# Service difficulty reports: N575UP

A list on [N575UP](https://openairdocs.org/aircraft/N575UP.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 6 · 252 reports

- [SDR IPXA2026102153875](https://openairdocs.org/sdr/IPXA2026102153875.md): Window · cracked · Oct 21, 2026 · N575UP · Boeing 74744AF · Flight Compartment Windows
  > ARRIVAL FOUND L1 WINDOW CRACK.
- [SDR IPXA2026042797242](https://openairdocs.org/sdr/IPXA2026042797242.md): Adapter · corroded · Apr 27, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > ADDITION SDR AND CPCP FOR SATELLITE COMMUNICATIONS (SATCOM) SYSTEM [T3F18E0082B65]. REVIEWED PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026042329452](https://openairdocs.org/sdr/IPXA2026042329452.md): Bolt · worn · Apr 16, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flaps
  > RIGHT WING OUTBOARD MID FLAP, T/E UPPER SKIN, BOLT WORN 1 EA. REMOVE THE WORN MATERIALS AND CLEAN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. AND PSDL 65B08533 SHEET DL, REV.A. INSTALL THE RH WING OUTBD MID FLAP SUPPORT STRUT.
- [SDR IPXA2026042187945](https://openairdocs.org/sdr/IPXA2026042187945.md): Fairing · damaged · Apr 14, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flaps
  > ENLARGED HOLE NR 4 AFT FAIRING HOLE.IAW AMM 51-24-11-477-083 REV.116, REPAINT PEEL OFF AREA. CHECK NORMAL.
- [SDR IPXA2026042571341](https://openairdocs.org/sdr/IPXA2026042571341.md): Angle · cracked · Apr 13, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage Doors
  > FOUND MAIN DECK SIDE CARGO DOOR ANGLE ASSY DAMAGE. IAW SRM 51-40-02-0G REV.106. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV.106, AND DWG 65B57353, SH 2, REV G, INSTALLED NEW CLIP.
- [SDR IPXA2026042162642](https://openairdocs.org/sdr/IPXA2026042162642.md): Fitting · chafed · Apr 12, 2026 · N575UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > FOUND L1 ENTRY DOOR CUTOUT AFT LOWER FITTING CHAFING. REQUEST PERFORM OK TO CLOSE CHECK FOR L1 DOOR AFT SIDE LOWER SIDEWALL PANEL.
- [SDR IPXA2026041750112](https://openairdocs.org/sdr/IPXA2026041750112.md): Seal · broken · Apr 11, 2026 · N575UP · Boeing 74744AF · Fuselage Main, Structure
  > BROKEN SEAL, LT WING LANDING GEAR W/W CUTOUT FWD LWR SEAL. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE SEAL IAW SRM 51-40-02-0G REV. 106 AND DWG 65B10555, SH 3, REV G INSTALLED NEW SEAL.
- [SDR IPXA2026042047400](https://openairdocs.org/sdr/IPXA2026042047400.md): Rub Strip · chafed · Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > CHAFED STRIP, NR 2 ENGINE LT CORE COWL INNER AFT UPPER AREA. IAW AMM 71-11-06-004-001-J00, REV 116. REMOVED THE CORE COWL. IAW SRM 51-40-02-0G, REV. 106, REMOVED DAMAGE STRIP IAW SRM 51-40-02-0G, REV 106, AND CMM IPL 71-13-23, REV 47. INSTALLED NEW STRIP I
- [SDR IPXA2026042547996](https://openairdocs.org/sdr/IPXA2026042547996.md): Tube · worn · Apr 11, 2026 · N575UP · Boeing 74744AF · Hydraulic System, Main
  > WORN FLARED TUBE OF ENG-1 ADP. I.A.W.AMM 29-11-15-002-001 REV116 AND AMM29-11-15-402-009, REV 116. REPLACED THE SPEED CONTROL AIR PRESSURE LINE
- [SDR IPXA2026042447341](https://openairdocs.org/sdr/IPXA2026042447341.md): Retainer · cracked · Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACKED RETAINER, NR 2 ENG RT T/R TRANSLATING COWL UPPER TEE TRACK HINGE PIN CRACKED. IAW AMM 70-50-00-912-034, REV 116 REPLACED THE RETAINER.
- [SDR IPXA2026042046129](https://openairdocs.org/sdr/IPXA2026042046129.md): Rub Strip · broken · Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > NO. 2 ENG NOSE COWL AFT FLANGE WEAR STRIP, AT 6 O'CLOCK POSITION. I.A.W SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-11-16 REV.54 INSTALLED NEW STRIP.
- [SDR IPXA2026042147492](https://openairdocs.org/sdr/IPXA2026042147492.md): Seal · frayed · Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > FRAYED SEAL, NR 1 PYLON OTBD AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106, REMOVED DAMAGE SEAL. IAW GMM-MTX 9.08, REV 15, REQUIREMENT AND EGAT WORK SHEET 60275 AND DWG 323U2325, SH 11, REV A. DWG 323U2325-153, PL, REV A, AND ORIGINAL PART AS
- [SDR IPXA2026042150427](https://openairdocs.org/sdr/IPXA2026042150427.md): Angle · cracked · Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACKED ANGLE, NR 4 ENG RT THRUST REVERSER DRIAN TUBE SUPPORT CLAMP. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE ANGLE. IAW SRM 51-40-02-0G, REV 106, & IPC 78-32-52, REV 96. INSTALLED NEW ANGLE.
- [SDR IPXA2026042047446](https://openairdocs.org/sdr/IPXA2026042047446.md): Seal · broken · Apr 11, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > BROKEN SEAL, NR 4 PYLON LT AFT FAIRING DOOR LWR SEAL. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE SEAL. IAW GMM-MTX CH 9.08, REV 15 REQUIREMENT AND EGAT WORK SHEET 60267 AND DWG 323U2325, SH 11, REV A, DWG 323U2325-153, PL REV A, AND ORIGINAL PART AS A SAM
- [SDR IPXA2026041649774](https://openairdocs.org/sdr/IPXA2026041649774.md): Scoop · damaged · Apr 11, 2026 · N575UP · Boeing 74744AF · Wing Main, Frame Structure
  > ENLARGED HOLE, LT WING OUTBD LOWER FUEL VENT SCOOP PANEL FWD FASTENER HOLE. IAW DWG 112U0700, SHEET 01, REV D. REMOVED LT WING FUEL VENT SCOOP PANEL IAW DWG 112U0700, SHEET 01, REV. D. INSTALLED LT WING FUEL VENT SCOOP PANEL.
- [SDR IPXA2026041547552](https://openairdocs.org/sdr/IPXA2026041547552.md): Bracket · chafed · Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG LT T/R LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-21 REV. 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026041547525](https://openairdocs.org/sdr/IPXA2026041547525.md): Bracket · chafed · Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 1 ENG RT THRUST REVERSER LWR FWD CLOSURE DOOR T/E AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE BRACKET. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026041547574](https://openairdocs.org/sdr/IPXA2026041547574.md): Bracket · chafed · Apr 11, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CHAFED BRACKET, NR 2 ENG RT THRUST REVERSER FWD LWR CLOSURE DOOR T/E AREA. IAW SRM 51-40-02-0G, REV 106 REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106 & IPC 78-32-22 REV. 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026042128355](https://openairdocs.org/sdr/IPXA2026042128355.md): Seal · broken · Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > BROKEN SEAL, NR 3 ENG, LT THRUST REVERSER AFT LWR AREA. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21 REV. 96, INSTALLED NEW SEAL.
- [SDR IPXA2026042028336](https://openairdocs.org/sdr/IPXA2026042028336.md): Bracket · cracked · Apr 10, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACKED BRACKET, NR 3 ENG LT THRUST REVERSER HINGE PANEL SUPPORT BRACKET. IAW SRM 51-40-02-0G, REV 106. REMOVED DAMAGE BRACKET. IAW SRM 51-40-02-0G, REV 106, AND IPC 78-32-21, REV 96 INSTALLED NEW BRACKET.
- [SDR IPXA2026042711816](https://openairdocs.org/sdr/IPXA2026042711816.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap Actuator
  > FAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 INBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5385. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP INBD'S OUTBD ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACC
- [SDR IPXA2026042711853](https://openairdocs.org/sdr/IPXA2026042711853.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap Actuator
  > FAULT - R/H WING L/E VARIABLE CAMBER FLAP #17 OTBD ROTARY ACTUATOR HAS CRACKED OTBD COVER. NO.5311. I.A.W AMM 27-81-07-004-001 REV 116 REMOVE NO.17 V.C FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2).(P) TO STEP 3.G.(2) ACCOMPLISHED THE I
- [SDR IPXA2026042711764](https://openairdocs.org/sdr/IPXA2026042711764.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap Actuator
  > LT WING L/E VARIABLE CAMBER FLAP NR 2 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001 REV 116 REMOVE NR 2 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV.116, STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND ADJUST
- [SDR IPXA2026042713748](https://openairdocs.org/sdr/IPXA2026042713748.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap Actuator
  > RIGHT WING L/E VARIABLE CAMBER FLAP 24 ROTARY ACTUATOR AT HAS CRACKED COVER. IAW AMM 27-81-07-004-001, REV 116. REMOVE 24 V.C FLAP ROTARY ACTUATOR. IAW AMM 27-81-07-404-008, REV 116. STEP 3.F.(2).(P) TO STEP 3.G.(2). ACCOMPLISHED THE INSTALLATION AND A
- [SDR IPXA2026042711916](https://openairdocs.org/sdr/IPXA2026042711916.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flap Actuator
  > LEFT WING LE VARIABLE CAMBER FLAP NR 5, ROTARY ACTUATOR AT HAS CRACKED COVER. 5386. IAW AMM 27-81-07-004-001, REV 116. REMOVED NR 5 VC FLAP ROTARY ACTUATOR. I.A.W AMM 27-81-07-404-008 REV.116 STEP 3.F.(2). P TO STEP 3.G. (2). ACCOMPLISHED THE INSTALLATION AN
- [SDR IPXA2026042411547](https://openairdocs.org/sdr/IPXA2026042411547.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACK- COVER, NO.4 ENG R/H T/R ACTUATOR ACCESS PNL 446B, 446C, 445C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 446B 446C 445C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 446B 446C 445C WITH NEW.
- [SDR IPXA2026042411487](https://openairdocs.org/sdr/IPXA2026042411487.md): Cover · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACK- COVER, NO.3 ENG R/H T/R ACTUATOR ACCESS PNL 436B, 436C. I.A.W.AMM 78-31-10-004-001-J00 REV116 REMOVED THE PANEL 436B 436C. I.A.W.AMM 78-31-10-404-008-J00 REV116 INSTALLED THE PANEL 436B 436C WITH NEW.
- [SDR IPXA2026042014756](https://openairdocs.org/sdr/IPXA2026042014756.md): Rub Strip · chafed · Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > CHAFED RUB STRIP, NR 3 ENG RT CORE COWL AFT UPR RUB STRIP. I.A.W SRM 51-40-02-0G REV. 106 AND CMM IPL 71-13-24 REV.50 INSTALLED NEW STRIP.
- [SDR IPXA2026042114858](https://openairdocs.org/sdr/IPXA2026042114858.md): Seal · broken · Apr 9, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > BROKEN - SEAL, NR 4 ENG RT T/R CLOSURE DOOR FWD AREA. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE SEAL. I.A.W SRM 51-40-02-0G REV. 106 AND ST ENGINEERING IPC 78-32-22 REV. 96 INSTALLED NEW SEAL.
- [SDR IPXA2026042014715](https://openairdocs.org/sdr/IPXA2026042014715.md): Rub Strip · chafed · Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > CHAFING AND MISSING - STRIP AND RIVET, NO.3 ENG L/H CORE COWL AFT UPR WEAR STRIP. IAW SRM 51-40-02-0G REV. 106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-23 REV.47 INSTALLED NEW STRIP.
- [SDR IPXA2026042315124](https://openairdocs.org/sdr/IPXA2026042315124.md): Nose Cowl · dented · Apr 9, 2026 · N575UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > DENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 2:00 POS. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.4", 5.5" FROM AFT EDGE, 59.5" FROM LWR EDGE, AT 2 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE CURED
- [SDR IPXA2026042214799](https://openairdocs.org/sdr/IPXA2026042214799.md): Seal Depressor · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Cargo/Baggage Doors
  > CRACKED DEPRESSURE SEAL, AFT CARGO DOOR CUTOUT AFT SIDE. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE DRPRESSOR SEAL AND DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B01865 SH10 REV E AND BOEING DWG NO.65B06880 SH2 REV B INSTALL NEW DRPRESSOR
- [SDR IPXA2026041815210](https://openairdocs.org/sdr/IPXA2026041815210.md): Fairing · dented · Apr 9, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flaps
  > DENTED SKIN, LT WING T/E FLAP NR 4 AFT FAIRING EXTERNAL SURFACE LOWER SIDE ADJACENT AFT CONE. IAW SRM 57-53-70-2R-1 REFER TO SRM 51-70-17-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN C
- [SDR IPXA2026041811914](https://openairdocs.org/sdr/IPXA2026041811914.md): Skin · cracked · Apr 9, 2026 · N575UP · Boeing 74744AF · Wing, Plate/Skin
  > RIGHT WING INBOARD T/E UPPER FIXED PANEL SKIN CRACK, WBL 235.2. I.A.W. 747-400F SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV. 106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 26
- [SDR IPXA2026041214960](https://openairdocs.org/sdr/IPXA2026041214960.md): Floorboard · damaged · Apr 9, 2026 · N575UP · Boeing 74744AF · Fuselage Floor Panel
  > MAJOR REPAIR. DAMAGED FLOORBOARD ON RT MAIN CARGO DECK BS 1220. REMOVE THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53-21-02. INSTALL THE REPLACEMENT FLOOR PANEL PER AMM 53-21-02.
- [SDR IPXA2026042573876](https://openairdocs.org/sdr/IPXA2026042573876.md): Panel · broken · Apr 7, 2026 · N575UP · Boeing 74744AF · Cargo Compartments
  > FWD CARGO COMPARTMENT CEILING PANEL ASSY ZIPPER BROKEN AT STA 840 - 860..I.A.W AMM25-52-01-004-049 REV116 AND I.A.W AMM25-52-01-404-062 REV116 REPLACE PANEL ASSY WITH NEW PARTS.
- [SDR IPXA2026042355538](https://openairdocs.org/sdr/IPXA2026042355538.md): Support · worn · Apr 6, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous Structure
  > FOUND LT WING OTBD FLAP NR 7 SUPPORT STRUT (OTBD TO INBD) UPPER AND LOWER PANEL WORN. I.A.W DWG 65B08533, SHEET 3, ZONE C12, VIEW 2B6, REV.C. REMOVED THE LH WING OUTBD FLAP NO.7 SUPPORT STRUT (OUTBD TO INBD). FAULT- FOUND LH WING OUTBD FLAP NO.7 SUPPORT STRUT
- [SDR IPXA2026042634350](https://openairdocs.org/sdr/IPXA2026042634350.md): Clamp · cracked · Apr 4, 2026 · N575UP · Boeing 74744AF · APU Bleed Air System
  > CRACKED CLAMP - APU ACOC COOLING DUCT. I.A.W.AMM 49-51-04-004-001 REV116 AND AMM 49-51-04-404-011 REV116 REPLACED THE CLAMP WITH NEW.
- [SDR IPXA2026042119204](https://openairdocs.org/sdr/IPXA2026042119204.md): Skin · damaged · Apr 3, 2026 · N575UP · Boeing 74744AF · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE- SKIN, RT NOSE AREA (ABOVE UPS LOGO) SUSPECTED LIGHTENING STRIKE ON FASTENER. BLEND OUT THE DAMAGE AREA I.A.W SRM 51-10-02-0G REV.106. ACCOMPLISHMENT LIGHTNING STRIKE REPAIR I.A.W UPS EO-97134-REQ1 REV.1.
- [SDR IPXA2026042072963](https://openairdocs.org/sdr/IPXA2026042072963.md): Ring · cracked · Apr 1, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > CRACKED ACSR-ON ENG-2, R/H THRUST REVERSER HALF. IAW AMM 78-31-01-004-001-J00 REV 116 REMOVED THE T/R HALF. RII NO.2 ENG R/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.
- [SDR IPXA2026042075055](https://openairdocs.org/sdr/IPXA2026042075055.md): Fitting · cracked · Apr 1, 2026 · N575UP · Boeing 74744AF · Engine Thrust Reverser
  > FND 3L T/R AGB FITTING CRACK AT 7 O'CLOCK POSITION. I.A.W. AMM 78-31-01-004-001-J00 REV116 REMOVED THE T/R HALF. I.A.W SRM 51-40-02-0G REV.106 REMOVE DAMAGE AGB FITTING. RII NO.3 ENG L/H THRUST REVERSER HALF OK TO INSTALLED CHECKED OK AND INSTALLED CHECKED OK.
- [SDR IPXA2026041557453](https://openairdocs.org/sdr/IPXA2026041557453.md): Angle · cracked · Mar 31, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous Structure
  > DURING PERFORMANCE OF EO-95214-JIC2, FOUND RT WING LG SHOCK STRUT DOOR FAIRING SEAL DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 REMOVED DAMAGE DEPRESSOR. I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B11675 SH. 2 REV. G INSTALLED NEW DEPRESSOR.
- [SDR IPXA2026041557510](https://openairdocs.org/sdr/IPXA2026041557510.md): Angle · cracked · Mar 31, 2026 · N575UP · Boeing 74744AF · Wing Miscellaneous Structure
  > DURING PERFORM EO-95214-JIC2, FOUND RT WING SHOCK STRUT DOOR FAIRING CLIP CRACKED. I.A.W SRM 51-40-02-0G REV. 106 REMOVED DAMAGE CLIP. I.A.W SRM 51-40-02-0G REV. 106 AND BOEING DWG NO: 65B11675 SHEET 1 REV. K INSTALLED FABRICATED CLIP.
- [SDR IPXA2026040554363](https://openairdocs.org/sdr/IPXA2026040554363.md): Fairing · punctured · Mar 6, 2026 · N575UP · Boeing 74744AF · Trailing Edge Flaps
  > PUNCTURE IN FWD OTBD AREA OF #1 MOVEABLE FLAP TRACK FAIRING. I.A.W. 747-400F SRM 57-53-70-2R-1 REFER TO SRM 51-70-07-0G-0 REV.106 PERFORM REPAIR AS BELOW STEP: 1.1 REMOVE THE PUNCTURE MATERIALS AND CLEAN. 1.2 MEASURE THE DAMAGE AREA (DIA:1", 2.5" FROM THE PA
- [SDR IPXA2026030919342](https://openairdocs.org/sdr/IPXA2026030919342.md): Floorboard · worn · Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Floor Panel
  > MAJOR REPAIR, FLOORBOARD INSIDE L1 DOOR THRESHOLD IS WORN AND IS SHOWING CORE MATERIAL. INSTALLED NEW FLOORBOARD INSIDE L1 DOOR THRESHOLD IAW AMM 53-21-02.
- [SDR IPXA2026030908993](https://openairdocs.org/sdr/IPXA2026030908993.md): Door Frame · damaged · Mar 4, 2026 · N575UP · Boeing 74744AF · Fuselage Main, Structure
  > FOUND DAMAGE ON UNDERLYING STRUCTURE BEHIND SEAL DEPRESSOR SPLICE AT FS 615 APPROX WL 170. ALL STEPS ARE COMPLETE EO-96726-REQ1.
- [SDR IPXA2026041369914](https://openairdocs.org/sdr/IPXA2026041369914.md): Skin · dented · Mar 1, 2026 · N575UP · Boeing 74744AF · Leading Edge Devices
  > NR 25 VCF HAS DENT ON LEADING INB END RII COMPLETED STEP 13 I.A.W AMM 27-81-02-404-010 REV.116 ASSEMBLY THE NR 26 FOLDING NOSE AND INSTALLED THE NR 26 V.C FLAP CHECK OK. ACCOMPLISHED REPAIR I.A.W EGAT WORK SHEET NO.60222 AND SRM 57-43-02-2R-2 REPAIR2 REV.106
- [SDR IPXA2024052554554](https://openairdocs.org/sdr/IPXA2024052554554.md): Battery · inoperative · May 19, 2024 · N575UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE L1 DOOR EMERGENCY LIGHT INOP. REPLACED THE EMERGENCY LIGHT BATTERY (M5170) AT UPPER DECK (STA550 WL323 LBL83)I.A.W AMM 33-51-04-902-001-001 REV.110 AND SSM 33-51-01 REV.44
- [SDR IPXA2024052554537](https://openairdocs.org/sdr/IPXA2024052554537.md): Battery · inoperative · May 19, 2024 · N575UP · Boeing 74744AF · Emergency Lighting
  > FAULT - FOUND THE EMERGENCY EXIT SIGN LIGHT INOP AT UPPER DECK STA 410. (REPLACE).I.A.W AMM 33-51-04-902-001-001 REV.110 AND SSM 33-51-01 REV.44 REPLACED THE EMERGENCY LIGHT BATTERY (M5169) AT UPPER DECK (STA590 WL323 RBL83). REVIEW COMPLETED
- [SDR IPXA2024052054554](https://openairdocs.org/sdr/IPXA2024052054554.md): Light · inoperative · May 19, 2024 · N575UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE L1 DOOR EMERGENCY LIGHT INOP. (REPLACE) OK TO WORK

Next page: https://openairdocs.org/aircraft/N575UP/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 = 'N575UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N575UP/reports

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