# Service difficulty reports: N465UP

A list on [N465UP](https://openairdocs.org/aircraft/N465UP.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 · 208 reports

- [SDR IPXA2026061235641](https://openairdocs.org/sdr/IPXA2026061235641.md): Doubler · corroded · Jun 12, 2026 · N465UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > TOILET/WASTE PANEL DRAIN VALVE ASSEMBLY, PAN ASSY (INTERNAL AND EXTERNAL DOUBLER) CORRODED
- [SDR IPXA2026060510499](https://openairdocs.org/sdr/IPXA2026060510499.md): Valve · faulted · Jun 4, 2026 · N465UP · Boeing 75724APF · Waste Disposal System
  > DURING REQUEST OF LEAK CHECK VERIFICATION. FOUND FWD RHS TOILET/WASTE PANEL DRAIN VALVE ASSEMBLY, PAN ASSY (INTERNAL AND EXTERNAL DOUBLER) CORRODED, INSTALLED NEW WASTE DRAIN VALVE ASSY PN: 331-0001-01, NEW GASKET PN: 2174, SAME FIBERGLASS DUCT ON FWD TOILET
- [SDR IPXA2025090405528](https://openairdocs.org/sdr/IPXA2025090405528.md): Seal · dirty · Sep 4, 2025 · N465UP · Boeing 75724APF · Passenger/Crew Doors
  > L1 DOOR IS VERY DIFFICULT TO OPEN. ADJUSTED AND CLEANED L1 DOOR SEAL AND DOOR LINING REF. AMM 52-12-00. DOOR OPS CHECKS NORMAL.
- [SDR IPXA2025052810387](https://openairdocs.org/sdr/IPXA2025052810387.md): Hydraulic System · warning message · May 28, 2025 · N465UP · Boeing 75724APF · Hydraulic System, Main
  > **ATB** ON TAKE OFF AFTER- 80 KTS, LEFT HYD QTY IN FLIGHT PROGRESSED TO (L) HYD SYS PRESS, ALT GEAR EXTEND, AND ALT FLAP EXTEND. FOUND FLAP/SLAT DEPRESSURIZATION MODULE PRESSURE SWITCH LEAKING. REPLACED REF AMM 27-51-29-422-026. OPS AND LEAK CHECKS GOOD.
- [SDR IPXA2025022783755](https://openairdocs.org/sdr/IPXA2025022783755.md): Retainer · corroded · Feb 21, 2025 · N465UP · Boeing 75724APF · Landing Gear Doors
  > FAULT: Z193 LH MLG WW DOOR TANG FWD BULB SEAL RETAINER IS EXFOLIATED. VERIFIED REMOVAL OF CORROSION FROM WW DOOR TANG BULB SEAL RETAINER PN 1496016-41. ORIGINAL THICKNESS.050,.046 MATERIAL REMAINING FINDING THE RETAINER TO BE WITHIN LIMITS IAW SRM 53--00-71-1
- [SDR IPXA2025030354337](https://openairdocs.org/sdr/IPXA2025030354337.md): Fastener · missing · Feb 14, 2025 · N465UP · Boeing 75724APF · Engine Thrust Reverser
  > FAULT-STR-ZONE 400. ENG #2 O/B T/R FWD UPPER CHANNEL HAS (1EA) FASTENER MISSING. DOT 28-81. INSTALLED FASTENER (1EA) AT ENG #2 O/B T/R FWD UPPER CHANNEL, IAW B757-200PF 51-40-02. FASTENER P/N CR3212-5-04, BATCH#: 0004334085. REVIEWED
- [SDR IPXA2025030636262](https://openairdocs.org/sdr/IPXA2025030636262.md): Access Door · delaminated · Feb 13, 2025 · N465UP · Boeing 75724APF · Wing Miscellaneous Structure
  > PANEL 532HZ IS DELAMINATED.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 122 CHAPTER 51-70-07 (250 DEGREE CURE), PER SRM 57-20-09-2R-1.CLEANED & EVALUATED PANEL 532HZ AND FOUND IT TO BE REPAIRABLE IAW 757-SRM-51-70-07-0G-0 PARA 5.J & PARA 5.H FIG.13.PREPARED AND A
- [SDR IPXA2025030636145](https://openairdocs.org/sdr/IPXA2025030636145.md): Panel · delaminated · Feb 13, 2025 · N465UP · Boeing 75724APF · Wing Miscellaneous Structure
  > COMP DRY BAY DOOR CUT OUT HAS COMPOSITE DELAM. ACCOMPLISHED REPAIR PER VT-MAE EA 757-5720-27-A3804.
- [SDR IPXA2025021397102](https://openairdocs.org/sdr/IPXA2025021397102.md): Strip · cracked · Feb 12, 2025 · N465UP · Boeing 75724APF · Engine Thrust Reverser
  > FAULT-STR- ZONE 420, ACCESS PANEL 425BL METAL STRIP EDGE CRACKED. DOT 68-16.REMOVED SEAL, HINGE-REAR WITH CRACK IAW SRM B757-200 TASK: 51-40-02.INSTALLED NEW SEAL, HINGE-REAR WITH (3EA) NAS1097AD4-7 BATCH: 0003968643 IAW SRM B757-200 TASK: 51-40-02.
- [SDR IPXA2025022693724](https://openairdocs.org/sdr/IPXA2025022693724.md): Floor Panel · cracked · Feb 11, 2025 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT-STR-ZONE 100. AFT CARGO COMPT FLOOR PANEL 153BF HAS A CRACK. DOT 28-57.FABRICATED NEW FLOOR PANEL 153BF IAW GMM 09.08.01.03.
- [SDR IPXA2025021378219](https://openairdocs.org/sdr/IPXA2025021378219.md): Bracket · cracked · Feb 11, 2025 · N465UP · Boeing 75724APF · Cargo/Baggage Doors
  > FAULT: STR Z800 FWD LWR CARGO DOOR HAS A CRACK IN AN "L" BRACKET LOCATED IN THE FWD UPPER CORNER. DOT 06677-03.INSTALLED BRACKET WITH (3EA) BACR15FT6D6C, BATCH: 0004364973 & (2EA) CR3213-6-05, BATCH: 0004214429 & (1EA) HL12VF6-6, BATCH: 0004208818 & (1EA) MS2
- [SDR IPXA2025021271069](https://openairdocs.org/sdr/IPXA2025021271069.md): Skin · cracked · Feb 10, 2025 · N465UP · Boeing 75724APF · Wing, Plate/Skin
  > LH WING LEADING EDGE UPPER SURFACE AT SLAT #4 LOCATION, HAS 1 CRACK. DOT 28-38. MADE A REPLACEMENT SKIN FROM 2024-T3 CLAD SHEET, 0.100''. PER E.A. #: 757-5741-27-A3790 PRELIMINARY 1, STEP 8. P/N: 2024-T3.100C, BATCH: 0004322815. INSTALLED FASTENERS CODE A, B
- [SDR IPXA2025021577164](https://openairdocs.org/sdr/IPXA2025021577164.md): Floorbeam · corroded · Feb 10, 2025 · N465UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FAULT-STR- ZONE 142 MAIN CARGO COMPARTMENT RIGHT SIDE STA 1020, BL 0 TO RBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. CLEANED MAIN CARGO COMPARTMENT /RH SIDE STA 1020, BL 0 TO RBL 24.5 FLOOR BEAM SUPPORT CHANNEL IAW SOPM 20-30-03. AFTER FURTHER IN
- [SDR IPXA2025021577074](https://openairdocs.org/sdr/IPXA2025021577074.md): Support Channel · corroded · Feb 10, 2025 · N465UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > MAIN CARGO COMPARTMENT LEFT SIDE STA 1050 BL 0 TO LBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-02 FR-68. LOCATED AND DRILLED NEW TEE SUPORT IAW SRM B757-200 TASK: 51-40-05. INSTALLED NEW TEE IAW SRM B757-200 TASK: 51-40-02.
- [SDR IPXA2025022576954](https://openairdocs.org/sdr/IPXA2025022576954.md): Floorbeam · corroded · Feb 10, 2025 · N465UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > MAIN CARGO COMPARTMENT LEFT SIDE STA 1050 LBL 45.5 TO LBL 65.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-01 FR-68. REMOVE AND REPLACE 1 EACH FLOORBOARD SUPPORT TEE (P/N: 144N5005-4) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51
- [SDR IPXA2025021760646](https://openairdocs.org/sdr/IPXA2025021760646.md): Cam · gouged · Feb 9, 2025 · N465UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/006. EL-69. BLEND OUT GOUGE ON MAIN CREW DOOR LWR CAMLATCH IAW B757-200PF, SRM 51-10-02. SURFACE HFEC PERFORMED ON MAIN CREW DOOR LOWER CAM LATCH BLENDED AREA. NO DEFECTS FOUND IAW NTM 51-00-21 T
- [SDR IPXA2025021760600](https://openairdocs.org/sdr/IPXA2025021760600.md): Latch · gouged · Feb 9, 2025 · N465UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/005. EL-69. SURFACE HFEC PERFORMED ON MAIN CREW DOOR UPPER CAM LATCH BLENDED AREA. NO DEFECTS FOUND IAW NTM 51-00-21 T96525.
- [SDR IPXA2025021060646](https://openairdocs.org/sdr/IPXA2025021060646.md): Cam · gouged · Feb 9, 2025 · N465UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE.
- [SDR IPXA2025021060600](https://openairdocs.org/sdr/IPXA2025021060600.md): Cam · gouged · Feb 9, 2025 · N465UP · Boeing 75724APF · Passenger/Crew Doors
  > MAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE.
- [SDR IPXA2025020848485](https://openairdocs.org/sdr/IPXA2025020848485.md): Floorbeam · corroded · Feb 8, 2025 · N465UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FAULT: Z100 STR FS 1240 RBL 22 TO RBL 30 FWD FLANGE OF LOWER TEE CHORD HAS SEVERE INTERGRANULAR CORROSION. INSTALLED T-CHORD AN ANGLES ON STR FS 1240 RBL IAW B757-200 SRM 51-40-02 AND SRM 51-70-12-0G-0 DETAIL VIII FIGURE 1 SHEET 7. REVIEWED
- [SDR IPXA2025022851520](https://openairdocs.org/sdr/IPXA2025022851520.md): Floorbeam · corroded · Feb 8, 2025 · N465UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FAULT: Z100 STR FS 900 BETWEEN RBL 12 TO RBL 16.5 LOWER TEE CHORD HAS CORROSION. INSTALLED OUTBOARD CHORD AND 8(EA) REPAIR PLATES AT STA 900 I.A.W SRM 51-70-12-OG AND SRM 51-40-02-OG. REVIEWED.
- [SDR IPXA2025022751440](https://openairdocs.org/sdr/IPXA2025022751440.md): Floorbeam · corroded · Feb 8, 2025 · N465UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FS 1037 RBL 59 LOWER TEE CHORD HAS CORROSION FWD AND AFT FLANGE. RESTORED SURFACE PROTECTION AT NEW T-CHORD IAW B757-200PF SRM 51-20-01-0G-0. ALODINE P/N; ALODINE1132 B/N;0004315010 PRIMER P/N;10-P4-2/2TU B/N; 0004341746 PAINT WHITE P/N; PG6-W2K4Q B/N; 4361130
- [SDR IPXA2025020848535](https://openairdocs.org/sdr/IPXA2025020848535.md): Tee Angle · corroded · Feb 8, 2025 · N465UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FS 1238- FS 1240 RBL 31 INBD LOWER TEE CHORD FLANGE HAS SEVERE INTERGRANULAR CORROSION. REMOVE AND REPLACE 1 EACH RBL 30.75 (P/N: 149N7633-14) LOWER TEE CHORD AT STA 1240 PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS. VERIFIED I
- [SDR IPXA2024060535801](https://openairdocs.org/sdr/IPXA2024060535801.md): Idg · faulted · May 31, 2024 · N465UP · Boeing 75724APF · AC Generator-Alternator
  > **SUPPLEMENTAL SDR**L GEN DRIVE EICAS MESSAGE DURING DECENT PHASE OF FLIGHT. COMPLIED WITH QRH PROCEDURE R&R LH ENGINE IDG REF 757 AMM 24-11-01 OPS AND LEAK CK GOOD DMP REVERSED PLACARD REMOVED OK TO CONTINUE
- [SDR IPXA2024053135801](https://openairdocs.org/sdr/IPXA2024053135801.md): Warning Light · illuminated · May 31, 2024 · N465UP · Boeing 75724APF · AC Generator-Alternator
  > LEFT GEN DRIVE EICAS MESSAGE DURING DECENT PHASE OF FLIGHT. COMPLIED WITH QRH PROCEDURE DEFERRED LH IDG PER MEL 24-00-1. C/W DMP. VERIFIED IDG DISCONNECTED WITH ENGINE RUN. PLACARD INSTALLED *** PIREP: ARRIVED AT THE AIRCRAFT COCKPIT AND SMELLED HEAVY ACETONE/
- [SDR IPXA2024012502634](https://openairdocs.org/sdr/IPXA2024012502634.md): Door · stuck · Jan 24, 2024 · N465UP · Boeing 75724APF · Doors
  > CREW ENTRY DOOR JAMMED AND WAS UNABLE TO ENTER AIRCRAFT WITHOUT EFFORT OF SOMEONE INSIDE THE COCKPIT, WAS OPENED WITH GREAT DIFFICULTY CLEANED BOTTOM OF SEAL AFT OF ENTRY DOOR IAW AMM 52-09-00-801. DOOR OPENS NORMALLY.
- [SDR IPXA2023112998124](https://openairdocs.org/sdr/IPXA2023112998124.md): Flap · warning message · Nov 28, 2023 · N465UP · Boeing 75724APF · Leading Edge Devices
  > *EMERGENCY DECLARED* ON APPROACH LE FLAP DISAGREE LIGHT W/ EICAS CAUTION MESSAGE. WENT AROUND AND LANDED W/ FLAPS 20 USING ALTN FLAP EXTENSION CHECKLIST. PERFORMED FSEU BITE PER FIM 27-51-00/101 FIG 104. NO EXISTING FAULTS FOUND. PERFORMED FIM 27-81 FAULT TREE
- [SDR IPXA2023042793003](https://openairdocs.org/sdr/IPXA2023042793003.md): Landing Gear · inoperative · Apr 27, 2023 · N465UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* *EMERGENCY DECLARED* AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT- CHECKLIST COMPLETED GEAR SHOWED 3 GREE, LANDING UNEVENTFUL. DEFERRED PER MEL 32-3-0-1, LANDING GEAR ADJ SYS VMO SELECTED TO 270, DMP C/W. WMO/MMO SWITCHED
- [SDR IPXA2023050193059](https://openairdocs.org/sdr/IPXA2023050193059.md): Landing Gear · warning message · Apr 23, 2023 · N465UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:NA*ATB* AFTER SELECTING THE GEAR TO UP THE GREEN NOSE GEAR LIGHT REMAIN ILUMINATED AS DID THE AMBER DOORS AND GEAR LIGHT. EICAS SHOWED GEAR DISAGREE AND GEAR DOORS. WHEN GEAR LEVER EAS SELECTED TO DN WE HAD THREE GREEN GEAR DOWN LIGHTS AND NO A
- [SDR IPXA2023042192952](https://openairdocs.org/sdr/IPXA2023042192952.md): Warning Message · illuminated · Apr 21, 2023 · N465UP · Boeing 75724APF · Nose/Tail Landing Gear
  > INSPECTION TYPE:NA*SDR FILED OPEN* *ATB* GEAR DISAGREE AND GEAR DOOR EICAS
- [SDR IPXA2023030491513](https://openairdocs.org/sdr/IPXA2023030491513.md): Floorbeam · corroded · Feb 22, 2023 · N465UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG1*MAJOR REPAIR* MAIN CARGO COMPARTMENT, STA 1600 LBL 55, FLOOR BEAM UPPER CHORD HAS CORROSIONREPAIRED PER UPS RCD 271627 AND VT MAE EA 757-5360-27-A3150 REV-
- [SDR IPXA2023030491514](https://openairdocs.org/sdr/IPXA2023030491514.md): Skin · corroded · Feb 20, 2023 · N465UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG1#2 ENGINE PYLON INBD SKIN AT THE FWD HINGE DOOR INNER AFT LIP HAS A EXFOLIATION CORROSIONCORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE #2 ENGINE PYLON INBD FWD SKIN PER SRM 51-40-02
- [SDR IPXA2023030591540](https://openairdocs.org/sdr/IPXA2023030591540.md): Skin · corroded · Feb 18, 2023 · N465UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG1*MAJOR REPAIR* #1 ENGINE OUTBD PYLON SKIN OF VENT 433CL OPENING HAS EXFOLIATION CORROSION ON THE INNER SKINREPAIR PER UPS RCD 271422 AND VT MAE EA 757-5450-27-A3154 REV-
- [SDR IPXA2023030391502](https://openairdocs.org/sdr/IPXA2023030391502.md): Skin · corroded · Feb 18, 2023 · N465UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG1#2 ENGINE PYLON OUTBD EXTERIOR SKIN BELLOW PANEL 443AR HAS BULDGING CORROSIONREPAIRED PER EA 757-5450-27-A3152 REV-
- [SDR IPXA2021082473088](https://openairdocs.org/sdr/IPXA2021082473088.md): Radar · faulted · Aug 22, 2021 · N465UP · Boeing 75724APF · Weather Radar System
  > INSPECTION TYPE:N/A**AIR TURNBACK** ENROUTE RECIVED ON BOTH CAPT & F/O PFD EXR FAIC AND EXR WEAK AT FL340 ALSO RECEIVED A EXR SYS STATUS MESSAGE DUE TO ENROUTE WEATHER - RESULTED IN AN ATBREMOVED & REPLACED WEATHER READAR TRANSCEIVER PER AMM 34-43-01-401. NO F
- [SDR IPXA2021042468568](https://openairdocs.org/sdr/IPXA2021042468568.md): Barrier · cracked · Apr 24, 2021 · N465UP · Boeing 75724APF · Fuel Storage
  > INSPECTION TYPE:SEG2 EA CRACKS ON THE LH WING DRY BAY BARRIER (P/N: 112N8004-15) COMMON TO DRY BAY ACCESS DOOR 532HZACCOMPLISHED WORK PER PRELIM 1 EA 757-5720-27-A2571 REV AND PRELIM 2 EA 757-5720-27-A2571 REV
- [SDR IPXA2021042068451](https://openairdocs.org/sdr/IPXA2021042068451.md): Fitting · cracked · Apr 20, 2021 · N465UP · Boeing 75724APF · Wing, Attach Fittings
  > INSPECTION TYPE:SEGREMOVE O/B DRAG LINK FITTING P/N 653N0002-15 FROM #1 PYLON. REMOVED AND REPLACED IAW EA 757-5720-27-A2563 REV
- [SDR IPXA2021042068450](https://openairdocs.org/sdr/IPXA2021042068450.md): Fitting · cracked · Apr 20, 2021 · N465UP · Boeing 75724APF · Nacelle/Pylon, Main Frame
  > INSPECTION TYPE:SEGREMOVE #1 PYLON I/B DRAG LINK FITTING P/N: 653N0002-13REMOVED AND REPLACED IAW EA# 757-5720-27-A2563 REV
- [SDR IPXA2021041368178](https://openairdocs.org/sdr/IPXA2021041368178.md): Seat Track · corroded · Apr 13, 2021 · N465UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:SEG4SEAT TRACK LOCATED AT STA 1060-1080 HAS CORROSIONREMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-52-1A-1 DET VII
- [SDR IPXA2021033167573](https://openairdocs.org/sdr/IPXA2021033167573.md): Skin · delaminated · Mar 31, 2021 · N465UP · Boeing 75724APF · Aerodynamic Fairings
  > INSPECTION TYPE: SEG DELAMINATION ON THE UPPER SKIN SECTION 48. REPAIRED PANEL IAW B757 SRM 51-70-10-2R-2 350 DEG F CURE PER SRM 53-80-01-2R FIG 201.
- [SDR IPXA2021030766499](https://openairdocs.org/sdr/IPXA2021030766499.md): A/C Pack · odor · Mar 6, 2021 · N465UP · Boeing 75724APF · Cabin Cooling System
  > INSPECTION TYPE:N/ASLIGHT OILY SMELL COMING FROM THE PACKS. MORE PRONOUNCED WITH THE LEFT PACK ON. AT ALTITUDE OIL PRESSURE LEFT ENGINE 51, RIGHT ENGINE 91.R+R LEFT ENGINE IAW TC #5001 (RR) OPS AND LEAK CKED GOOD. A/C OK FOR SERVICE.
- [SDR IPXA2020072097927](https://openairdocs.org/sdr/IPXA2020072097927.md): Line · unsecure · Jul 18, 2020 · N465UP · Boeing 75724APF · Hydraulic System, Main
  > EMERGENCY DECLARED, LANDED AND REQUIRED TOW FROM RUNWAY. LEFT HYD QTY EICAS C, LT HYD QTY DECREASED DURING FLIGHT TO 0.20. DRY MOTORED LT ENGINE, NO LEAKS NOTED. FOUND PRESSURE OUTLET LINE LOOSE. SECURED THE LINE IAW MM 71-00-02-844-082-P00. LEAK CHEC
- [SDR IPXA2019042294243](https://openairdocs.org/sdr/IPXA2019042294243.md): Floor Panel · delaminated · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 222XCF IS DAMAGEDFABBED PANEL 222XCF FROM 5024N400001SS-G, BATCH # 3467574 PER SREO B757-5320-9692-K
- [SDR IPXA2019042294241](https://openairdocs.org/sdr/IPXA2019042294241.md): Floor Panel · delaminated · Apr 19, 2019 · N465UP · Boeing 75724APF · Cargo Compartments
  > INSPECTION TYPE:SEG3MAIN CARGO COMPARTMENT FLOOR PANEL 231XDF IS DAMAGEDFABBED PANEL 231XDF FROM 5024N400001SS-G, BATCH # 3467574 PER SREO B757-5320-9692-K
- [SDR IPXA2019042294240](https://openairdocs.org/sdr/IPXA2019042294240.md): Floor Panel · delaminated · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 231XEF IS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941239](https://openairdocs.org/sdr/IPXA2019041941239.md): Floor Panel · damaged · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 231XHF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-53320-9692-K.
- [SDR IPXA2019041941237](https://openairdocs.org/sdr/IPXA2019041941237.md): Floor Panel · damaged · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 222XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941236](https://openairdocs.org/sdr/IPXA2019041941236.md): Floor Panel · delaminated · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE: SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XCF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941235](https://openairdocs.org/sdr/IPXA2019041941235.md): Floor Panel · delaminated · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XBF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.
- [SDR IPXA2019041941234](https://openairdocs.org/sdr/IPXA2019041941234.md): Floor Panel · damaged · Apr 19, 2019 · N465UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG3, MAIN CARGO COMPARTMENT FLOOR PANEL 221XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL PER SREO B757-5320-9692-K.

Next page: https://openairdocs.org/aircraft/N465UP/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 = 'N465UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N465UP/reports

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