583UP · Boeing 7474R7F · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, RT BLG W/W HYD TUBE SUPPORT BRACKET AT BS 1480 UNDER BLG HYD TRUCK POSITIONER SHUTOFF FUSE. REVIEWED TASK IAW GMM-MTX 09.05.01.09. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV.107, AND DWG 272U4448, SH 6, REV B.
- [SDR IPXA2026071124310](https://openairdocs.org/sdr/IPXA2026071124310.md): Skin · delaminated · Jun 18, 2026 · N583UP · Boeing 7474R7F · Wing, Plate/Skin
  > DELAMINATED SKIN, LOWER FACE OF LT WING INBD T/E CAVITY LOWER FIXED PANEL, WBL 294. I.A.W. AMM 20-51-01-912-008 REV.117 INSTALLED P-SEAL. CONDITION CHECK NORMAL.
- [SDR IPXA2026063024575](https://openairdocs.org/sdr/IPXA2026063024575.md): Tail Cone · debonded · Jun 18, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > NR 7 FLAP TRACK AFT TAIL CONE, LOWER SKIN FOUND TAPE APPLY. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA, IAW NDT MANUAL PART 1 51-01-01 REV:182. NO DEFECT WAS FOUND. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130
- [SDR IPXA2026070124788](https://openairdocs.org/sdr/IPXA2026070124788.md): Rub Strip · chafed · Jun 18, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFED RUB STRIP, NR 3 ENG LT CORE COWL T/E INNER UPPER SIDE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-23 REV.47
- [SDR IPXA2026070124731](https://openairdocs.org/sdr/IPXA2026070124731.md): Rub Strip · chafed · Jun 18, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFED RUB STRIP, NR 3 ENG RT CORE COWL INNER FACE AFT UPPER EDGE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-24 REV.50.
- [SDR IPXA2026070124595](https://openairdocs.org/sdr/IPXA2026070124595.md): Fairing · debonded · Jun 18, 2026 · N583UP · Boeing 7474R7F · Wing Miscellaneous Structure
  > DEBONDED SKIN, LOWER FACE OF LT WING NR 4 FLAP TRACK AFT FAIRING. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 107 CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026070124777](https://openairdocs.org/sdr/IPXA2026070124777.md): Rub Strip · chafed · Jun 18, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFED RUB STRIP, NR 3 ENG RT CORE COWL T/E INNER UPPER SIDE. INSTALLED NEW STRIP IAW SRM 51-40-02-0G, REV 107, AND CMM IPL 71-13-24, REV 50.
- [SDR IPXA2026063024753](https://openairdocs.org/sdr/IPXA2026063024753.md): Bracket · chafed · Jun 18, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFED BRACKET ASSY, NR 3 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND CMM IPL 71-13-24 REV.50 3.
- [SDR IPXA2026062525030](https://openairdocs.org/sdr/IPXA2026062525030.md): Bracket · chafed · Jun 18, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > FAULT- CHAFING- BRACKET ASSY, NO.3 ENG L/H CORE COWL HOLD OPEN ROD STOWAGE. (REPLACE). INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47. REVIEWED TASK PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026062923795](https://openairdocs.org/sdr/IPXA2026062923795.md): Seal · broken · Jun 18, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > BROKEN MOLDING SEAL, LT WING NR 3 V.C FLAP INBD SIDE CORD MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.
- [SDR IPXA2026062924546](https://openairdocs.org/sdr/IPXA2026062924546.md): Seal · damaged · Jun 18, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > NR 22 V.C FLAP INBOARD MOLDING SEAL DAMAGE. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR.
- [SDR IPXA2026062924655](https://openairdocs.org/sdr/IPXA2026062924655.md): Seal · broken · Jun 18, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > BROKEN- MOLDING SEAL, L/H WING NO.1E V.C FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR
- [SDR IPXA2026062924669](https://openairdocs.org/sdr/IPXA2026062924669.md): Seal · broken · Jun 18, 2026 · N583UP · Boeing 7474R7F · Trailing Edge Flaps
  > BROKEN- MOLDING SEAL, L/H WING NO.9 V.C FLAP INBD SIDE MOLDING. IAW. SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 159 PERFORM REPAIR AS BELOW. REMOVE THE RAIN EROSION SHIELDS AND CLEAN. APPLY THE SEALANT TO REPAIR AREA CURED AT 70 F FOR 48 HOURS
- [SDR IPXA2026072705515](https://openairdocs.org/sdr/IPXA2026072705515.md): Rub Strip · missing · Jun 17, 2026 · N583UP · Boeing 7474R7F · Cargo/Baggage Doors
  > FOUND FORWARD CARGO ACTUATOR ARM RUB STRIP MISSING AT FORWARD AND AFTER SIDE I.A.W UPS SREO NO: SREO-69479-REQ2 REV3 TO INSTALL RUB STRIP. REVIEWED PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026072010384](https://openairdocs.org/sdr/IPXA2026072010384.md): Bracket · broken · Jun 17, 2026 · N583UP · Boeing 7474R7F · Wing Miscellaneous Structure
  > BROKEN - BRACKET, LT WING INBD L/E CAVITY AIR DUCT LINK SUPPORT, ILES 1098 (REPLACE). IAW AMM 20-51-01-912-008 REV.117 INSTALLED LT WING L/E DUCT LINK ROD. CONDITION CHECK NORMAL.
- [SDR IPXA2026071706780](https://openairdocs.org/sdr/IPXA2026071706780.md): Bracket · cracked · Jun 17, 2026 · N583UP · Boeing 7474R7F · Engine Thrust Reverser
  > CRACKED DISCONNECT PANEL, NR 4 ENG R/H T/R FWD UPPER AREA. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107 2. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.107 AND AIPC 78-31-00-60 REV.61 AND SREO-62461-REQ1 REV.1 3.
- [SDR IPXA2026071106966](https://openairdocs.org/sdr/IPXA2026071106966.md): Skin · debonded · Jun 17, 2026 · N583UP · Boeing 7474R7F · Aerodynamic Fairings
  > DEBONDED SKIN, LT AFT WING TO BODY FAIRING 193 BL. IAW SRM 53-60-70-2R-0 REFER TO SRM 53-00-70-2R-1 AND SRM 51-70-07-0G-0 REV.107. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026071007466](https://openairdocs.org/sdr/IPXA2026071007466.md): Stiffener · cracked · Jun 17, 2026 · N583UP · Boeing 7474R7F · Engine Thrust Reverser
  > CRACKED BRACKET, NR. 4 ENG LT THRUST REVERSER TORQUE BOX AFT 10:00 POSITION. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.107. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G, REV.107 AND AIPC 78-31-00-55 REV 61.
- [SDR IPXA2026070110500](https://openairdocs.org/sdr/IPXA2026070110500.md): Rub Strip · chafed · Jun 17, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon Miscellaneous Structure
  > CHAFED RUB STRIP, NR 3 ENG LT CORE COWL INNER FACE AFT UPPER EDGE. INSTALLED NEW STRIP I.A.W SRM 51-40-02-0G REV.107 AND GOODRICH CMM IPL 71-13-23 REV.47
- [SDR IPXA2026072386960](https://openairdocs.org/sdr/IPXA2026072386960.md): Skin Panel · cracked · Jun 16, 2026 · N583UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACK NEAR STA 1810 S-26R. ACCOMPLISH THE REPAIR I.A.W SRM 53-60-01-02-3 REV.107 AND EGAT WORK SHEET NO.60486 AND EGAT EI NO.F2026A53M-1385 REV.3 AND EO-98148-REQ1 REV.1
- [SDR IPXA2026072348181](https://openairdocs.org/sdr/IPXA2026072348181.md): Web · corroded · Jun 13, 2026 · N583UP · Boeing 7474R7F · Fuel Storage
  > CORROSION, WEB OF CENTER WING TANK REAR SPAR NEAR JETTSION PUMP AT STA 1240 RBBL 93. (REPAIR) 1.PERFORMED EO-98103-REQ1 REV.1 AND EGAT EI NO.F2026A57M-1365 REV.1. 2.JOB COMPLETED AND ATTACHMENT ARE UPLOADED.
- [SDR IPXA2026062586867](https://openairdocs.org/sdr/IPXA2026062586867.md): Fairing · cracked · May 28, 2026 · N583UP · Boeing 7474R7F · Cargo/Baggage Doors
  > DURING PHASE 1A HARD LANDING INSPECTION NOTED POSSIBLE ISSUE -FORWARD LOWER CARGO DOOR TOP AFT CORNER REQUIRES -SHEET METAL EVALUATION. IAW AMM 52-34-01-004-001 REV.116 AND AMM 52-34-01-404-014 REV.116 REPLACE HINGE FAIRING AT FWD CARGO DOOR TOP AFT CORNER.
- [SDR IPXA2026070254508](https://openairdocs.org/sdr/IPXA2026070254508.md): Seal Depressor · broken · May 12, 2026 · N583UP · Boeing 7474R7F · Cargo/Baggage Doors
  > LOWER FORWARD CRG DOOR SEAL DEPRESSOR WITH MINOR DAMAGE. REVIEWED TASK PER GMM-MTX 09.05.01.09. INSTALLED NEW SEAL I.A.W SRM 51-40-02-0G REV.107 AND BOEING DWG NO: 65B04220 SH 2 REV.F.
- [SDR IPXA2026041766467](https://openairdocs.org/sdr/IPXA2026041766467.md): Inlet · cracked · Apr 12, 2026 · N583UP · Boeing 7474R7F · Engine Air Intake System
  > NR 2 ENGINE INLET COWL 12 O CLOCK POS. CRACK MEASURES 11IN DRILLED 4 EA. COUNTERSINK HOLES FOR HOIST SLING ATTACHMENT POINT PLUGS (BOLTS) I/A/W SRM 51-40-02. INLET SKIN SEALANT APPLIED I/A/W CMM 71-11-16.
- [SDR IPXA2026041366467](https://openairdocs.org/sdr/IPXA2026041366467.md): Cowling · cracked · Apr 12, 2026 · N583UP · Boeing 7474R7F · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE INLET COWL 12 O CLOCK POS. CRACK MEASURES 11IN PART IS ON TABLE IN S/M SHOP. BEGAN REMOVAL OF INLET LIP SKIN SECTION. ALL RIVETS REMOVED. SOME TOPSIDE HI-LOKS REMOVED (HAVE TO BE DRILLED). IAW SRM 51-40-02
- [SDR IPXA2026011254239](https://openairdocs.org/sdr/IPXA2026011254239.md): Floor Panel · damaged · Jan 5, 2026 · N583UP · Boeing 7474R7F · Fuselage Floor Panel
  > DURING WALKAROUND FOUND FLOOR PANEL NEAR 15L SPONGY. INSTALLED FLOOR PANEL REF AMM 53-21-02. REF GMM 04-02. PERFORMED A FINAL GVI FOR THE REPLACEMENT OF FLOOR PANEL 15L NO DEFECT NOTED. OK FOR RETURN TO SERVICE. C/W PER SREO-42648-REQ1 THIS CLEARS DEFERRAL
- [SDR IPXA2025102314177](https://openairdocs.org/sdr/IPXA2025102314177.md): Skin · cracked · Oct 17, 2025 · N583UP · Boeing 7474R7F · Fuselage Main, Plate/Skin
  > FOUND CRACK AT FORWARD LOWER CARGO DOOR CUTOUT AFT LOWER CORNER. C/W EO 95458-REQ1.
- [SDR IPXA2024123042606](https://openairdocs.org/sdr/IPXA2024123042606.md): Floor Panel · damaged · Dec 28, 2024 · N583UP · Boeing 7474R7F · Fuselage Floor Panel
  > FOUND FLOORBOARD ABOVE AFT EQUIPMENT COOLING FANS DAMAGED, APPROX STA 2270, LEFT OF CENTER, ROUTED TO SHEETMETAL. OKAY TO INSTALL FABRICATED FLOORBOARD LOCATED AROUND STA 2270. DONE PER GMM 04-02. INSTALLED FLOOROARD. REF AMM 53-21-02.
- [SDR IPXA2024082414905](https://openairdocs.org/sdr/IPXA2024082414905.md): Oil System · low pressure · Aug 23, 2024 · N583UP · Boeing 7474R7F · Turbine Engine Oil System
  > DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLUCTUATED BETWEEN 10-13 BEFORE STEADY RED WE SHU #4 ENGINE CHANGED.C/W MASTER CHIP DETECTOR INSPECTION REFER
- [SDR IPXA2024082314905](https://openairdocs.org/sdr/IPXA2024082314905.md): Indication Sys · false indication · Aug 23, 2024 · N583UP · Boeing 7474R7F · Turbine Engine Oil System
  > OPEN, DURING CRUISE FLIGHT #4 ENG. OIL QUANITY DROPPED TO ZERO. OVER THE NEXT 20 MINUTES THE OIL PRESSURE DROPPED STEADILY REACHIMG 10 PSI(RED ZONE) THEN IT FLUCTUATED BETWEEN 10-13 BEFORE STEADY RED WE SHU C/W MASTER CHIP DETECTOR INSPECTION REFERENCE: TASK

Next page: https://openairdocs.org/aircraft/N583UP/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 = 'N583UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N583UP/reports

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