# Service difficulty reports: N578UP

A list on [N578UP](https://openairdocs.org/aircraft/N578UP.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 · 288 reports

- [SDR IPXA2026100851661](https://openairdocs.org/sdr/IPXA2026100851661.md): Strap · broken · Oct 8, 2026 · N578UP · Boeing 74745E · Fuselage Main, Structure
  > MAJOR REPAIR, TRIM BACKING BROKEN STATION 7120. REPAIRED IAW EO-98860-REQ1
- [SDR IPXA2026101229819](https://openairdocs.org/sdr/IPXA2026101229819.md): Warning Message · illuminated · Oct 1, 2026 · N578UP · Boeing 74745E · Door Warning System
  > L1 DOOR NOT SHOWING CLOSED AND LATCHED ON EXTERIOR DOOR SYNOPTIC WHEN L1 DOOR CLOSED FOUND L-1 DOOR CLOSE SWITCH NG.REPLACED L-1 DDOR CLOSE SWITCH PER AMM 52-71-01.NOW L-1 DOOR INDICATION BACK TO NORMAL.
- [SDR IPXA2026100129819](https://openairdocs.org/sdr/IPXA2026100129819.md): Warning Message · indication · Oct 1, 2026 · N578UP · Boeing 74745E · Door Warning System
  > L1 DOOR NOT SHOWING CLOSED AND LATCHED ON EXTERIOR DOOR SYNOPTIC WHEN L1 DOOR CLOSED DEFER PER MEL 52-73-1-0-1.
- [SDR IPXA2026090480472](https://openairdocs.org/sdr/IPXA2026090480472.md): Latch · broken · Sep 4, 2026 · N578UP · Boeing 74745E · Emergency Equipment
  > PED- LITHIUM FIRE CONTAINMENT CASE IS BROKEN SECURING LATCH PERFORMED SREO-90628-REQ2, PED FIRE CONTAINMENT CASE TAMPER SEAL DAMAGED, MISSING OR DAMAGED FILTER COVERS OR CASE MISSING FROM AIRCRAFT. INSTALLED PED CASE PER SREO-90628-REQ20.
- [SDR IPXA2026082480215](https://openairdocs.org/sdr/IPXA2026082480215.md): Fire Warning · false activation · Aug 23, 2026 · N578UP · Boeing 74745E · Fire Detection
  > FIRE CARGO FWD EICAS MSG ON SHORT FINAL EXTINGUISH AFTER APPROX 15 SECONDS NO STATUS MSG,CMC MSG SHOWS CARGO FWD. -4 LOOP -B FAIL,FIM 26-16 TASK 891 FOLLOWED. OPERATIONAL TEST C/OUT,TEST PASS.REV 15 JUL 2026.
- [SDR IPXA2026022552524](https://openairdocs.org/sdr/IPXA2026022552524.md): Power Supply · inoperative · Feb 23, 2026 · N578UP · Boeing 74745E · Emergency Lighting
  > FOUND M5055 POWER SUPPLY MALFUNCTION. (REPLACE) IAW AMM 33-51-04-902-001-001 REV.115 REPLACED POWER SUPPLY (M5055) AT UPPER DECK LEFT SIDE AND PERFORMED POWER SUPPLY TEST, THE RESULT WAS SATISFACTORY.
- [SDR IPXA2026022323848](https://openairdocs.org/sdr/IPXA2026022323848.md): Seat Track · broken · Feb 4, 2026 · N578UP · Boeing 74745E · Fuselage, Seat/Cargo Attach Fittings
  > FOUND MAIN DECK FLOOR STRUCTURE BROKEN AT STA 2054 RBL 75 (REPAIR). CUT AND REMOVE THE DAMAGED SEAT TRACK. MAKE THE EDGES OF THE CUT SMOOTH TO 125 MICROINCHES RA OR BETTER. RECORD THE INITIAL SEAT TRACK PN:65B37086-30 INSTALL THE FLOOR PANELS. REFER TO 747
- [SDR IPXA2026021021755](https://openairdocs.org/sdr/IPXA2026021021755.md): Skin · cracked · Jan 29, 2026 · N578UP · Boeing 74745E · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. FUSELAGE SKIN CRACK AT BS 560 S-23L - S-24L. (REPAIR). ACCOMPLISH THE REPAIR I.A.W SRM 53-00-01-2R-13 REV.64 AND EGAT WORK SHEET NO.60081 REVIEWED TASK PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026022021669](https://openairdocs.org/sdr/IPXA2026022021669.md): Bracket · gouged · Jan 29, 2026 · N578UP · Boeing 74745E · Fuselage Miscellaneous Structure
  > GOUGED BRACKET, BULK CGO APU PNEUMATIC DUCT SUPPORT UPPER BEAM LOWER SIDE AT STA 2280. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.64 2. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.64, AND DWG 65B07693 SH 7 REV.
- [SDR IPXA2026013021723](https://openairdocs.org/sdr/IPXA2026013021723.md): Floor Panel · damaged · Jan 29, 2026 · N578UP · Boeing 74745E · Fuselage Floor Panel
  > MAJOR REPAIR - FOUND MAIN DECK FLOOR PANEL DAMAGE AT STA 1460 RBL 15 P/N:144U5880-26 (REPAIR) REMOVE THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53 21 02. I.A.W. SREO-42648-REQ1 REV.3 COMPLETED FABRICATE A NEW FLOOR PNL.
- [SDR IPXA2026013021744](https://openairdocs.org/sdr/IPXA2026013021744.md): Floor Panel · delaminated · Jan 29, 2026 · N578UP · Boeing 74745E · Fuselage Floor Panel
  > MAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL DELAMINATED AT STA 1000 RBL 20 P/N:144U5882-14 (REPAIR) REVIEWED TASK PER GMM-MTX 09.05.01.09.
- [SDR IPXA2026020600994](https://openairdocs.org/sdr/IPXA2026020600994.md): Angle · corroded · Jan 28, 2026 · N578UP · Boeing 74745E · Aerodynamic Fairings
  > FAULT- CRACK- BRACKET, FWD LOWER WING TO BODY INTERNAL ATTACH BRACKET OF THE CORROSION AT STA 986 LBL 4. (REPLACE) 1. REMOVE DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV.64. 2. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.64 AND BOEING DWG NO.65B0676 SH2 REV.G. 3
- [SDR IPXA2026020630367](https://openairdocs.org/sdr/IPXA2026020630367.md): Cargo Track · cracked · Jan 16, 2026 · N578UP · Boeing 74745E · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR FWD CARGO COMPARTMENT SEAT TRACK CRACK AT STA 968 RBL45. (REPAIR) 1. ACCOMPLISH THE REPAIR I.A.W SRM 53-00-52-2R-10 REV. 64 AND EGAT WORK SHEET NO: 60024 2. REFER TO DAMAGE REPORT FOR THE ORIGINAL MATERIAL & THICKNESS, REPAIR MATERIAL & THICKNESS
- [SDR IPXA2026022330508](https://openairdocs.org/sdr/IPXA2026022330508.md): Support Fitting · cracked · Jan 16, 2026 · N578UP · Boeing 74745E · Ailerons
  > ***MAJOR REPAIR*** FAULT - FOUND #6 SPOILER ACTUATOR SUPPORT FITTING L/H LOWER CRACK. (REPAIR) CUT OUT THE DAMAGED AREA AS SHOWN IN FIGURE 202 INSTALL THE REPAIR PARTS WITH BMS 5-95 SEALANT BETWEEN THE MATING SURFACES..ACCOMPLISHED REPAIR I.A.W EO-96614-RE
- [SDR IPXA2025121778168](https://openairdocs.org/sdr/IPXA2025121778168.md): Slide · unwanted deploy · Dec 16, 2025 · N578UP · Boeing 74745E · Escape Slide
  > RIGHT UPPER DECK ESCAPE DOOR/SLIDE DEPLOYED. REINSTALLED NEW RH UPPER DECK ESCAPE SLIDE IAW AMM 25-68-01 UP TO AND INCLUDING STEP G. 9. VERIFIED SAFETY PINS REMOVED AND PROPER SYSTEM PRESSURES IAW AMM 25-68-01 AND GMM 04-02. COMPLETED REMAINING STEPS IAW AMM
- [SDR IPXA2025071825183](https://openairdocs.org/sdr/IPXA2025071825183.md): Aileron Sys · no discrepancy · Jul 14, 2025 · N578UP · Boeing 74745E · Aileron Control System
  > DURING CLIMB OUT AILERON FORCE WERE A LITTLE HEAVIER THAN NORMAL AND RIGHT AILERON REQUIRED SIGNIFICANTLY MORE FORCE THEN LEFT AILERON. PERFORM ROTATIONAL TORQUE CK OF BOTH YOKES IAW AMM 27-11-00-705-091. WITH IN LIMITS.
- [SDR IPXA2025040311394](https://openairdocs.org/sdr/IPXA2025040311394.md): Sign · inoperative · Apr 3, 2025 · N578UP · Boeing 74745E · Emergency Lighting
  > FAULT - FOUND THE UPPER DECK EMERGENCY EXIT SIGN LIGHT INOP AT STA 620 AND STA 690 (REPLACE). I.A.W AMM 33-51-00-715-105 REV.113 CONTINUE TO SUPPLY POWER TO THE EMERGENCY LIGHT SYSTEM FOR SUFFICIENT TIME TO CHARGE THE BATTERY PACKS FOR THE POWER SUPPLIES, THE
- [SDR IPXA2024122013341](https://openairdocs.org/sdr/IPXA2024122013341.md): Circuit Card · faulted · Dec 20, 2024 · N578UP · Boeing 74745E · Fire Detection
  > DURING PRE-DEPARTURE CHECK FOUND CARGO FIRE MD ZONE 6 LOOP-A FAIL NO CURENT FAULT FOUND. C/O FIRE TEST IAW AMM 26-11-00-715-001 REV 112. CHECKED SATIS. THIS CLOSES DMI. PLACARD REMOVED.
- [SDR IPXA2024082676285](https://openairdocs.org/sdr/IPXA2024082676285.md): Structure · broken · Aug 21, 2024 · N578UP · Boeing 74745E · Fuselage Structure (General)
  > LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) INSTALLED 2(EA) BALL MAT PANELS IN LWR AFT PIT AT STATIONS 1840 AND 1900 PER AMM 25-53-15-400-801, PDU OPS CHECK GOOD PER AMM SUBTASK 25-53-01-864-03
- [SDR IPXA2024082176285](https://openairdocs.org/sdr/IPXA2024082176285.md): Structure · broken · Aug 21, 2024 · N578UP · Boeing 74745E · Fuselage Main, Structure
  > LOAD CREW FOUND CENTERLINE GUIDE AND AIRCRAFT STRUCTURE BROKEN AT STATION 1820-1840 (POSITION 9 AFT LOWER PIT) OPEN
- [SDR IPXA2024080588574](https://openairdocs.org/sdr/IPXA2024080588574.md): Window · delaminated · Aug 4, 2024 · N578UP · Boeing 74745E · Flight Compartment Windows
  > CAPT€™S #1 (FRONT) WINDSHIELD DELAMINATING ON TOP SECTION OF WINDOW COMPLETED WINDOW INSLALL WITH REF TO B747 MM 56-11-01. PERFORMED WIPER OPS CHECK WITH REF TO B747 MM 30-42-00.
- [SDR IPXA2024071862660](https://openairdocs.org/sdr/IPXA2024071862660.md): Hmu · inoperative · Jul 17, 2024 · N578UP · Boeing 74745E · Fuel Controlling System
  > ON DECENT GOT #3 GEN ELECT FAIL. THEN ENG 3 FAILED APPEARED. N1 WAS AROUND 28%. ENGINE RETURNED TO NORMAL IDLE. ENG FAIL MESSAGE LASTED ABOUT 20 SECONDS NO OTHER PROBLEMS WITH ENG. CREW REPORTS CLEAR GOOD WEATHER DURING FAULT. REF FIM TASK 71-00 TASK A72 AND 7
- [SDR IPXA2024062744323](https://openairdocs.org/sdr/IPXA2024062744323.md): Light · faulted · Jun 27, 2024 · N578UP · Boeing 74745E · Emergency Lighting
  > EMER LIGHTS EICAS. RESET EMERGENCY LIGHT SWITCH. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-715-001. OPS CHECK GOOD.
- [SDR IPXA2024021728160](https://openairdocs.org/sdr/IPXA2024021728160.md): Battery · inoperative · Feb 12, 2024 · N578UP · Boeing 74745E · Emergency Lighting
  > FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE) C/W I.A.W AMM 33-51-04-902-001-001 REV.109 REPLACED THE EMERGENCY LIGHT BATTERY (M5056) AT UPPER DECK,AND PERFORMED UPPER DECK EMERGENCY LIGHT OPERATIONAL TEST, RESULT WAS SATISFACTORY. I
- [SDR IPXA2024021228160](https://openairdocs.org/sdr/IPXA2024021228160.md): Light · inoperative · Feb 12, 2024 · N578UP · Boeing 74745E · Emergency Lighting
  > SDR FILED OPEN. FOUND THE UPPER DECK DOOR RIGHT SIDE EXIT EMERGENCY LIGHT INOP (REPLACE)
- [SDR IPXA2024013125856](https://openairdocs.org/sdr/IPXA2024013125856.md): Snubber · out of limits · Jan 31, 2024 · N578UP · Boeing 74745E · Passenger/Crew Doors
  > FOUND L4 ENTRY DOOR SNUBBER INDICATOR OUT OF LIMIT. (REPLACE) C/W 1. I.A.W AMM 52-11-10-004-001 REV. 109 AND AMM 52-11-10-404-005 REV. 109 REPLACE SNUBBER. 2. IPC VERIFIED AND SERVICEABLE PARTS TAG NO. 983747. 3. JOB COMPLETE AND CONDITION CHECK NORMAL.
- [SDR IPXA2024021230568](https://openairdocs.org/sdr/IPXA2024021230568.md): Tension Tie · cracked · Jan 19, 2024 · N578UP · Boeing 74745E · Fuselage Main, Attach Fittings
  > *MAJOR REPAIR* FAULT - CRACK - FND TENSION TIE CHANNEL FWD SIDE CRACK AT STA 1120 L/H (REPAIR) ACCOMPLISH REINFORCING REPAIR I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2 (FIGURE 201). 1.ACCOMPLISH INSPECTION I/A/W B747-400SF (REV. 58) SRM 53-40-30-2R-2, TABLE
- [SDR IPXA2024021610259](https://openairdocs.org/sdr/IPXA2024021610259.md): Skin · dented · Jan 18, 2024 · N578UP · Boeing 74745E · Nacelle/Pylon, Plate/Skin
  > DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) 1.REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (DIAMETER:1",DEPTH:0.0175",32.5" FROM FORWARD EDGE,25.5" FROM LOWER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE CURED A
- [SDR IPXA2024021610224](https://openairdocs.org/sdr/IPXA2024021610224.md): Skin · dented · Jan 18, 2024 · N578UP · Boeing 74745E · Nacelle/Pylon, Plate/Skin
  > DENT - SKIN SURFACE AT 10 O'CLOCK, NR 1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.7",DEPTH:0.012",30.4" FROM FORWARD EDGE,38" FROM UPPER EDGE). FILL THE DAMAGE AREA WITH ADHESIVE
- [SDR IPXA2024011810224](https://openairdocs.org/sdr/IPXA2024011810224.md): Skin · dented · Jan 18, 2024 · N578UP · Boeing 74745E · Nacelle/Pylon, Plate/Skin
  > *** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 10 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK
- [SDR IPXA2024011810259](https://openairdocs.org/sdr/IPXA2024011810259.md): Skin · dented · Jan 18, 2024 · N578UP · Boeing 74745E · Nacelle/Pylon, Plate/Skin
  > *** SDR FILED OPEN *** FAULT - DENT - SKIN SURFACE AT 7 O'CLOCK, NO.1 ENG LH FAN COWL EXTERNAL AREAS (REPAIR) OK TO WORK
- [SDR IPXA2024022347664](https://openairdocs.org/sdr/IPXA2024022347664.md): Skin · cracked · Jan 16, 2024 · N578UP · Boeing 74745E · Leading Edge Devices
  > CRACKED SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) INSTALLED NEW PART I.A.W. SRM 51-40-02-0G REV.58 AND BOEING DWG NO:65B15168 SH.2 REV.G AND AIPC 27-81-02-01 REV.54. I.A.W AMM 27-81-02-404-010 REV.109 STEP 3.A TO 3.E.(5), INSTALL LH WING NO. 1
- [SDR IPXA2024022347710](https://openairdocs.org/sdr/IPXA2024022347710.md): Skin · broken · Jan 16, 2024 · N578UP · Boeing 74745E · Wing, Plate/Skin
  > BROKEN SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) C/W 1. OK TO INSTALL PANEL NO: 521EB. 2. I.A.W AMM 20-51-01-912-008 REV.109 INSTALL PANEL NO: 521EB. 3. CONDITION CHECK NORMAL. 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB
- [SDR IPXA2024021647771](https://openairdocs.org/sdr/IPXA2024021647771.md): Panel · debonded · Jan 16, 2024 · N578UP · Boeing 74745E · Wing, Plate/Skin
  > LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) 1.I.A.W AMM 51-24-11-477-083 REV.109,CLEANING UP SURFACE AND ROLLER PAINT. 2.JOB COMPLETED AND CONDITION CHECK NORMAL.
- [SDR IPXA2024021645990](https://openairdocs.org/sdr/IPXA2024021645990.md): Fairing · damaged · Jan 16, 2024 · N578UP · Boeing 74745E · Wing Miscellaneous Structure
  > NR 8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) REMOVE THE DAMAGE MATERIALS AND CLEAN.MEASURE THE DAMAGE AREA (LENGTH:0.8",WIDTH:0.5",AT UPPER EDGE,5" FROM AFTER EDGE). BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUT
- [SDR IPXA2024021645522](https://openairdocs.org/sdr/IPXA2024021645522.md): Stiffener · cracked · Jan 16, 2024 · N578UP · Boeing 74745E · Elevator, Plate/Skin
  > *** SUPPLEMENTAL SDR *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W AMM 27-31-01-404-015 REV.109 STEP 3.H(14) TO 3.H(23) ADJUST R/H INBOARD ELEVATOR AND OPERATION.
- [SDR IPXA2024011747664](https://openairdocs.org/sdr/IPXA2024011747664.md): Skin · cracked · Jan 16, 2024 · N578UP · Boeing 74745E · Trailing Edge Flaps
  > *** SDR FILED OPEN *** FAULT - CRACK - SKIN, LH WING NO.1E VC FLAP PANEL OUTER SURFACE (REPAIR) I.A.W AMM 27-81-02-004-001 REV 109 REMOVE #1E V.C FLAP
- [SDR IPXA2024011745990](https://openairdocs.org/sdr/IPXA2024011745990.md): Fairing · unknown · Jan 16, 2024 · N578UP · Boeing 74745E · Flight Control System
  > *** SDR FILED OPEN *** FAULT - NO.8 MOVABLE FAIRING OUTBD SIDE AND AFT SIDE SURFACE DAMAGE (REPAIR) OK TO WORK
- [SDR IPXA2024011745522](https://openairdocs.org/sdr/IPXA2024011745522.md): Stiffener · cracked · Jan 16, 2024 · N578UP · Boeing 74745E · Elevator Structure
  > *** SDR FILED OPEN *** FAULT - RIGHT INBOARD ELEVATOR, INBOARD, LEADING EDGE RIB ANDSTIFFENER CRACK (REPLACE) I.A.W. AMM 27-31-01-004-001 REV.109 REMOVED R/H INBOARD ELEVATOR.
- [SDR IPXA2024011747771](https://openairdocs.org/sdr/IPXA2024011747771.md): Skin · debonded · Jan 16, 2024 · N578UP · Boeing 74745E · Wing, Plate/Skin
  > *** SDR FILED OPEN *** FAULT - LEFT WING INBOARD LEADING EDGE UPPER FIXED PANEL DISBOND, 46" FROM LEADING, EDGE, 157" FROM INBOARD EDGE (REPAIR) OK TO WORK
- [SDR IPXA2024011747710](https://openairdocs.org/sdr/IPXA2024011747710.md): Skin · damaged · Jan 16, 2024 · N578UP · Boeing 74745E · Wing, Plate/Skin
  > *** SDR FILED OPEN *** FAULT - BROKEN - SKIN, LH WING LE LWR SURFACE PANEL (REPAIR) OK TO WORK
- [SDR IPXA2024010359777](https://openairdocs.org/sdr/IPXA2024010359777.md): Door · binding · Dec 27, 2023 · N578UP · Boeing 74745E · Passenger/Crew Doors
  > *** SUPPLEMENTAL SDR *** MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE REPLACED ROD END ASSY. ON LOWER HINGE GUIDE ARM REF AMM 52-11-01-401. OPS NORMAL AT THIS TIME. REF BARCODE T3F18E003MVRM FOR PARTS INFORMATION.
- [SDR IPXA2023122759777](https://openairdocs.org/sdr/IPXA2023122759777.md): Unknown · unknown · Dec 27, 2023 · N578UP · Boeing 74745E · Passenger/Crew Doors
  > MAIN ENTRY DOOR DIFFICULT TO OPEN AND CLOSE, OPEN
- [SDR IPXA2023110891070](https://openairdocs.org/sdr/IPXA2023110891070.md): Trunnion · cracked · Sep 27, 2023 · N578UP · Boeing 74745E · Main Landing Gear Attach Section
  > RIGHT AFT TRUNNION, CRACKS
- [SDR IPXA202309281070](https://openairdocs.org/sdr/IPXA202309281070.md): Unknown · unknown · Sep 27, 2023 · N578UP · Boeing 74745E · Fuselage, Landing Gear Attach Fittings
  > OPEN, RIGHT AFT TRUNNION, CRACKS
- [SDR IPXA2023092551464](https://openairdocs.org/sdr/IPXA2023092551464.md): Cargo Track · damaged · Jul 25, 2023 · N578UP · Boeing 74745E · Fuselage, Seat/Cargo Attach Fittings
  > *** MAJOR REPAIR *** DURING CARGO LOADING OPERATIONS, FOUND FWD LWR CARGO DOUBLE PALLET LOCK ASSY. SECURING RAIL BROKEN, WL-118 ST-560, RH FWD BALL-MAT.***SM26/LMX13*** **WORK WITH 25TEY**457790 INSTALLED PDU CANNON PLUG REF AMM 25-53-01
- [SDR IPXA2023052052755](https://openairdocs.org/sdr/IPXA2023052052755.md): Lamp · inoperative · May 16, 2023 · N578UP · Boeing 74745E · Emergency Lighting
  > *** SUPPLEMENTAL SDR *** FAULT - THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) ALL PAPERWORK C/W
- [SDR IPXA52755](https://openairdocs.org/sdr/IPXA52755.md): Unknown · unknown · May 16, 2023 · N578UP · Boeing 74745E · Emergency Lighting
  > THE EMERGENCY SLIDE LIGHT (L2930) INOP AT RIGHT UPPER DECK DOOR. (REPLACE) OK TO WORK. OPEN
- [SDR IPXA2024021763758](https://openairdocs.org/sdr/IPXA2024021763758.md): Skin · corroded · Feb 3, 2023 · N578UP · Boeing 74745E · Wing, Plate/Skin
  > *MAJOR REPAIR* FASTENERS PULLED THROUGH SKIN, LH WING***SM40/LMX6***HGR*** 1.REPAIR PER UPS EO-89517-REQ1 REV.1. 2.JOB COMPLETED. REVIEWED
- [SDR 2022FA0000519](https://openairdocs.org/sdr/2022FA0000519.md): Access Panel · missing · Sep 12, 2022 · N578UP · Boeing 74745E · Nacelle/Pylon, Plate/Skin
  > OUTBD PYLON NO.4 FOUND PANEL 484DR MISSING

Next page: https://openairdocs.org/aircraft/N578UP/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 = 'N578UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N578UP/reports

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