# Service difficulty reports: N572UP

A list on [N572UP](https://openairdocs.org/aircraft/N572UP.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 4 · 181 reports

- [SDR IPXA2026080575871](https://openairdocs.org/sdr/IPXA2026080575871.md): Battery · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOP. IAW SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK AISLE EMERGENCY LIGHT SYSTEM CHECK, FOUND THE EMERGENCY LIGHT BATTERY M5168 FUNCTION FAIL. IAW AMM 33-51-04-902-001-001, REV.117. REPLACED THE EMERGENCY LIGH
- [SDR IPXA2026080575748](https://openairdocs.org/sdr/IPXA2026080575748.md): Battery · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. I.A.W SSM 33-51-01 REV.47 PERFORMED THE UPPER DECK EMERGENCY EXIT SIGN LIGHT SYSTEM CHECK, FOUND THE EMERGENCY LIGHT BATTERY M5169 FUNCTION FAIL. I.A.W AMM 33-51-04-902-001-001 REV.117 REPLACED THE EMERGEN
- [SDR IPXA2026080375748](https://openairdocs.org/sdr/IPXA2026080375748.md): Light · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP. (REPLACE)
- [SDR IPXA2026080375871](https://openairdocs.org/sdr/IPXA2026080375871.md): Light · inoperative · Aug 2, 2026 · N572UP · Boeing 74744AF · Emergency Lighting
  > FOUND THE UPPER DECK AISLE EMERGENCY LIGHT INOPERATIVE. (REPLACE)
- [SDR IPXA2026070878270](https://openairdocs.org/sdr/IPXA2026070878270.md): Flap · cracked · Jul 3, 2026 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > FOUND RT WING OUTBD AFT FLAP INBD SIDE BOTTOM SURFACE CRACK. PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2 INCHES AROUND HEATED AREA,PER 747 NDT MANUAL PART 1 51-01-01 REV:183 RESULT:NO DEFECT WAS FOUND. IAW AMM 51-24-11-477-083, REV 116, REPAINT PEEL OFF
- [SDR IPXA2026071560216](https://openairdocs.org/sdr/IPXA2026071560216.md): Skin · cracked · Jul 2, 2026 · N572UP · Boeing 74744AF · Nacelle/Pylon, Plate/Skin
  > CRACKED SKIN, NR 4 PYLON R/H FAIRING DOOR L/E AREA. I.A.W.AMM 54-62-03-404-005 REV117 INSTALLED NO.4 PYLON R/H FAIRING DOOR.
- [SDR IPXA2026070759188](https://openairdocs.org/sdr/IPXA2026070759188.md): Cowling · dented · Jul 2, 2026 · N572UP · Boeing 74744AF · Nacelle/Pylon, Main Frame
  > DENTED SKIN, NR 2 ENG NOSE COWL INLET AT 10 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA: 0.5", 12.8" FROM AFT EDGE, 51.7" FROM LWR EDGE, AT 10 O'CLOCK ON THE ACOUSTIC PNL OF NO.2 ENG INLET COWL). FILL THE CUT OUT WITH ADHESIVE C
- [SDR IPXA2026070724623](https://openairdocs.org/sdr/IPXA2026070724623.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 11 KRUEGER FLAP INBD SIDE MOLDING. CHECKED OK.
- [SDR IPXA2026070921962](https://openairdocs.org/sdr/IPXA2026070921962.md): Web · corroded · Jun 30, 2026 · N572UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > CORRODED UPPER DECK FLOOR PNL WEB AT BS 480 - 520, LBL 10 - RBL 40 CORRODED. INSTALLED A NEW WEB IAW SRM 51-40-02-0G, REV 107.
- [SDR IPXA2026070724617](https://openairdocs.org/sdr/IPXA2026070724617.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 6 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR
- [SDR IPXA2026070624604](https://openairdocs.org/sdr/IPXA2026070624604.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 3 VC FLAP INBD SIDE, IAW SRM 57-43-02-2R-5 REV. 107 REFER TO SOPM 20-50-12 REV. 160 PERFORM REPAIR.
- [SDR IPXA2026070624589](https://openairdocs.org/sdr/IPXA2026070624589.md): Seal · broken · Jun 30, 2026 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > BROKEN MOLDING SEAL, LT WING NR 2 VC FLAP INBD SIDE. REMOVED THE RAIN EROSION SHIELDS AND CLEANED. APPLY THE SEALANT TO REPAIR AREA.
- [SDR IPXA2026070324858](https://openairdocs.org/sdr/IPXA2026070324858.md): Skin · damaged · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > ABRADED SKIN, UPPER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR, PANEL 521BB, IAW AMM 52-49-09-402-003, REV 116. INSTALLED REFUELING PANEL 521BB. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070420634](https://openairdocs.org/sdr/IPXA2026070420634.md): Fairing · debonded · Jun 30, 2026 · N572UP · Boeing 74744AF · Aerodynamic Fairings
  > DEBONDED PANEL, AFT WING TO BODY FAIRING PANEL 193CL EXTERNAL SURFACE. IAW AMM 20-51-01-912-008 REV.116 INSTALL PANEL 193CL. CONDITION CHECK NORMAL.
- [SDR IPXA2026070524776](https://openairdocs.org/sdr/IPXA2026070524776.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING T/E NEAR INBD AILERON PANEL 673AB. IAW SRM 57-51-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.107 PERFORM REPAIR AS BELOW STEP: REMOVE THE DAMAGE MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (L:0.38", W:0.28", 11" FROM INBD EDGE,AT PNL AFT ED
- [SDR IPXA2026070324807](https://openairdocs.org/sdr/IPXA2026070324807.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING T/E NEAR INBD AILERON 673CB. IAW AMM 20-51-01-912-008 REV. 116 INSTALLED THE ACCESS PANEL 673CB. CONDITION CHECKED NORMAL.
- [SDR IPXA2026070624831](https://openairdocs.org/sdr/IPXA2026070624831.md): Skin · cracked · Jun 30, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, LOWER FACE OF LT WING INBD L/E REFUELING STATION LOWER DOOR CUTOUT, ILES 845. IAW AMM 52-49-09-402-003, REV. 116. INSTALLED REFUELING PANEL NO. 521CB. 2. CONDITION CHECK NORMAL. ATTACHMENT ARE UPLOADED.
- [SDR IPXA2026073009895](https://openairdocs.org/sdr/IPXA2026073009895.md): Web · cracked · Jun 29, 2026 · N572UP · Boeing 74744AF · Wing Miscellaneous Structure
  > SURFACE & HOLE CRACK INDICATION, DURING PFM SB 747-57A2357 FND SURFACE & HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98227-REQ1, REV 1, & EGAT EI F2026A57M-1427, REV 4.
- [SDR IPXA2026072111084](https://openairdocs.org/sdr/IPXA2026072111084.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF · Vertical Stabilizer, Plate/Skin
  > DEBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322BL. REPAIR DISBOND ON PANEL ASSY OF VST FWD TORQUE BOX BETWEEN STA 2365 AND STA 2413 I.A.W. EGAT EI F2026A55M-1378 REV.1 AND UPS EO-98179-REQ1 REV.1 2. CONDITION CHECK IS SATISFACTORY.
- [SDR IPXA2026072111043](https://openairdocs.org/sdr/IPXA2026072111043.md): Panel · debonded · Jun 29, 2026 · N572UP · Boeing 74744AF · Vertical Stabilizer, Plate/Skin
  > DISBONDED PANEL, VERTICAL STABILIZER LOWER PANEL 322CL. REPAIR DISBOND DAMAGE ON LH FWD LWR VST FORWARD TORQUE BOX PANEL BETWEEN STA 2285 AND 2365 AND BETWEEN FIN WL10 AND 25 I.A.W. EGAT EI NO. F2026A55M-1379 REV. 1 AND UPS EO-98180-REQ1 REV. 2
- [SDR IPXA2026070697892](https://openairdocs.org/sdr/IPXA2026070697892.md): Seal · broken · Jun 28, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, L/H WING NR 4 VC FLAP INBD SIDE MOLDING. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12 REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED.APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.
- [SDR IPXA2026070697902](https://openairdocs.org/sdr/IPXA2026070697902.md): Seal · broken · Jun 28, 2026 · N572UP · Boeing 74744AF · Leading Edge Devices
  > BROKEN MOLDING SEAL, LT WING NR 5 VC FLAP INBD SIDE. IAW SRM 57-43-02-2R-5, REV 107, REFER TO SOPM 20-50-12, REV 160. PERFORMED A REPAIR, REMOVED THE RAIN EROSION SHIELDS AND CLEANED, APPLY THE SEALANT TO REPAIR AREA. CONDITION CHECKED SATISFACTORY.
- [SDR IPXA2026072186856](https://openairdocs.org/sdr/IPXA2026072186856.md): Seal · damaged · Jun 27, 2026 · N572UP · Boeing 74744AF · Passenger/Crew Doors
  > FOUND NR 1 ENTRY DOOR LOWER SEAL DAMAGED. IAW AMM 52-09-00-308-001, REV.116. REPLACED NR 1 ENTRY DOOR LOWER SEAL. CONDITION CHECK NORMAL.
- [SDR IPXA2026071085535](https://openairdocs.org/sdr/IPXA2026071085535.md): Skin · broken · Jun 27, 2026 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > CRACKED SKIN, RT WING L/E NR 23 V.C FLAP INBD LWR. ACCOMPLISHED JOB IAW EO-97981-REQ1, REV1 AND EGAT EI F2026A57M-1340. ACCOMPLISHED JOB I.A.W UPS EO-97981-REQ1 REV2 AND EGAT EI NO. F2026A57M-1340, REV.0 AND REV.1.
- [SDR IPXA2026062986856](https://openairdocs.org/sdr/IPXA2026062986856.md): Seal · damaged · Jun 27, 2026 · N572UP · Boeing 74744AF · Passenger/Crew Doors
  > FOUND NO.1 ENTRY DOOR LOWER SEAL DAMAGED
- [SDR IPXA2026073003261](https://openairdocs.org/sdr/IPXA2026073003261.md): Stiffener · worn · May 28, 2026 · N572UP · Boeing 74744AF · Fuselage Miscellaneous Structure
  > MAJOR REPAIR, SUPPORT ROD INSIDE FUELING PANEL STATION AFT ATTACH BOLT HOLE IS ELONGATED AND ATTACH ANGLE IS WORN. ACCOMPLISH THE REPAIR IAW EO-97627-REQ2 REV1 AND EGAT EI F2026A57M-1357, REVISION 1. REFER TO DAMAGE REPORT FOR THE ORIGINAL MATERIAL & THICK
- [SDR IPXA2026060120516](https://openairdocs.org/sdr/IPXA2026060120516.md): Fuel Sys · out of balance · May 11, 2026 · N572UP · Boeing 74744AF · Aircraft Fuel Distribution System
  > AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG2 PUMPS. REMOVED AND REPLACED MAIN 2 AFT BOOST PUMP REF AMM 28-22-
- [SDR IPXA2026051220516](https://openairdocs.org/sdr/IPXA2026051220516.md): Transfer Sys · malfunctioned · May 11, 2026 · N572UP · Boeing 74744AF · Aircraft Fuel Distribution System
  > AFTER LEVEL OFF ENG 3 FUEL INDICATED 2,000LBS LESS THAN ENG 2. WE BALANCED THE FUEL MANUALLY BUT HAD TO CONTINUE TO BALANCE THE FUEL THE ENTIRE FLIGHT. SUSPECT ENG 3 PUMPS ARE STRONGER THAN ENG 2 PUMPS DEFERRED IAW EO-97441.
- [SDR IPXA2026041322009](https://openairdocs.org/sdr/IPXA2026041322009.md): Window · cracked · Apr 9, 2026 · N572UP · Boeing 74744AF · Flight Compartment Windows
  > AT FL 370 FWD WINDOW LEFT CRACKED. R & R L1 WINDOW IAW AMM 56-11-01/401. REPLACED WINDOW HEAT CONTROL UNIT IAW AMM 30-41-01/401. OPS CHKD WINDSHIED HEATER SYS AND WIPER IAW AMM 30-41-00/501 & 30-42-00/501, CHKD NORMAL, AIRCRAFT OK FOR SERVICE.
- [SDR IPXA2026041022009](https://openairdocs.org/sdr/IPXA2026041022009.md): Window · cracked · Apr 9, 2026 · N572UP · Boeing 74744AF · Flight Compartment Windows
  > AT FL 370, FWD WINDOW LEFT CRACKED
- [SDR IPXA2026012682273](https://openairdocs.org/sdr/IPXA2026012682273.md): Start Valve · faulted · Jan 26, 2026 · N572UP · Boeing 74744AF · Engine Start Valves/Controls
  > AIR TURN BACK, NR 3 STARTER CUTOUT EICAS MESSAGE IN CLIMB, CONTINUED THROUGH FLIGHT. QRH PROCEDURE FOLLOWED. R & R NR 3 ENG START VALVE IAW AMM 80-11-02/401 & OPS CHECKED NORMAL.
- [SDR IPXA2025012496294](https://openairdocs.org/sdr/IPXA2025012496294.md): Skin · damaged · Jan 9, 2025 · N572UP · Boeing 74744AF · Fuselage Main, Plate/Skin
  > DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND FOR CORRECTIVE ACTION PLEASE SEE REF: EO-92470-REQ1 (SECTION 48 FUSELAGE SKIN PANEL DENT, GOUGE, AND CRACK DAMAGE FORWARD OF STA 2598; BETWEEN STR 38R AND 46R - CATEGORY B REPAIR) COMPLIED WITH EO-92470
- [SDR IPXA202501096294](https://openairdocs.org/sdr/IPXA202501096294.md): Structure · damaged · Jan 9, 2025 · N572UP · Boeing 74744AF · Fuselage Main, Structure
  > DAMAGE AFT OFF TAIL STAND MOUNT FOUND DURING WALK-AROUND DIRECT AFTER LANDING WE FOUND DAMAGE TO THE TAIL AREA OF THE AIRPLANE. BEFORE GROUND HANDLING TOUCHED THE AIRPLANE AT CGN. WE FOUND FOLLOWING DAMAGES BELOW THE TAIL STAND MOUNT:ONE TIME WE HAD A DENT AND
- [SDR IPXA2024122341321](https://openairdocs.org/sdr/IPXA2024122341321.md): Bulb · inoperative · Dec 21, 2024 · N572UP · Boeing 74744AF · Emergency Lighting
  > EMERGENCY LIGHT IN CEILING PANEL ABOVE L-1 DOOR FWD BULB INOP. RE-LAMPED FWD BULB IN EMERGENCY CEILING LIGHT ABOVE L1 DOOR PER AMM 33-51-07. OPS CHECK GOOD PER AMM 33-51-00.
- [SDR IPXA2024101703256](https://openairdocs.org/sdr/IPXA2024101703256.md): Floor Panel · cracked · Oct 12, 2024 · N572UP · Boeing 74744AF · Fuselage Floor Panel
  > MAIN CARGO DECK FLOOR PANEL APPROX. STA 1140 L TO APPROX STA 1220L CRACKED ALONG ENTIRE OUTBID LENGTH MARKED WITH TAPE. INSTALLED NEW FLOOR PANEL IAW AMM 53-21-02, RII €ŒOK TO INSTALL€? GIVEN ON BARCODE T3F18E005CL38.
- [SDR IPXA2024070771367](https://openairdocs.org/sdr/IPXA2024070771367.md): Skin · dented · Jun 22, 2024 · N572UP · Boeing 74744AF · Wing, Plate/Skin
  > DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE.REMOVED THE DAMAGED SKIN,MEASURE THE CUTOUT (DIA:0.8", 10.75" FROM OUTBD EDGE I.A.W. 747-400F SRM 57-53-01-2R-1.PERFORMED NDT/ET FOR CUTOUT AREA I.A.W. 747 NTM PART6 51-00-00 PROCEDURE 23 REV:176 RESULT:NO CR
- [SDR IPXA20240701367](https://openairdocs.org/sdr/IPXA20240701367.md): Skin · dented · Jun 22, 2024 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > DENT -SKIN, LH WING OUTBD AFT FLAP OUTBD LOWER SIDE. (REPAIR) PERFORMED NDT/UT REWORKED AREA AND PLUS 8" AROUND HEATED AREA, I.A.W. 747 NDT MANUAL PART 1 51-01-01 AND 747 NDT MANUAL PART 1 51-04-00 REV.176, RESULT: NO DEFECT FOUND. OPEN
- [SDR IPXA2024070258057](https://openairdocs.org/sdr/IPXA2024070258057.md): Shear Tie · cracked · Jun 21, 2024 · N572UP · Boeing 74744AF · Fuselage Internal Mounting Structure
  > L/H FRONT SPAR THE SHEAR TIE AT LBL 75.92, STA 1000. REMOVED HARNESS FOR SM REWORK UNDER FLOOR PANEL IAW SWPM 20-10-12
- [SDR IPXA2024070258045](https://openairdocs.org/sdr/IPXA2024070258045.md): Fitting · cracked · Jun 21, 2024 · N572UP · Boeing 74744AF · Fuselage Main, Attach Fittings
  > R/H FRONT SPAR THE INERCOSTAL LUG FITTING AT RBL 11.33 STA 1000 REMOVED BOTS AT STA 1000. CKD NORMAL. REMOVED TUBE. CKD NORMAL IAW IPC 57-14-01-01A.
- [SDR IPXA2024070257995](https://openairdocs.org/sdr/IPXA2024070257995.md): Fitting · cracked · Jun 21, 2024 · N572UP · Boeing 74744AF · Fuselage Main, Attach Fittings
  > L/H FRONT SPAR THE INTERCOSTAL LUG FITTING AT LBL 11.30, STA 1000.REMOVED AND REINSTALLED THE BOLTS AND TUBE AT STA 1000. CONDITIONS WERE NORMAL IAW AMM 20-11-28-964-010
- [SDR IPXA2024070518937](https://openairdocs.org/sdr/IPXA2024070518937.md): Stringer · cracked · Jun 19, 2024 · N572UP · Boeing 74744AF · Leading Edge Devices
  > STRINGER, L/H WING NO.7 V/C FLAP (REPLACE) INSTALL NEW PART IAW SRM 51-40-02-0G REV.101 AND BOEING DWG NO: 65B15170 SH 2 REV:H. IAW AMM 27-81-02-404-010, REV110, STEP A~5(E), INSTALL NO.7 VARIABLE CAMBER FLAP IAW AMM 27-81-02-404-010 REV.110 STEP E(6) TO E(33)
- [SDR IPXA2024041455734](https://openairdocs.org/sdr/IPXA2024041455734.md): Skin · dented · Feb 25, 2024 · N572UP · Boeing 74744AF · Leading Edge Devices
  > NUMBER 14 INBOARD MOST RIGHT WING KRUGER FLAP HAS 2 DENTS VERIFIED CORRECT CLEARANCES AND OPS CHECK OF THE #14 KRUEGER FLAP IAW AMM 27-81-01. ALL CHECKS GOOD AT THIS TIME.
- [SDR IPXA2024081812684](https://openairdocs.org/sdr/IPXA2024081812684.md): Skin · cracked · Jun 26, 2023 · N572UP · Boeing 74744AF · Fuselage Main, Plate/Skin
  > HFEC REINSPECT REVEALED CRACK INDICATION AND NEW DAMAGED IDENTIFIED VISUALLY (T3F18E001Y856 CLOSED IN ERROR) FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01-2R. MATERIAL ID FOR FILLER IS.100" 2024-T3 PO.#SP2586586, AND FOR DOUBLER.125" 2024 T-3 PO.#SP2
- [SDR IPXA2023062831080](https://openairdocs.org/sdr/IPXA2023062831080.md): Structure · punctured · May 27, 2023 · N572UP · Boeing 74744AF · Trailing Edge Flaps
  > LH I/B AFT FLAP HAS A PUNCTURE APPROX 26.75€? FROM TRAILING EDGE & 63€? FROM I/B EDGE. MARKED WITH TAPE.***SM36/LMX4/HGR*** ACCOMPLISHED STEPS 1-14 OF EO-87186-REQ3 PERMANENT REPAIR. THIS CLEARS DEFERRAL MOC 2500762.
- [SDR IPXA2022122046355](https://openairdocs.org/sdr/IPXA2022122046355.md): Gust Lock · broken · Dec 18, 2022 · N572UP · Boeing 74744AF · Passenger/Crew Doors
  > L1 CREW ENTRANCE DOOR LATCH TO HOLD OPEN IS BROKEN CLEANED AND CHECKED HOLD OPEN MECHANISM IAW AMM 52-11-00-201 REV. 106.01. FOUND SATIS
- [SDR IPXA2022081179940](https://openairdocs.org/sdr/IPXA2022081179940.md): Light · inoperative · Jul 17, 2022 · N572UP · Boeing 74744AF · Emergency Lighting
  > **SUPPLEMENTAL SDR**FAULT FOUND THE MAIN DECK L1 DOOR AREA EMERGENCY LIGHT INOP (REPLACE) TASK COMPLETED IAW AMM 33-51-01 REV39.00
- [SDR IPXA2022080419083](https://openairdocs.org/sdr/IPXA2022080419083.md): Panel · broken · Jun 26, 2022 · N572UP · Boeing 74744AF · Wing Structure
  > FAULT - BROKEN - LEFT WING OUTBOARD FORE FLAP ACCESS PANEL WBL 754 (REPAIR) TASK COMPLETED
- [SDR IPXA2022080100360](https://openairdocs.org/sdr/IPXA2022080100360.md): Panel · corroded · Jun 20, 2022 · N572UP · Boeing 74744AF · Fuselage Main, Plate/Skin
  > FAULT - CORROSION - SUPPORT, RH AIR CONDITION COMPARTMENT ACCESS DOOR, MIDDLE SUPPORT. (REPLACE) TASK COMPLETED
- [SDR IPXA2022032580472](https://openairdocs.org/sdr/IPXA2022032580472.md): Floor Panel · damaged · Mar 25, 2022 · N572UP · Boeing 74744AF · Fuselage Floor Panel
  > INSPECTION TYPE:N/AMAIN DECK FLOOR PANEL POS 9L HAS DAMAED UPEPR FACE SHEETFABRICATE REPLACEMENT FLOOR PANEL PER EO B747-5320-42648-A
- [SDR IPXA2022032580471](https://openairdocs.org/sdr/IPXA2022032580471.md): Floor Panel · delaminated · Mar 25, 2022 · N572UP · Boeing 74744AF · Fuselage Floor Panel
  > INSPECTION TYPE:N/AUPPER FACE SHEET OF FLOOR PANEL POS 9L DELAMINATEDFABRICATE NEW FLOOR PANEL PER EO B747-5320-42648-A

Next page: https://openairdocs.org/aircraft/N572UP/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 = 'N572UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N572UP/reports

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