# Service difficulty reports: N405UP

A list on [N405UP](https://openairdocs.org/aircraft/N405UP.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 · 189 reports

- [SDR IPXA2025091690459](https://openairdocs.org/sdr/IPXA2025091690459.md): Strap · corroded · Sep 3, 2025 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. INSTALLED 1EA REPAIR DOUBLER (1), 1EA STRAP (2), 1EA FILLER (3), 1EA FILLER (4) AND 9EA NUTPLATES ON APU AIR INLET SUPPORT STRUCTURE AT STA 1825 BETWEEN STGRS 3R AND 6R IAW B757-200PF SRM 53-80-15
- [SDR IPXA2025091653930](https://openairdocs.org/sdr/IPXA2025091653930.md): Support Angle · corroded · Aug 31, 2025 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > APU INLET SUPPORT STRUCTURE FWD STRAP O/B END SHOWS SIGNS OF CORROSION, HAS 3 EA NUT PLATES PULLED THROUGH STRAP WHITH A LAYER OF WHITE POWDER. REMOVED AND REPLACED SUPPORT ANGLES IAW SRM 51 GUIDELINES, USING THE ORIGINAL PARTS AS SAMPLE IAW UPS GMM REV 12
- [SDR IPXA2025042577738](https://openairdocs.org/sdr/IPXA2025042577738.md): Flap System · warning message · Apr 22, 2025 · N405UP · Boeing 75724APF · Trailing Edge Flap Control System
  > ON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT.REMOVED & REINSTALLED #1 FWD TE FLAP TRACK FAIRING. IAW AMM 27-51-31-422-068.(FWD AND AFT FAIRING) COMPLETE, REPAIR COMPLETE. OPS CHECK NORMAL PER AMM 27-51-00-715-00
- [SDR IPXA2025042377738](https://openairdocs.org/sdr/IPXA2025042377738.md): Transmission · tripped · Apr 22, 2025 · N405UP · Boeing 75724APF · Trailing Edge Flap Control System
  > EMERGENCY DECLARED, ON APPROACH FLAP SELECTOR TO 25 TE FLAP DISAGREE EICAS, FLAPS REMAIN 20, USED CHECKLIST ALT. FLAPS TO 25 T/S REF FIM 27-51 FAULT TREE 808, FOUND LH WING FLAP TRANSMISSIONS #1 & #4 OVERLOAD INDICATORS POPPED. SEE BARCODES T3F18E006J294 & T3
- [SDR IPXA2024100791720](https://openairdocs.org/sdr/IPXA2024100791720.md): Heater · warning message · Oct 1, 2024 · N405UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > ON PREFLIGHT AFTER ALL WINDOW HEAT SWITCHED SELECTED ON L SIDE WINDOW EICAS AND OVERHEAD INOP LIGHT ILLUMINATED REVERSED DMP. REMOVED AND REPLACED L2 WINDOW IRW 56-11-02/401. OPS/LEAK CHECK GOOD. THIS CLEARS 2825620. PLACARD REMOVED.
- [SDR IPXA2024100191720](https://openairdocs.org/sdr/IPXA2024100191720.md): Heater · faulted · Oct 1, 2024 · N405UP · Boeing 75724APF · Windshield/Door Rain/Ice Removal
  > *** SDR FILED OPEN *** ON PREFLIGHT AFTER ALL WINDOW HEAT SWITCHED SELECTED ON L SIDE WINDOW EICAS AND OVERHEAD INOP LIGHT ILLUMINATED ITEM PLACED ON DEFERRAL PER MEL 30-41-1-2. PLACARD INSTALLED. DMP APPLIED
- [SDR IPXA2024052294935](https://openairdocs.org/sdr/IPXA2024052294935.md): Outflow Valve · malfunctioned · May 22, 2024 · N405UP · Boeing 75724APF · Pressure Regulator/Outflow Valve
  > **EMERG DECLARED**CABIN ALT WARNING CAME ON & DESCENDED TO 25000 FT. RAN THE QRH & WARNING WENT OUT THEN OVERBOARD EX VLV OPEN ON STAT MSG. PILOTS REPORTED OUTFLOW VALVE & CABIN PRESSURIZATION WORKED PROPERLY DURING QRH PROCEDURE. PERF PRESSURE CONTROL SYSTEM
- [SDR IPXA2023112660660](https://openairdocs.org/sdr/IPXA2023112660660.md): Tee Angle · corroded · Nov 12, 2023 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: WTB T-CHORD STRUCTURE AT STA 900, BL 0 HAS EXFOLIATED CORROSION. INSTALLED T-CHORD AND 8 (EA) SPLICE PLATES AT STA 900 I.A.W SRM 51-70-12-OG-O DETAIL VIII AND SRM 51-40-02-0G. INSTALLED PANEL 193FL PER SRM 51-40-02. REVIEWED
- [SDR IPXA2023112621920](https://openairdocs.org/sdr/IPXA2023112621920.md): Spar · corroded · Nov 9, 2023 · N405UP · Boeing 75724APF · Wing Spar
  > FAULT-RIGHT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. NO DOT. INSTALLED PANEL 196AR IAW SRM 51-40-02. REVIEWED
- [SDR IPXA2023112621836](https://openairdocs.org/sdr/IPXA2023112621836.md): Spar · corroded · Nov 9, 2023 · N405UP · Boeing 75724APF · Wing Spar
  > FAULT-LEFT WING UPPER EXTEIOR SURFACE STA 150 TO STA 204 SHOWS SPOTS WITH CORROSION. DOT 68-01. INSTALLED PANEL 195AL PER SRM 51-40-02. REVIEWED
- [SDR IPXA2023113099488](https://openairdocs.org/sdr/IPXA2023113099488.md): Access Door · unknown · Nov 8, 2023 · N405UP · Boeing 75724APF · Doors
  > FWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W) BOTH IB AND OB HINGES HAS WEAR BUSHINGS. 89-096. UPON FURTHER INVESTIGATION DOOR HINGES FOUND TO BE IN SERVICEABLE CONDITION I.A.W AMM 52-48-01-404-005.
- [SDR IPXA2023113099411](https://openairdocs.org/sdr/IPXA2023113099411.md): Door Latch · gouged · Nov 8, 2023 · N405UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES. 89-095. BLENDED OUT GOUGES ON UPPER AND LOWER LATCHES OF CREW ENTRY DOOR. PER STEP 1 OF SREO-14721-REQ001. PERFORMED SURFACE HFEC INSP. AT CREW ENTRY DOOR LATCHES UPPER AND LOWER IAW NTM PART
- [SDR IPXA2023110999411](https://openairdocs.org/sdr/IPXA2023110999411.md): Unknown · unknown · Nov 8, 2023 · N405UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR LATCHES UPPER AND LOWER 2EA APPEAR TO HAVE GOUGES. OPEN
- [SDR IPXA2023110999488](https://openairdocs.org/sdr/IPXA2023110999488.md): Unknown · unknown · Nov 8, 2023 · N405UP · Boeing 75724APF · Cargo/Baggage Doors
  > FWD EXTERNAL ACCESS DOOR 113 AL ( AREA FWD OF NLG W/W) BOTH IB AND OB HINGES HAS WEAR BUSHINGS. OPEN
- [SDR IPXA2023112475686](https://openairdocs.org/sdr/IPXA2023112475686.md): Frame · none · Nov 7, 2023 · N405UP · Boeing 75724APF · Fuselage Main, Frame
  > *MAJOR REPAIR* FAULT: EXISTING FRAME REPAIR FOUND AT AFT CARGO COMPARTMENT STA 1240 R/H. VERIFIED ALL WORK ACCOMPLISHED IAW EO-87166-REQ1 AND VTMAE EA 757-5360-27-A3424 REV. JOB COMPLETE. AUDIT COMPLETE. REVIEWED
- [SDR IPXA2023111979160](https://openairdocs.org/sdr/IPXA2023111979160.md): Skin · out of limits · Nov 7, 2023 · N405UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > *SDR FILED OPEN* FAULT: PUNCTURE BETWEEN STA 1400- 1420. STR 24-25 L/H. GIVEN THE OK TO APPLY TOP COAT. SUPPLEMENTAL INSPECTIONS DEFERRED IAW B757-200PF REV 118.00 SRM CHAPTER 53-00-01-2R-29, TABLE 206, FOR ZONE A.
- [SDR IPXA2022012178121](https://openairdocs.org/sdr/IPXA2022012178121.md): Flap System · fault message · Jan 19, 2022 · N405UP · Boeing 75724APF · Trailing Edge Flap Control System
  > INSPECTION TYPE: A, EMERGENCY DECL'D* NO EQUIP USED*LANDED UNEVENTFULLY ON APPROACH WHEN SLECTING FLAPS 25 RECIEVED TE FLAP DISAGREE EICAS MESSAGE. COMPLETED QRH PROCEDURE. MESSAGE EXTINGUISHED WHEN ALT TE WAS SELECTEDPERFORMED NORMAL OPER OF FLAP/SLAT SYSTE
- [SDR IPXA2022011077696](https://openairdocs.org/sdr/IPXA2022011077696.md): None · unreliable · Jan 9, 2022 · N405UP · Boeing 75724APF · Pitot/Static System
  > INSPECTION TYPE:NA**ATB** AIRSPEED UNRELIABLE ON DEPARTURE. RAN QRH PROCEDURE. RETURN TO SDFREPLACED CAPT / L/H ADC & FOUND LEAK IN PITOT STATIC PORT SEE THIS PG ITEM #2 & #3 FOR CORRECTIVE ACTIONS
- [SDR IPXA2021111676025](https://openairdocs.org/sdr/IPXA2021111676025.md): None · none · Nov 16, 2021 · N405UP · Boeing 75724APF · Wing, Control Surfaces
  > INSPECTION TYPE:SEG4LEFT WING O/B FLAP TOP SURFACE REPAIR IS DELAMINATED. DOT 18-10REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 57-53-01-2R-1.
- [SDR IPXA2021111676024](https://openairdocs.org/sdr/IPXA2021111676024.md): None · none · Nov 16, 2021 · N405UP · Boeing 75724APF · Standard Practices/Structures
  > INSPECTION TYPE:SEG4FOUND A DELAMINATED AREA ON THE UPPER SURFACE OF THE L/H O/B MAIN FLAP. LOCATED 31" IN FROM THE O/B SIDE OF THE PART, AND 8.5" UP FROM THE T/E. FOUND DURING INSP FOR E.O. B757-5750-36691-A.REPAIRED PANEL IAW B757 SRM 51-70-07-OG PER SRM 57-
- [SDR IPXA2021111575994](https://openairdocs.org/sdr/IPXA2021111575994.md): None · none · Nov 7, 2021 · N405UP · Boeing 75724APF · Vertical Stabilizer
  > INSPECTION TYPE:CTHE VERT. STAB. UPR FWD TORQUE BOX PANEL HAS A DISBONDED DENT AT FSS 321.046 ON THE L/H SIDE.REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 55-30-01-2R-4
- [SDR IPXA2021111575993](https://openairdocs.org/sdr/IPXA2021111575993.md): None · none · Nov 7, 2021 · N405UP · Boeing 75724APF · Standard Practices/Structures
  > INSPECTION TYPE:CTHE VERT. STAB. R/H LWR FWD TORQUE BOX HAS MULTIPLE DENTS FROM HAIL DAMAGE. AFTER CLEAN UP AND PAINT REMOVAL, ONE DISBOND FOUNDREPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 PER SRM 55-30-01-2R-5
- [SDR IPXA2021031566817](https://openairdocs.org/sdr/IPXA2021031566817.md): Seat Track · damaged · Mar 14, 2021 · N405UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:N/APOS 11/12 SEAT TRACK DAMAGE.REPAIRED SEAT TRACK IAW EO B757-5310-79593.
- [SDR IPXA2019120659733](https://openairdocs.org/sdr/IPXA2019120659733.md): Tube · damaged · Dec 3, 2019 · N405UP · Boeing 75724APF · Cabin Cooling System
  > AT 27,000 FT, CABIN ALTITUDE RED WARNING EICAS, CREW PERFORMED AN EMERGENCY, DESCENDED TO 10,000 FT, APPROACHING 10,000 FT, THE CABIN ALTITUDE AUTO STATUS MESSAGE, CREW HEARD A LOUD AIR HISSING NOISE, COULDN`T DETERMINE SOURCE OF SOUND. REPOSITIONED &
- [SDR IPXA2019113049525](https://openairdocs.org/sdr/IPXA2019113049525.md): Warning Message · false activation · Nov 30, 2019 · N405UP · Boeing 75724APF · Cabin Cooling System
  > CLIMBING THRU 28,000' THE CABIN ALT WARNING EICAS WAS RECEIVED. NO OTHER INDICATIONS LEFT PACK WAS OFF AND WE TURNED IT BACK ON. CABIN ALT WAS ACCEPTABLE BELOW 20,000.PER CERT LEAVE BOTH PACKS ON-PERFORMED PRESS DECAY CHECK, OP'S CHECKED NORMAL, BITE CHECK OF
- [SDR IPXA2019111859042](https://openairdocs.org/sdr/IPXA2019111859042.md): Angle · cracked · Nov 15, 2019 · N405UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:A300#2 PYLON AFT FAIRING FWD END RH SIDE FWD CORNER ANGLE PLATE CRACKEDREMOVED AND REPLACED IAW SRM 51-40-02
- [SDR IPXA2019112049213](https://openairdocs.org/sdr/IPXA2019112049213.md): Floor Panel · damaged · Nov 14, 2019 · N405UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEGFLOOR BOARD PANBEL #252XTF HAS DAMAGED CORNERFABBED PNL 252XTF FROM 5024N00001SS-G BTCH#3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2019112769454](https://openairdocs.org/sdr/IPXA2019112769454.md): Stringer Clip · broken · Nov 12, 2019 · N405UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1STATION 297,STRINGER 17L CLIP BROKENFABRICATED NEW BRACKET PER DRAWING #232N1504
- [SDR IPXA2019112769453](https://openairdocs.org/sdr/IPXA2019112769453.md): Stringer Clip · broken · Nov 12, 2019 · N405UP · Boeing 75724APF · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C1STATION 297,STRINGER 17L CLIP BROKENFABRICATED NEW BRACKET PER DRAWING #232N1504
- [SDR IPXA2019112769449](https://openairdocs.org/sdr/IPXA2019112769449.md): Seat Track · worn · Nov 9, 2019 · N405UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEGMAIN DECK SEAT TRACK SCALLOP LBL 45.5 DAMAGED BETWEEN STA 610-620WORK PER 757-200 PF SRM 53-30-52-2-R PROCEDURE 1
- [SDR IPXA2019111869055](https://openairdocs.org/sdr/IPXA2019111869055.md): Floor Panel · delaminated · Nov 8, 2019 · N405UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEGFLIGHT DECK FLOOR PANEL 212XAF DELAMINATEFABBED PNL 212XAF FROM 5024N400001SS-G BTH# 0003546253 PER SREO B757-5320-9692-K
- [SDR IPXA2019111549013](https://openairdocs.org/sdr/IPXA2019111549013.md): Angle · cracked · Nov 7, 2019 · N405UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:C1#1 PYLON AFT FAIRING FWD END RH SIDE HAVE CRACKED ANGLEREMOVED AND REPLACED IAW SRM 51-40-2
- [SDR IPXA2019112769458](https://openairdocs.org/sdr/IPXA2019112769458.md): Panel · delaminated · Nov 6, 2019 · N405UP · Boeing 75724APF · Vertical Stabilizer
  > INSPECTION TYPE:C1LH VERTICAL STAB LOWER FWD TORQUE BOX PANEL DELAMINATED STARTING AT TOP EDGE EXTENDING DOWN APPROX 2.0 FEET AND SPANNING THE ENTIRE WIDTH OF PANELREMOVED AND REPLACED
- [SDR IPXA2018091984133](https://openairdocs.org/sdr/IPXA2018091984133.md): Bulb · inoperative · Sep 18, 2018 · N405UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHT HAS FIVE BULBS INOPERATIVE. REPLACED THE FIVE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2017111523600](https://openairdocs.org/sdr/IPXA2017111523600.md): Floor Support · cracked · Nov 12, 2017 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C-13, E & E BAY FLOOR SUPPORT IS CRACKED BS 460. REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR IPXA2017111623634](https://openairdocs.org/sdr/IPXA2017111623634.md): Skin · dented · Nov 1, 2017 · N405UP · Boeing 75724APF · Cargo/Baggage Doors
  > INSPECTION TYPE: C-18, AFT CARGO DOOR EXTERNAL SKIN FOUND DENTED JUST BELOW LATCH HANDLE. REPAIRED THE DOOR SKIN IAW SRM 52-30-01, REPAIR 4.
- [SDR IPXA2017110723358](https://openairdocs.org/sdr/IPXA2017110723358.md): Floor Panel · punctured · Nov 1, 2017 · N405UP · Boeing 75724APF · Fuselage Floor Panel
  > E&E FLOOR PANEL 119BF HAS PUNCTURE. FAB NEW PANEL 119BF IAW GMM 09-10 AND DWG 284N1033.
- [SDR IPXA2017111523601](https://openairdocs.org/sdr/IPXA2017111523601.md): Skin · dented · Oct 29, 2017 · N405UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > DENT 41 INCHES LEFT OF RUDDER, 1.3 INCHES IN DIAMETER. REPAIRED IAW SRM 51-70-10, REPAIR 2.
- [SDR IPXA2017111323496](https://openairdocs.org/sdr/IPXA2017111323496.md): Panel · dented · Oct 29, 2017 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > DENT 16" LEFT OF RUDDER, 4.2" FORWARD OF AFT RIVET ROW 1.4" IN DIAMETER. PERMANENT REPAIR. INSTALLED INTERIM REPAIR IAW SRM 51-70-10 REPAIR 2.
- [SDR IPXA2017111323497](https://openairdocs.org/sdr/IPXA2017111323497.md): Panel · dented · Oct 29, 2016 · N405UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > DENT 41" LEFT OF RUDDER 1.3" IN DIAMETER. PERMANENT REPAIR. INSTALLED INTERIM IAW SRM 51-70-10 REPAIR 2.
- [SDR IPXA2015091893686](https://openairdocs.org/sdr/IPXA2015091893686.md): Container · damaged · Sep 18, 2015 · N405UP · Boeing 75724APF · Life Jacket
  > F/O'S LIFE VEST BAG TORN. R & R F/O'S LIFE VEST IAW MM 25-11-00.
- [SDR IPXA2015051589114](https://openairdocs.org/sdr/IPXA2015051589114.md): Bulb · inoperative · May 15, 2015 · N405UP · Boeing 75724APF · Emergency Lighting
  > EMERGENCY LIGHT HAS SIX INOPERATIVE BULBS. REPLACED THE INOPERATIVE BULBS IAW AMM 33-51-01-2.
- [SDR IPXA2014080483860](https://openairdocs.org/sdr/IPXA2014080483860.md): Skin · damaged · Aug 4, 2014 · N405UP · Boeing 75724APF · Trailing Edge Flaps
  > LEFT OTBD T/E FLAP LOWER SKIN DAMAGED. REPAIRED IAW EO B757-5750-55118-A.
- [SDR IPXA2014021281899](https://openairdocs.org/sdr/IPXA2014021281899.md): Frame · dented · Feb 11, 2014 · N405UP · Boeing 75724APF · Fuselage Main, Frame
  > DURING INSPECTION 4C16, AFT CARGO BAY FRAME, BS 1600 ABOVE S26L DENTED. CHECK LIMITS NO DENTS ALLOWED IAW SRM 53-00-07-1A-1, FIG 101 (SHEET 1) TRIMMED OUT DENT IAW SRM 53-00-07-2R-5, FIG 201, SHEET 1, STEP 1. HFEC CUTOUT IAW NTM 51-00-19. NO DEFECTS.
- [SDR IPXA2014021481914](https://openairdocs.org/sdr/IPXA2014021481914.md): Frame · dented · Feb 3, 2014 · N405UP · Boeing 75724APF · Fuselage Main, Frame
  > DURING INSPECTION 4C16, AFT CARGO BAY, FRAME BS 1340 ABOVE S26R DENTED. ACCOMPLISHED FRAME REPAIR IAW SRM 53-00-07, REPAIR 5, DETAIL-1.
- [SDR IPXA2014021481913](https://openairdocs.org/sdr/IPXA2014021481913.md): Frame · dented · Feb 3, 2014 · N405UP · Boeing 75724APF · Fuselage Main, Frame
  > DURING INSPECTION 4C16, AFT CARGO BAY FRAME BS 1320 ABOVE STINGER 26R DENTED. ACCOMPLISHED FRAME REPAIR, IAW SRM 53-00-07. REPAIR 5, DETAIL 1.
- [SDR IPXA2014021281898](https://openairdocs.org/sdr/IPXA2014021281898.md): Frame · dented · Feb 3, 2014 · N405UP · Boeing 75724APF · Fuselage Main, Frame
  > DURING INSPECTION 4C16, AFT CARGO BAY FRAME, BS 1240 ABOVE S26L DENTED. TRIMMED OUT DENT IAW SRM 53-00-07-2R-6, STEP 4C. HFEC CUTOUT IAW PT6 NTM 51-00-19. NO DEECTS.
- [SDR IPXA2014021081832](https://openairdocs.org/sdr/IPXA2014021081832.md): Floor Panel · damaged · Feb 2, 2014 · N405UP · Boeing 75724APF · Fuselage Floor Panel
  > C16 INSPECTION, MAIN DECK FLOOR PANEL 242XMF HAS TWO DAMAGED HOLES. FABRICATED NEW FLOOR PANE IAW SREO EO B757-5320-9692-H.
- [SDR IPXA12575334](https://openairdocs.org/sdr/IPXA12575334.md): Wedge · dented · Sep 16, 2012 · N405UP · Boeing 75724APF · Leading Edge Devices
  > NR 5 SLAT T/E WEDGE DENTED WITH DELAMINATION. REPAIRED IAW EO B757-5750-48255B.
- [SDR IPXA12571808](https://openairdocs.org/sdr/IPXA12571808.md): Floor Panel · cracked · Feb 20, 2012 · N405UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C-CK, MAIN CARGO FLOOR PANEL 252XTF IS CRACKED, DELAMINATED AND MISSING INSERTS. FABRICATED MAIN CARGO FLOOR PANEL 252XTF IAW EO B757-5320-9692-H.

Next page: https://openairdocs.org/aircraft/N405UP/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 = 'N405UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N405UP/reports

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