# Service difficulty reports: N444UP

A list on [N444UP](https://openairdocs.org/aircraft/N444UP.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 5 · 206 reports

- [SDR IPXA2026092196740](https://openairdocs.org/sdr/IPXA2026092196740.md): Access Panel · delaminated · Sep 17, 2026 · N444UP · Boeing 75724APF · Wing, Plate/Skin
  > MAJOR REPAIR, RT WING DRY BAY ACCESS PANEL 632FZ DAMAGED MADE REPAIR PLIES FROM BMS8-79 BATCH 4506113 AND BMS 5-129 BATCH 4494000, LAYED UP AND BAGGED AND CURED IAW SRM 51-70-07-OG-0 PARA. 4.D-G. REPAIR ACCOMPLISHED IAW SRM REV 125 CHAPTER 51-70-07-0G-0, REP
- [SDR IPXA2026100555363](https://openairdocs.org/sdr/IPXA2026100555363.md): Frame · not grounded · Sep 15, 2026 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > EXISTING REPAIR FOUND AT AFT CARGO COMPARTMENT FRAME STA 1460 L/H. ACCOMPLISHED THE REPAIR PER EO-98750-REQ1 AND STE-PNA EA 757-5360-27-A4633, REV. -.
- [SDR IPXA2026092825914](https://openairdocs.org/sdr/IPXA2026092825914.md): Skin · corroded · Sep 7, 2026 · N444UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > ***MAJOR REPAIR*** FAULT-400-STR- #2 ENGINE NACELLE PYLON STRUT, OUTBD INNER SKIN, FWD OF THE VENT PANEL OPENING HAS CORROSION AT SEAM OF FRAME, MAY BE UNDER THE PREVIOUS REPAIR. DOT 8-002. REMOVED EXISTING REPAIR DOUBLER AND REPAIR FILLER IN STR- #2 ENGINE NA
- [SDR IPXA2026091925377](https://openairdocs.org/sdr/IPXA2026091925377.md): Skin · cracked · Sep 7, 2026 · N444UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > ENG 2 PYLON, CRACK AT LOWER T/E WEDGE. INSTALLED PANEL ASSY AT ENG 2 PYLON AT LOWER T/E WEDGE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026092803255](https://openairdocs.org/sdr/IPXA2026092803255.md): Drag Fitting · cracked · Sep 5, 2026 · N444UP · Boeing 75724APF · Nacelle/Pylon, Attach Fittings
  > FAULT: RIGHT WING PYLON HOLE #4 HAS 1EA CRACK AT 2 O'CLOCK AT TOP OF FITTING. COMPLIED WITH PER EO -88069-JIC11. REVIEWED
- [SDR IPXA2026092803215](https://openairdocs.org/sdr/IPXA2026092803215.md): Drag Fitting · cracked · Sep 5, 2026 · N444UP · Boeing 75724APF · Nacelle/Pylon, Attach Fittings
  > RIGHT WING PYLON HOLE #5 HAS 2EA CRACKS AT 11 AND 4 O'CLOCK AT TOP OF FITTING AND 2EA CRACKS AT 7 AND 4 O'CLOCK AT BOTTOM OF SKIN. IAW EO -88069-JIC11 STEP # 3 AND NDT MANUAL PART 6, 51-00-16.
- [SDR IPXA2026092176383](https://openairdocs.org/sdr/IPXA2026092176383.md): Bracket · corroded · Sep 3, 2026 · N444UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB, BRACKET AT THE OUTBD END OF HORIZONTAL STAB, LOCATED BETWEEN THE REAR SPAR AND THE ELEVATOR LEADING EDGE, SHOWS EVIDENCE OF CORROSION. DOT 65-01 INSTALLED ANGLE (BRACKET) AREA. IAW B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026091656672](https://openairdocs.org/sdr/IPXA2026091656672.md): Angle · corroded · Sep 2, 2026 · N444UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR LOWER ANGLE FROM STA 1787.45 TO STA 1825.00 S-3R HAS A CORROSION INSTALLED NEW LOWER ANGLE I.A.W. B757-200PF SRM 51-40-02-0G-0
- [SDR IPXA2026091756601](https://openairdocs.org/sdr/IPXA2026091756601.md): Angle · corroded · Sep 2, 2026 · N444UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR FWD LOWER CORNER ANGLE AT BS 1787.45, S-3R HAD CORROSION. INSTALLED NEW FWD LOWER CORNER IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026091856663](https://openairdocs.org/sdr/IPXA2026091856663.md): Angle · corroded · Sep 2, 2026 · N444UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR UPPER ANGLE FROM BS 1787.45 - 1825, S3R HAD CORROSION. INSTALLED NEW UPPER ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026091556641](https://openairdocs.org/sdr/IPXA2026091556641.md): Strap · corroded · Sep 2, 2026 · N444UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET DOOR FWD STRAP HAD CORROSION. INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026091553994](https://openairdocs.org/sdr/IPXA2026091553994.md): Support Channel · cracked · Sep 2, 2026 · N444UP · Boeing 75724APF · Wing Miscellaneous Structure
  > RH MLG WEEL WELL FWD SEAL SUPPORT CRACKED. REMOVED PANELS 198CR AND 198BR FOR ACCESS AND REMOVRD SEAL AND SEAL RETEINER AND SEAL SUPPORT DAMAGED IAW B757-200PF SRM 51-40-02-0G. INSTALLED NEW SEAL AT RH MLG WEEL WELL IAW B757-200PF AMM 32-12-51-404-004.
- [SDR IPXA2026091554044](https://openairdocs.org/sdr/IPXA2026091554044.md): Support Bracket · cracked · Sep 2, 2026 · N444UP · Boeing 75724APF · Wing Miscellaneous Structure
  > RIGHT MLG WEEL WELL RH GEAR DOOR CLOSED SWITCH LATERAL SUPPORT CRACKED. REMOVED DAMAGED SUPPORT BRACKET AT RT MLG WEEL WELL R/H GEAR DOOR CLOSED SWITCH LATERAL IAW SRM B757-200PF SRM 51-40-02-0G. INSTALLED NEW ANGLE IAW B757-200PF SRM 51-40-02-0G-0.
- [SDR IPXA2026091554070](https://openairdocs.org/sdr/IPXA2026091554070.md): Support Bracket · cracked · Sep 2, 2026 · N444UP · Boeing 75724APF · Wing Miscellaneous Structure
  > RH MLG WEEL WELL FWD SEAL SUPPORT ANGLE CRACKED. REMOVED SEAL SUPPORT ANGLE IS CRACKED AT R/H MLG WEEL WELL FWD IAW SUPPORT ANGLE IAW SRM SRM 51-40-02-0G. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0.
- [SDR IPXA2026050631728](https://openairdocs.org/sdr/IPXA2026050631728.md): Slat System · warning message · Apr 29, 2026 · N444UP · Boeing 75724APF · Leading Edge Slat Control System
  > EMERGENCY DECLARED. LE SLAT DISAGREE PREFORMED FIM 27-81-803. NO FAULTS NOTED ON BITE PROCEDURE. CYCLED FLAPS AND SLATS SEVERAL TIMES WITH NO FAULTS. SYSTEM IS OK.
- [SDR IPXA2026020973228](https://openairdocs.org/sdr/IPXA2026020973228.md): Lamp · inoperative · Feb 6, 2026 · N444UP · Boeing 75724APF · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT, 5 LAMPS INOPERATIVE. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-00-501.
- [SDR IPXA2026020673228](https://openairdocs.org/sdr/IPXA2026020673228.md): Lamp · inoperative · Feb 6, 2026 · N444UP · Boeing 75724APF · Emergency Lighting
  > COCKPIT EMERGENCY LIGHT- 5 LAMPS INOPERATIVE. OPEN
- [SDR IPXA2025012426474](https://openairdocs.org/sdr/IPXA2025012426474.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QEH, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0334 IR. OSD: 1/24/2025
- [SDR IPXA2025012326458](https://openairdocs.org/sdr/IPXA2025012326458.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QE4, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0331 IR.
- [SDR IPXA2025012426435](https://openairdocs.org/sdr/IPXA2025012426435.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QE6, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0330 IR. OSD: 1/24/2025
- [SDR IPXA2025012326400](https://openairdocs.org/sdr/IPXA2025012326400.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QC2, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0328 IR. OSD: 1/24/2025
- [SDR IPXA2025012326442](https://openairdocs.org/sdr/IPXA2025012326442.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QCU, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0337 IR. OSD: 1/24/2025
- [SDR IPXA2025012326367](https://openairdocs.org/sdr/IPXA2025012326367.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QBG, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0326 IR. OSD: 1/24/2025
- [SDR IPXA2025012326402](https://openairdocs.org/sdr/IPXA2025012326402.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QCB, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5330-01-B0329 IR. OSD: 1/24/2025
- [SDR IPXA2025012326492](https://openairdocs.org/sdr/IPXA2025012326492.md): Frame · dented · Jan 16, 2025 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > REF HEAVY CHECK REPAIR T3F18E0051QFY, HFEC AFTER TRIM OUT REQUIRES RII VERIFICATION. ACCOMPLISHED REPAIR PER EA 757-5360-01-B0335 IR. OSD: 1/24/2025
- [SDR IPXA2024101590204](https://openairdocs.org/sdr/IPXA2024101590204.md): Warning Message · illuminated · Oct 1, 2024 · N444UP · Boeing 75724APF · Door Warning System
  > FWD ENT DOOR€? EICAS MESSAGE ILLUMINATED ON SHORT FINAL. CAME ON AT 1200 FT AGL. AND EXTINGUISHED AT 800FT AGL. REMOVED AND REPLACED CRACKED BRACKET PER SRM 51-40-02. REINSTALLED PREVIOUSLY REMOVED SIDEWALL PANELS AND OPS CHECKED L1 DOOR INDICATION IAW AMM 52
- [SDR IPXA2024100190204](https://openairdocs.org/sdr/IPXA2024100190204.md): Bracket · not reported · Oct 1, 2024 · N444UP · Boeing 75724APF · Door Warning System
  > *SDR FILED OPEN* €ŒL FWD ENT DOOR€? EICAS MESSAGE ILLUMINATED ON SHORT FINAL. CAME ON AT 1200 FT AGL. AND EXTINGUISHED AT 800FT AGL. WILL REQUIRE 13 HOURS SHEET METAL TO R&R BRACKET. WILL REQUIRE LMX EVAL FOR OPEN FOR ACCESS. HANGAR SHOULD NOT BE NEEDED FOR
- [SDR IPXA2024091941134](https://openairdocs.org/sdr/IPXA2024091941134.md): Floorboard · corroded · Aug 24, 2024 · N444UP · Boeing 75724APF · Fuselage Floor Panel
  > COOROSION AT STA 1200 UNDER FLOORBOARD 242XKF. DOT 140-011.SURFACE HFEC PERFORMED ON BLENDED AREAS ON STA 1200 UNDER FLOORBOARD 242XKF. NO DEFECTS FOUND IAW 51-00-19.
- [SDR IPXA2024090541134](https://openairdocs.org/sdr/IPXA2024090541134.md): Floor Support · corroded · Aug 24, 2024 · N444UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > COOROSION AT STA 1200 UNDER FLOORBOARD 242XKF. OPEN
- [SDR IPXA2024090587187](https://openairdocs.org/sdr/IPXA2024090587187.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND DENT AT STA 1220 RH BTW STRG 26-25 WORK PERFORMED: REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-6 DETAIL VI PER SRM 53-60-07-2R.
- [SDR IPXA2024090587078](https://openairdocs.org/sdr/IPXA2024090587078.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND DENT AT STA 820 LH BTW STR23 TO STR24. VERIFIED WORK PERFORMED: REPAIR PER B757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, DETAIL III PER SRM 53-30-07-2R.
- [SDR IPXA2024090587385](https://openairdocs.org/sdr/IPXA2024090587385.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND DENT AT STA 1520 LH BTW STRG 25-26. REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, DETAIL III PER SRM 53-60-07-2R. INSTALLED STR CLIP (01EA) AT STR 25 LH IAW B757 SRM 51-40-02.
- [SDR IPXA2024090587054](https://openairdocs.org/sdr/IPXA2024090587054.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND DENT AT STA 760 RH BTW STR24 TO STR25. VERIFIED REPAIRED PER 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, DETAIL III PER SRM 53-30-07-2R.
- [SDR IPXA2024090587185](https://openairdocs.org/sdr/IPXA2024090587185.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT. STR-Z100. FOUND DENT AT STA 1320 LH BTW STRG 24-25. REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, DETAIL III PER SRM 53-60-07-2R. INSTALLED NEW FRAME AT STA 1320 LH BTW STRG 24-25. IAW B757-200 SRM 51-40-02 AND SRM 53-00-07-2R-5, PER SRM 53-6
- [SDR IPXA2024090587040](https://openairdocs.org/sdr/IPXA2024090587040.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND 2 EA DENTS AT STA 660 RH BTW STR23 TO STR24. VERIFIED WORK PERFORMED: REPAIR PER 757-200PF SRM REV 120 CHAPTER 53-00-07-2R-5, DETAIL III PER SRM 53-30-07-2R.
- [SDR IPXA2024090587024](https://openairdocs.org/sdr/IPXA2024090587024.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT. STR-Z100. FOUND DENT AT STA 680 RH BTW STR23 TO STR24. INSTALLED NEW FRAME AT STA 680 RH BTW STRG 23-24. IAW B757-200 SRM 51-40-02 AND SRM 53-00-07-2R-5, PER SRM 53-30-07-2R DETAIL II. REVIEWED
- [SDR IPXA2024090587257](https://openairdocs.org/sdr/IPXA2024090587257.md): Frame · dented · Aug 21, 2024 · N444UP · Boeing 75724APF · Fuselage Main, Frame
  > FOUND DENT AT STA 1460 LH BTW STRG 25-26. NEW FRAME (REPAIR SPLICE) AT STA 1460 LH BTW STRG 22-23. IAW B757-200 REV 120 SRM 51-40-02 AND SRM 53-00-07-2R-5, DETAIL I PER SRM 53-60-07-2R.
- [SDR IPXA2024090566979](https://openairdocs.org/sdr/IPXA2024090566979.md): Skin · corroded · Aug 20, 2024 · N444UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > #2 PYLON OUTBD INNER SKIN FWD OF THE VENT PANEL OPENING HAS CORROSION. DOT 8-004. VERIFIED, ACCOMPLISHMENT OF WORK PER UPS EO 91221-REQ 1 AND VT MAE EA 757-5450-27-A3676 REV. FAA 8100 APPROVAL ATTCHED.
- [SDR IPXA2024090652829](https://openairdocs.org/sdr/IPXA2024090652829.md): Latch · gouged · Aug 20, 2024 · N444UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR, LOWER LATCH W/GOUGE SCRATCH; DOT 11-005, JR-117. WORK ACCOMPLISHED PER SREO-14721-REQ001.
- [SDR IPXA2024090652638](https://openairdocs.org/sdr/IPXA2024090652638.md): Latch · gouged · Aug 20, 2024 · N444UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR, UPPER LATCH W/GOUGE SCRATCH; DOT 11-004, JR-117. WORK ACCOMPLISHED PER SREO-14721-REQ001. REVIEWED
- [SDR IPXA2024082052638](https://openairdocs.org/sdr/IPXA2024082052638.md): Latch · gouged · Aug 20, 2024 · N444UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR, UPPER LATCH W/GOUGE SCRATCH.
- [SDR IPXA2024082052829](https://openairdocs.org/sdr/IPXA2024082052829.md): Latch · gouged · Aug 20, 2024 · N444UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW DOOR, LOWER LATCH W/GOUGE SCRATCH; DOT 11-005, JR-117.
- [SDR IPXA2025022694133](https://openairdocs.org/sdr/IPXA2025022694133.md): Fairing · punctured · Jan 5, 2024 · N444UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT AFT WING TO BODY FAIRING HAS 2 EACH PUNCTURES€¦.MARKED WITH YELLOW GREASE PENCIL. PREPARE AND APPLIED PLIES WITH EA 9390 BATCH 4303218 AND 04-009-0002 BATCH 4297288 AND CURED IAW-757-200-SRM-51-70-17-0G-0 PARA 4.B. 8-11. RESTORED PROTECTIVE COATING WITH
- [SDR IPXA2024010694133](https://openairdocs.org/sdr/IPXA2024010694133.md): Unknown · unknown · Jan 5, 2024 · N444UP · Boeing 75724APF · Aerodynamic Fairings
  > RIGHT AFT WING TO BODY FAIRING HAS 2 EACH PUNCTURES€¦.MARKED WITH YELLOW GREASE PENCIL. FOUND DAMAGE TO BE WITHIN LIMITS FOR DEFERRAL, ITEM REQUIRES REINSPECTION EVERY A CHECK AND REPAIR NO LATER THAN NEXT C CHECK, APPLIED TAPE TO SEAL THE PANEL IAW SRM 53-00
- [SDR IPXA2023101046076](https://openairdocs.org/sdr/IPXA2023101046076.md): Smoke Goggles · cracked · Oct 6, 2023 · N444UP · Boeing 75724APF · Emergency Equipment
  > *** SUPPLEMENTAL SDR *** ONE SMOKE GOGGLE HAS CRACKED LENS IN COURIER AREA INSTALLED REPLACEMENT SMOKE GOGGLES W/REF TO M/M 25-60-00/001
- [SDR IPXA2023100946076](https://openairdocs.org/sdr/IPXA2023100946076.md): Unknown · unknown · Oct 6, 2023 · N444UP · Boeing 75724APF · Emergency Equipment
  > ONE SMOKE GOGGLE HAS CRACKED LENS IN COURIER AREA INSTALLED REPLACEMENT SMOKE GOGGLES W/REF TO M/M 25-60-00/001. OPEN
- [SDR IPXA2022081485224](https://openairdocs.org/sdr/IPXA2022081485224.md): Skin · corroded · Jul 31, 2022 · N444UP · Boeing 75724APF · Wing, Plate/Skin
  > INSPECTION TYPE:DVI#2 PYLON WING SKIN/DRAG FTG HOLE #2 HAS CORROSION INDICATION INSIDE HOLE FOUND DURING INSP OF THE E.O. B757-5720-69617-I APPENDIX EREPAIRED IAW UPS E.O. B757-5720-84376-A DATED 08/14/2022
- [SDR IPXA2022081285169](https://openairdocs.org/sdr/IPXA2022081285169.md): Tie Clip · corroded · Jul 26, 2022 · N444UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CK17FWD CARGO DOOR AT APPROX FS 580 LOWER INNER T CHORD IS CORRODEDREMOVED AND REPLACED T CHORD USING AN 10136-1503 PER SRM 51-40-02 PAR 9
- [SDR IPXA2022042081321](https://openairdocs.org/sdr/IPXA2022042081321.md): Slat · none · Apr 20, 2022 · N444UP · Boeing 75724APF · Leading Edge Slat Control System
  > INSPECTION TYPE:NA**ATB** **EMERGENCY DECLARED** **LANDED WITHOUT INCIDENT** LE SLAT DISAGREE ON DEPARTURE. RAN APPROPRIATE CHECKLIST AND RETURNED TO MSP. ATB.TROUBLESHOT LE SLAT DISAGREE IN REF TO FIM 27-81-00-815-803. FOUND O/B OVERLOAD INDICATOR TRIPPED ON
- [SDR IPXA2022041581182](https://openairdocs.org/sdr/IPXA2022041581182.md): None · none · Apr 15, 2022 · N444UP · Boeing 75724APF · Leading Edge Slat Control System
  > INSPECTION TYPE:NA**ATB ** NON TAKEOFF WHILE RETRACTING FLAPS, RECEIVED A L.E. SLAT DISAGREE. WHILE RUNNING CHECKLIST TO CONFIGURE RECIEVED A T.E. DISAGREE. LANDED PER CHECKLIST WITH FLAPS 15 DEGREES.TROUBLESHOT PER FIM 27-81-815-803. NO FAULTS FOUND. PERFORME

Next page: https://openairdocs.org/aircraft/N444UP/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 = 'N444UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N444UP/reports

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