# Service difficulty reports: N473UP

A list on [N473UP](https://openairdocs.org/aircraft/N473UP.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 3 · 105 reports

- [SDR IPXA2025041047242](https://openairdocs.org/sdr/IPXA2025041047242.md): Skin · corroded · Mar 14, 2025 · N473UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > RH PYLON INSIDE PANEL 443CR FWD LOWER CORNER HAS CORROSION. DOT 28-45. ACOOMPLISHED STEP 23 INSTALLED REPAIR DOUBLER I.A.W EA# 757-5450-27-A3854 PRELIMINARY 3 AND SRM 51-40-02-OG. REVIEWED
- [SDR IPXA2025031647242](https://openairdocs.org/sdr/IPXA2025031647242.md): Skin · corroded · Mar 14, 2025 · N473UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin
  > RH PYLON INSIDE PANEL 443CR FWD LOWER CORNER HAS CORROSION. DOT 28-45 NOT ABLE TO REMOVE NOTED MEASUREMENTS. ALL MEASUREMENTS WERE ADDED TO CPCP AND SDR TASKS.
- [SDR IPXA2025040845454](https://openairdocs.org/sdr/IPXA2025040845454.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XBF HAS SEVERAL DENTS/PUCTURES (APPROX 45 EA), LOWER/UPPER SURFACE AND EDGE DAMAGED. DOT 103-35. FABRICATED MCD FLOOR PANEL 241XBF IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040745296](https://openairdocs.org/sdr/IPXA2025040745296.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL241XDF, LOWER SURFACE HAS DENTS/PUCTURES (APPROX 2 EA) AND EDGE DAMAGED. DOT 103-29. FABRICATED MCD FLOOR PANEL 241XDF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040745550](https://openairdocs.org/sdr/IPXA2025040745550.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT - Z200, COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL241XAF HAS UPPER SURFACE AND EDGE DAMAGED. DOT 103-38. FABRICATED MCD FLOOR PANEL 241XAF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040744836](https://openairdocs.org/sdr/IPXA2025040744836.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL242XJF HAS LOWER SURFACE AND EDGE DAMAGED. DOT 103-10. FABRICATED MCD FLOOR PANEL 242XJF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040745419](https://openairdocs.org/sdr/IPXA2025040745419.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT - Z200, COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL241XCF, LOWER SURFACE HAS SEVERAL DENTS/PUCTURES(APPROX 30 EA) AND EDGE DAMAGED. DOT 103-34. FABRICATED MCD FLOOR PANEL 241XCF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040744465](https://openairdocs.org/sdr/IPXA2025040744465.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT - Z200, COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL242XCF HAS SEVERAL DENTS AND PUCTURES (APPROX 23 EA). DOT 103-03. FABRICATED MCD FLOOR PANEL 242XCF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040744904](https://openairdocs.org/sdr/IPXA2025040744904.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > FAULT - Z200, COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL 242XEF HAS EDGE DAMAGED. DOT 103-15. FABRICATED MCD FLOOR PANEL 242XEF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040744974](https://openairdocs.org/sdr/IPXA2025040744974.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL 242XHF HAS EDGE DAMAGED. DOT 103-16. FABRICATED MCD FLOOR PANEL 242XHF, IAW UPS SREO: B757-9692-REQ 001 REVIEWED
- [SDR IPXA2025040444974](https://openairdocs.org/sdr/IPXA2025040444974.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL 242XHF HAS EDGE DAMAGED.
- [SDR IPXA2025040405454](https://openairdocs.org/sdr/IPXA2025040405454.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XBF HAS SEVERAL DENTS/PUCTURES (APPROX 45 EA), LOWER/UPPER SURFACE AND EDGE DAMAGED. REJECT- SREO AMT LABOR ROW NEEDS SIGNED OFF FINISH.
- [SDR IPXA2025040445296](https://openairdocs.org/sdr/IPXA2025040445296.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > **SDR FILED OPEN** FAULT - Z200, COMP, MCD, ABOVE CENTER BOX, FLOOR PANEL241XDF, LOWER SURFACE HAS DENTS/PUCTURES (APPROX 2 EA) AND EDGE DAMAGED. DOT 103-29 AUDIT COMPLETE
- [SDR IPXA2025040244732](https://openairdocs.org/sdr/IPXA2025040244732.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL242XFF HAS SEVERAL DENTS/PUCTURES. FABRICATED MCD FLOOR PANEL 242XFF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040345137](https://openairdocs.org/sdr/IPXA2025040345137.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XGF, LOWER SURFACE HAS DENTS/PUCTURES (APPROX 7 EA). FABRICATED MCD FLOOR PANEL 241XGF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040144998](https://openairdocs.org/sdr/IPXA2025040144998.md): Floor Panel · damaged · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL 242XGF HAS CORNER AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XGF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040344864](https://openairdocs.org/sdr/IPXA2025040344864.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL242XBF HAS SEVERAL DENTS/PUCTURES (APPROX 33 EA) FABRICATED MCD FLOOR PANEL 242XBF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040345010](https://openairdocs.org/sdr/IPXA2025040345010.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL242XDF HAS LOWER/UPPER SURFACE AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XDF,, IAW UPS SREO: B757-9692-REQ 001 U.
- [SDR IPXA2025040345190](https://openairdocs.org/sdr/IPXA2025040345190.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XJF HAS DENTS/PUCTURES AND EDGE DAMAGED. DOT 103-23. FABRICATED MCD FLOOR PANEL 241XJF, IAW UPS SREO: B757-9692-REQ 001. REVIEWED
- [SDR IPXA2025040245283](https://openairdocs.org/sdr/IPXA2025040245283.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XEF HAS SEVERAL DENTS/PUCTURES(APPROX 7 EA) AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 241XEF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025040345063](https://openairdocs.org/sdr/IPXA2025040345063.md): Floor Panel · punctured · Mar 14, 2025 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > MCD, ABOVE CENTER BOX, FLOOR PANEL241XHF LOWER SURFACE HAS SEVERAL DENTS/PUCTURES(APPROX 20 EA) AND EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 241XHF, IAW UPS SREO: B757-9692-REQ 001.
- [SDR IPXA2025041037198](https://openairdocs.org/sdr/IPXA2025041037198.md): Firewall · cracked · Mar 13, 2025 · N473UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/Firewall
  > NR 1 ENG LP COMPRESSOR INNER CASE AFT BULKHEAD FIREWALL WITH CRACK BTW 8-9 O'CLOCK. INSTALLED ENGINE#1 LH CENTER COMPRESSOR FAIRING OF LP COMPRESSOR INNER CASE. I.A.W AMM 72-03-01-424-006-R00. ACCOMPLISHED STEP 15 OF EO 535-7200-14571. INSTALLATION OF ENGINE
- [SDR IPXA2025041037319](https://openairdocs.org/sdr/IPXA2025041037319.md): Case · cracked · Mar 13, 2025 · N473UP · Boeing 75724APF · Turbine Engine Compressor Section
  > NR 1 ENG LP COMPRESSOR INNER CASE AFT AREA BTW 8-10 O'CLOCK WITH CRACKS AROUND HOLES (2 EA). REPAIR OF #1 ENG LP COMPRESSOR INNER CASE AFT AREA BTW 8-10 O'CLOCK ACCOMPLISHED ON JOB # T3F18E00694S2. I.A.W AMM 72-03-01-024-007-R00.
- [SDR IPXA2025040837319](https://openairdocs.org/sdr/IPXA2025040837319.md): Case · cracked · Mar 13, 2025 · N473UP · Boeing 75724APF · Turbine Engine Compressor Section
  > NR 1 ENG LP COMPRESSOR INNER CASE AFT AREA BTW 8-10 O'CLOCK WITH CRACKS AROUND HOLES (2 EA)-DOT 139/45-MR/139. REVIEWED
- [SDR IPXA2025032503443](https://openairdocs.org/sdr/IPXA2025032503443.md): Sill Drain · corroded · Mar 12, 2025 · N473UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FLOOR STRUCTURE, SUB-FLOOR PANEL AT MAIN CABIN COMPARTMENT RBL 50. UNDER FWD RH DRAIN HAS CORROSION AT NUTPLATE AREA. DOT 28-16. REPLACED NUTPLATE AT MAIN CABIN COMPARTMENT RBL 50 IAW SRM 51-40-02-0G-0. REVIEWED.
- [SDR IPXA2025031311399](https://openairdocs.org/sdr/IPXA2025031311399.md): Floorbeam · corroded · Mar 12, 2025 · N473UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FS 1180- FS1240 LBL 62 UPPER T-CHORD FALNGE IS EXFOLIATED AT FS1218-FS1224.REMOVED CORROSION FROM UPPER T-CHORD SURFACE, FS 1218-FS 1224 LBL 62, IAW 757-200PF SRM 51-10-02. EVALUATED REWORK.REMOVED CORRODED T-CHORD FROM FS1180-FS1240 LBL 62 IAW 757-200PF SRM 5
- [SDR IPXA2025031311380](https://openairdocs.org/sdr/IPXA2025031311380.md): Floorbeam · corroded · Mar 12, 2025 · N473UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FS 1220 LBL 65 TO LBL 70 UPPER PART OF T-CHORD FLANGE IS EXFOLIATED.REMOVED T-CHORD ON FS 1220 LBL 65 TO LBL 70 IAW B757-200, SRM 51-40-02, EVALUATED AND FOUND OUT OF LIMITS IAW B757-200, SRM 53-00-71-1A-1 DETAIL IX.INSTALLED NEW T-CHORD AT STA1220 LBL65-70 AN
- [SDR IPXA2025041087698](https://openairdocs.org/sdr/IPXA2025041087698.md): Skin · damaged · Mar 11, 2025 · N473UP · Boeing 75724APF · Leading Edge Devices
  > RIGHT WING SLAT NR 8 OUTER SURFACE T/E WEDGE HAS 5 DENTS. INSTALLED #8 SLAT IAW AMM 27-81-02-424-021. REVIEWED
- [SDR IPXA2025031180414](https://openairdocs.org/sdr/IPXA2025031180414.md): Skin · cracked · Mar 11, 2025 · N473UP · Boeing 75724APF · Wing, Plate/Skin
  > **SUPPLEMENTAL SDR** Z600 STR FAULT: RH WING FIXED LE SKIN UNDER SLAT #7 HAS A CRACK ON OB SIDE OF SKIN. INSTALLED RH WING FIXED LE SKIN REPAIR UNDER SLAT #7 IAW SREO-11855-REQ002 STEPS 1 THROUGH 31 WITHOUT DEVIATIONS. ACCCOMPLISH SREO-11855-REQ002 (APPX B)
- [SDR IPXA2025040180414](https://openairdocs.org/sdr/IPXA2025040180414.md): Skin · cracked · Mar 11, 2025 · N473UP · Boeing 75724APF · Wing, Plate/Skin
  > RH WING FIXED LE SKIN UNDER SLAT #7 HAS A CRACK ON OB SIDE OF SKIN VERIFIED STEPS 31 TO 33 OF SREO-11855-REQ002 (APPX B) ARE COMPLETED.<BR>RIGGING OF SLATS WILL BE ACCOMPLISHED ON TASK CARDS T3F18E0068H5E & T3F18E0068KDC.
- [SDR IPXA2025031265344](https://openairdocs.org/sdr/IPXA2025031265344.md): Floorbeam · eroded · Mar 10, 2025 · N473UP · Boeing 75724APF · Fuselage Main, Floor Beam
  > FS 900 BL 0 TO RBL 72 HAS CHAFING ON T-CHORD AND PAINT ERODED AWAY. INSTALLED 1EA OUTER CHORD & 8EA SPLICE IAW SRM B757-200 TASK: 51-40-02. REVIEWED
- [SDR IPXA2025041065680](https://openairdocs.org/sdr/IPXA2025041065680.md): Strap · corroded · Mar 10, 2025 · N473UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > UPPER APU INTAKE DOOR SURROUND STRAP P/N 148N3138-20 AT FS 1787 HAS CORROSION WITH CORRODED NUTPLATES. INSTALLED FWD STRAP P/N 148N3138-20 PER B757 SRM 51-40-02 P/N BACR15CE8KE7 BACH # 4256147 (35 EA) RIVETS
- [SDR IPXA2025041065760](https://openairdocs.org/sdr/IPXA2025041065760.md): Strap · damaged · Mar 10, 2025 · N473UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > FS 1825 UPPER FUSELAGE APU DOOR SURROUND STRAP P/N 148N3138-8000 HAS CORROSION AND CORRODED NUTPLATES. INSTALLED (3EA) STRAPS AND (1EA) FILLER PER B757 SRM 53-80-15-2R-1 HL P/N BACB30NW8K8X BACH #4374992 COLLAR P/N HL70-8 (235 EA) HL.
- [SDR IPXA2025031265885](https://openairdocs.org/sdr/IPXA2025031265885.md): Support Angle · corroded · Mar 10, 2025 · N473UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE FS 1820-FS1795 DOOR SURROUND LOWER STRAP AT STR 6R P/N 148N3152-1 HAS CORROSION. INSTALLED ANGLE STR6 PER SRM 51-40-02 RIVET P/N BACR15FT6D7C BACH #4364973 (30 EA)RIVETS.
- [SDR IPXA2025031265833](https://openairdocs.org/sdr/IPXA2025031265833.md): Support Angle · corroded · Mar 10, 2025 · N473UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE APU DOOR SURROUND FS1795 - FS1820 P/N 148N3152-2 AT STR 3R IS CORRODED. INSTALLED ANGLE STR3 PER SRM 51-40-02 RIVET P/N BACR15FT6D7C BACH #4364973 (30 EA) RIVETS.
- [SDR IPXA2024092765141](https://openairdocs.org/sdr/IPXA2024092765141.md): Indicator · malfunctioned · Sep 24, 2024 · N473UP · Boeing 75724APF · Door Warning System
  > ENTRY DOOR LIGHT DID NOT GO OUT UPON CLOSING DOOR AT DEPARTURE R&R L1 DOOR PROX SENSOR PER MM 52-71-00-000-802. ADJ PER MM 52-71-00-825-223. TESTS GOOD. CLEARS DEFERRAL
- [SDR IPXA2024092465141](https://openairdocs.org/sdr/IPXA2024092465141.md): Indication Sys · faulted · Sep 24, 2024 · N473UP · Boeing 75724APF · Door Warning System
  > ENTRY DOOR LIGHT DID NOT GO OUT UPON CLOSING DOOR AT DEPARTURE PLACARDED CREW ENTRY DOOR INDICATION IAW MEL 52-71-1. DMP COMPLIED WITH. PLACARD INSTALLED OPEN
- [SDR IPXA2024012929679](https://openairdocs.org/sdr/IPXA2024012929679.md): Bumper · missing · Jan 25, 2024 · N473UP · Boeing 75724APF · Passenger/Crew Doors
  > *** SUPPLEMENTAL SDR *** CREW DOOR DAMPER BUMPER MISSING REPLACED MISSING BUMPER
- [SDR IPXA2024012529679](https://openairdocs.org/sdr/IPXA2024012529679.md): Bumper · missing · Jan 25, 2024 · N473UP · Boeing 75724APF · Passenger/Crew Doors
  > **SDR FILED OPEN**CREW DOOR DAMPER BUMPER MISSING REPLACED MISSING BUMPER
- [SDR IPXA2023031191744](https://openairdocs.org/sdr/IPXA2023031191744.md): Frame · dented · Feb 28, 2023 · N473UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:CK1CAFT CARGO PIT FRAME STA 1500 BETWEEN STR 25R AND 26R HAS A DENT.FRAME WAS REPAIRED PER RCD 272034 / SRM 53-00-07-2R-5 DETAIL III
- [SDR IPXA2023031091731](https://openairdocs.org/sdr/IPXA2023031091731.md): Frame · dented · Feb 28, 2023 · N473UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:C13*MAJOR REPAIR* FWD CARGO PIT FRAME 680 RH BETWEEN STR 23 TO STR 27 HAS AN EXISTING REPAIR WITH DENTREPAIRED PER UPS RCD 267664 - SRM 53-00-07-2R-5 DETAIL I.
- [SDR IPXA2023031191748](https://openairdocs.org/sdr/IPXA2023031191748.md): Frame · dented · Feb 28, 2023 · N473UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEG1*MAJOR REPAIR* AFT CARGO PIT - FRAME AT STA 1220 BETWEEN STR 26 AND 27 RH SIDE HAS A DENTFRAME WAS REPAIRED IAW RCD 272032 / SRM 53-00-07-2R-6 DETAIL I
- [SDR IPXA2022053082667](https://openairdocs.org/sdr/IPXA2022053082667.md): Eicas · fault message · May 28, 2022 · N473UP · Boeing 75724APF · Cabin Pressure Control System
  > INSPECTION TYPE:NA***DIVERSION*** CABIN ALT WARNINGT/S IAW FIM 21-30-00-815-802, FOUND AC MOTOR #2 AT FAULT. M.M 7392277. R/R AC MOROT #2 IAW AMM 21-31-05 PB401 NO HELP.NN 7392277; REMOVED AND REPLACED OUTFLOW VLV ASSY IAW AMM 21-31-03. ACCOMPLISHED OPS CHECK
- [SDR IPXA2022012578266](https://openairdocs.org/sdr/IPXA2022012578266.md): Tat Probe · none · Jan 25, 2022 · N473UP · Boeing 75724APF · Pitot/Static Anti-Ice System
  > INSPECTION TYPE:N/A**ATB SDR FILED**NO EMERG**REQ'D RADAR VECTORS**A/C LANDED WITHOUT INCIDENT** AFTER ROTATION ON T.O RECIEVED TAT PROBE EICAS. A FEW MINUTES LATER RECIEVED L AND R ENG EEC EICAS. ACCOMPLISHED APPROPRIATE QRH CHECHLIST AIR TURNBACKFOLLOWED FIM
- [SDR IPXA2021110575635](https://openairdocs.org/sdr/IPXA2021110575635.md): Floor Panel · damaged · Nov 5, 2021 · N473UP · Boeing 75724APF · Cargo Compartments
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT, FLOOR PANEL 241XKF IS DAMAGED.FABBED PANEL 241XKF FROM 5024N400001SS-G, BATCH# 3855547 PER SREO B757-5320-9662-K
- [SDR IPXA2021110575633](https://openairdocs.org/sdr/IPXA2021110575633.md): Floor Panel · damaged · Nov 5, 2021 · N473UP · Boeing 75724APF · Cargo Compartments
  > INSPECTION TYPE:SEG4MAIN CARGO COMPARTMENT, FLOOR PANEL 241XFF IS DAMAGED.FABBED PANEL 241FF FROM 5024N400001SS-G, BATCH#3855547 PER SREO B757-5320-9692-K.
- [SDR IPXA2021021065528](https://openairdocs.org/sdr/IPXA2021021065528.md): Inertia Reel · broken · Feb 9, 2021 · N473UP · Boeing 75724APF · Emergency Equipment
  > INSPECTION TYPE:N/AIN TURBULENCE COVER FELL OFF INERITAL REEL AND HANDLES FELL OUT TO THE FLOORREMOVED AND REPLACED 2EA DESCENT DEVICES IAW AMM 25 61 02 252 005 IPC 25 61 01 01 ITEM 70
- [SDR IPXA2020060155925](https://openairdocs.org/sdr/IPXA2020060155925.md): Transmission · malfunctioned · May 29, 2020 · N473UP · Boeing 75724APF · Trailing Edge Flap Actuator
  > EMERGENCY DECLARED LANDED W/O INCIDENT. DURING APPROACH, WHEN FLAPS 1 SELECTED, TE FLAP DISAGREE EICAS MSG RECEIVED. USED ALT FLAPS PER CHECKLIST. LT INBD FLAP INBD FLAP TRANSMISSION PREVIOUSLY INDICATED AN OVERLOAD. IAW FIM 27-51-00-815, FOUND LT INBD TE
- [SDR IPXA2019101657945](https://openairdocs.org/sdr/IPXA2019101657945.md): Floor Panel · damaged · Oct 15, 2019 · N473UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1MAIN CARGO COMPARTMENT, FLOOR PANEL 221XCF DAMAGEDFABBED PANEL 221XCF FROM 5024N00001SS-G, BATCH# 3546253 PER SREO B757-5320-9692-K
- [SDR IPXA2019101647905](https://openairdocs.org/sdr/IPXA2019101647905.md): Floor Panel · damaged · Oct 14, 2019 · N473UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:C1, MAIN CABIN FLOOR BOARD #231XCF IS SATURATED WITH SKYDROL FLUID.FABBED 231XCF FROM 5024N40000155-G, BATCH# 3546253 PER SREO B757-5320-9692-K

Next page: https://openairdocs.org/aircraft/N473UP/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 = 'N473UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N473UP/reports

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