# Service difficulty reports: N425UP

A list on [N425UP](https://openairdocs.org/aircraft/N425UP.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 · 222 reports

- [SDR IPXA2025103131577](https://openairdocs.org/sdr/IPXA2025103131577.md): Handle · stuck · Oct 30, 2025 · N425UP · Boeing 75724APF · Landing Gear Selector
  > ***SUPPLEMENTAL SDR*** LANDING GEAR HANDLE STUCK DOWN.. LOCK OVRD INOP IN AIR. RESULTED IN ATB. AFTER PRESSURIZING LEFT SYSTEM HYDRAULICS, FOUND LEFT MAIN LANDING GEAR TRUCK DID NOT TILT. FOUND S452 LEFT MLG TILT SHUTTLE VALVE PRESSURE SWITCH WITH POSITIVE P
- [SDR IPXA2025103031577](https://openairdocs.org/sdr/IPXA2025103031577.md): Landing Gear · malfunctioned · Oct 30, 2025 · N425UP · Boeing 75724APF · Landing Gear Retraction/Extension System
  > AIR TURN BACK, LANDING GEAR HANDLE STUCK DOWN. LOCK OVER RIDE INOPERATIVE IN AIR. PERFORMED PSEU BITE CHECK IAW FIM 32-09 FAULT TREE 802. BITE CHECK GOOD.
- [SDR IPXA2025101554034](https://openairdocs.org/sdr/IPXA2025101554034.md): Crease Beam · corroded · Oct 2, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > CORROSION FOUND ON CREASE BEAM ON MAIN CABIN FLOOR BETWEEN STA 1600-1580 LBL AT STR 17. REMOVED 1EA SIDEWALL LINING P/N:146N5509-7 FROM MAIN CABIN BETWEEN BS 1580 TO 1660 LBL-STGR 17 FOR ACCESS IAW 51-40-02-0G-0. ASSEMBLED AND INTALLED REPAIR PARTS IAW E.A.
- [SDR IPXA2025101558814](https://openairdocs.org/sdr/IPXA2025101558814.md): Skin · damaged · Oct 2, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, SKIN DOUBLER BS 700 - 720, STRINGERS 1R & 2R IS BENT AND DEFORMED,. ACCOMPLISHED REPAIR PER EO-95379-REQ1 AND VT-SAA EA 757-5330-01-B0577, REV. IR.
- [SDR IPXA2025101354034](https://openairdocs.org/sdr/IPXA2025101354034.md): Crease Beam · corroded · Oct 2, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > CORROSION FOUND ON CREASE BEAM ON MAIN CABIN FLOOR BETWEEN STA 1600-1580 LBL AT STR 17. ATA 53-00 VERIFIED STEP 31, RESTORE ACCESS AT REPAIRED AREA PER EA 757-5300-01-B0575 STEP 13 WILL BE ACCOMPLISHED IN TASK CARD T3F18E0073RLF.
- [SDR IPXA2025100722583](https://openairdocs.org/sdr/IPXA2025100722583.md): Strap · corroded · Sep 24, 2025 · N425UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors
  > APU DOOR SUPPORT STRUCTURE AFT STRAP SHOWS SIGNS OF CORROSION. REMOVED OUTER STRAP, REPAIR DOUBLER (-1), FILLER (-3), STRAP (-2) AND FILLER (-4) FROM APU DOOR SUPPORT STRUCTURE IAW SRM 51-40-02-0G-0. INSTALLED -1 DOUBLER, -2 STRAP, -3 FILLER AND -4 FILLER AN
- [SDR IPXA2025102197638](https://openairdocs.org/sdr/IPXA2025102197638.md): Cam · damaged · Sep 23, 2025 · N425UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR FWD FRAME UPPER & LOWER LATCH CAM HAS GOUGED. REMOVED LATCH, CREW ENTRY DOOR UPPER CAM IN REFERENCE TO B757 CMM 52-11-08 AND SRM 51-40-02-0G-0. INSTALLED LATCH, CREW ENTRY DOOR UPPER CAM IAW CMM 52-11-08 AND SRM 51-40-02-0G-0. INSTALLED LATC
- [SDR IPXA2025101592752](https://openairdocs.org/sdr/IPXA2025101592752.md): Frame · corroded · Sep 23, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > RIGHT FWD FUSELAGE WASTE PANEL ACCESS HAS CORROSION INSIDE FRAME, FLL-011, ACCOMPLISHED REPAIR PER EO-95404-REQ1 AND VT-SAA EA 757-5249-01-B0574, REV. IR.
- [SDR IPXA2025092497638](https://openairdocs.org/sdr/IPXA2025092497638.md): Cam · gouged · Sep 23, 2025 · N425UP · Boeing 75724APF · Passenger/Crew Doors
  > CREW ENTRY DOOR FWD FRAME UPPER & LOWER LATCH CAM HAS GOUGED.
- [SDR IPXA2025100676445](https://openairdocs.org/sdr/IPXA2025100676445.md): Strap · corroded · Sep 22, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > APU INLET DOOR SUPPORT STRUCTURE FWD STRAP SHOWS SIGNS OF CORROSION. REMOVED FWD STRAP PN: 148N3138-20 AND UPPER MIDDLE ANGLE PN:148N3152-2 AT APU INLET DOOR STRUCTURE IAW SRM 51-40-02-0G-0. REMOVED LOWER MIDDLE ANGLE AND FWD LOWER ANGLE AT APU INLET DOOR STRU
- [SDR IPXA2025072313969](https://openairdocs.org/sdr/IPXA2025072313969.md): Stringer · dented · Jul 19, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR, STRINGER 25L DENTED AT STA 1340. DISPLACED FRAME AT STATION 1340, STRINGER 25L FOR FOM. EO-94445-REQ1
- [SDR IPXA2025072360023](https://openairdocs.org/sdr/IPXA2025072360023.md): Skin · damaged · Feb 9, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR. IMPACT DAMAGE TO FUSELAGE SKIN BS 1340, S25. REPAIRED IAW EO-91018-REQ3.
- [SDR IPXA2025020960023](https://openairdocs.org/sdr/IPXA2025020960023.md): Skin · ground damage · Feb 9, 2025 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > MAJOR REPAIR, IMPACT DAMAGE TO FUSE. SKIN STA. 1340 STR. 25L (REFERENCE SRM 53-60-01-0I-1, FIGURE 1, DETAIL II, ITEM 2). THE DAMAGE CONSISTS OF A DENT TO THE FUSELAGE SKIN PANEL. THE DENT MEASURES APPROXIMATELY 10.5IN CIRCUMFERENTIALLY BY 2.0IN FWD/AFT WITH A
- [SDR IPXA2024073196756](https://openairdocs.org/sdr/IPXA2024073196756.md): Skin · damaged · Jul 30, 2024 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > IMPACT DAMAGE BY CONTAINER ON FUSELAGE SKIN STA. 1340 STRINGER 25L REMOVED 4 RIVETS AT S25L AND REMOVED 6 RIVETS AT STA 1340 BETWEEN S25L AND S26L.REMOVED 4 RIVETS AT S25L AND REMOVED 6 RIVETS AT STA 1340 BETWEEN S25L AND S26L.PERFORMED MATERIAL REMAINING DAMA
- [SDR IPXA2023110228293](https://openairdocs.org/sdr/IPXA2023110228293.md): Frame · none · Oct 17, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Frame
  > FAULT: STA 740 FRAME WEB AT STR 25R AND STR 26R, I/B AND O/B WAS TRIMMED OUT WHILE ACCOMPLISHING SRM STRINGER REPAIR. INSTALLED J-SECTION I.A.W SRM 51-40-02-0G EA#757-5330-27-A3403 STEPS 18 TROUGH 26 PRELIM 3.- JOB WAS ACCOMPLISHED IAW UPS EO-88508-REQ1 AND VT
- [SDR IPXA2023102690583](https://openairdocs.org/sdr/IPXA2023102690583.md): Bulkhead · gouged · Sep 27, 2023 · N425UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/Firewall
  > MAJOR REPAIR, #2 ENG PYLON AFT I/B LWR CORNER REINFORCEMENT PANEL HAS A CRACK. VERIFIED ACCOMPLISHMENT PER UPS EO-88456-REQ 1 AND VTMAE EA 757-5453-27-A3388 REV-,WITHOUT ANY DEVIATION.
- [SDR IPXA2023102664541](https://openairdocs.org/sdr/IPXA2023102664541.md): Bulkhead · gouged · Sep 25, 2023 · N425UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/Firewall
  > MAJOR REPAIR, LOWER O/B EDGE OF AFT BULKHEAD ON #1 PYLON IS GOUGED DOT 06951-101. JOB WAS ACCOMPLISHED PER UPS EO-88455-REQ1 AND VT MAE EA # 757-5453-27-A3387 REV -, WITHOUT ANY DEVIATION.
- [SDR IPXA2023103121037](https://openairdocs.org/sdr/IPXA2023103121037.md): Tee Angle · corroded · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > FAULT: T-CHORD NEAR BODY STA. 1040, LH SIDE. HAS NUMEROUS RUSTED NUT PLATES. REVIEWED.
- [SDR IPXA2023103119871](https://openairdocs.org/sdr/IPXA2023103119871.md): Unknown · corroded · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > WING TO BODY T-CHORD, AT FR, 900 BETWEEN LBL 63 TO RBL 64 HAS CORROSION. DOT. 65-044. INSTALLED T-CHORD STA 900 R/H I.A.W SRM 51-40-02-0G.- REVIEWED.
- [SDR IPXA2023103133051](https://openairdocs.org/sdr/IPXA2023103133051.md): Stringer · corroded · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR, AFT CARGO PIT - STRINGER 26 LH BETWEEN STA 1570 AND 1620 IS CORRODED. REPAIRED IAW --1) REMOVE S-26L DAMAGED STRINGER SECTION (P/N: 146N3110-479) BETWEEN STA 1500-1520 (FAULT T3F18E002EKMP) AND STA 1560-1620 (FAULT T3F18E002EKMQ) RESPECTIVELY. 2)
- [SDR IPXA2023103120357](https://openairdocs.org/sdr/IPXA2023103120357.md): Unknown · corroded · Sep 21, 2023 · N425UP · Boeing 75724APF · Aerodynamic Fairings
  > WING TO BODY T-CHORD AT FR. 1037.67 BETWEEN LBL 63 TO RBL. 63, HAS CORROSION DOT. 65-046. INSTALLED NEW T-CHORD IAW B757 SRM 51-40-02-0G. REVIEWED.
- [SDR IPXA2023100633051](https://openairdocs.org/sdr/IPXA2023100633051.md): Unknown · unknown · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > *** SDR FILED OPEN *** FAULT: AFT CARGO PIT - STRINGER 26 LH BETWEEN STA 1570 AND 1620 IS CORRODED. OK TO INSTALL SPLICE, SPLICE FRAME, WEB, TIE DOWN BRACKET, STRINGER CLIP 5EA, SHEAR TIE (4EA), SHEAR TIE (2EA).
- [SDR IPXA2023100620357](https://openairdocs.org/sdr/IPXA2023100620357.md): Unknown · unknown · Sep 21, 2023 · N425UP · Boeing 75724APF · Aerodynamic Fairings
  > *** SDR FILED OPEN *** FAULT: WING TO BODY T-CHORD AT FR. 1037.67 BETWEEN LBL 63 TO RBL. 63, HAS CORROSION DOT. 65-046 INSTALLED NEW T-CHORD IAW B757 SRM 51-40-02-0G
- [SDR IPXA2023100619871](https://openairdocs.org/sdr/IPXA2023100619871.md): Unknown · unknown · Sep 21, 2023 · N425UP · Boeing 75724APF · Aerodynamic Fairings
  > *** SDR FILED OPEN *** FAULT: WING TO BODY T-CHORD, AT FR, 900 BETWEEN LBL 63 TO RBL 64 HAS CORROSION. DOT. 65-044 VERIFIED MATERIAL RECEIVED ON TRAVELER. T23/1707760.
- [SDR IPXA2023100621037](https://openairdocs.org/sdr/IPXA2023100621037.md): Unknown · unknown · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Structure (General)
  > *** SDR FILED OPEN ***FAULT: T-CHORD NEAR BODY STA. 1040, LH SIDE. HAS NUMEROUS RUSTED NUT PLATES. INSTALLED NEW T-CHORD AT STA 1040 LH SIDE I.A.W SRM 51-40-02-0G
- [SDR IPXA2023100633060](https://openairdocs.org/sdr/IPXA2023100633060.md): Stringer · corroded · Sep 21, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > *** MAJOR REPAIR *** FAULT: AFT CARGO PIT - STRINGER 26 LH AT STA 1510 IS CORRODED. JOB COMPLETE
- [SDR IPXA2023103112537](https://openairdocs.org/sdr/IPXA2023103112537.md): Skin · corroded · Sep 20, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > *SUPPLEMENTAL SDR* FAULT: EXTERNAL SKIN BULGING AT STA.1600 AND BETWEEN STR.29L AND STR.30L. INSTALLED NEW INTERCOSTAL AT STA.1600 BETWEEN STRG.29L AND 30L I.A.W. 51-40-02-0G. REVIEWED.
- [SDR IPXA2023100712537](https://openairdocs.org/sdr/IPXA2023100712537.md): Unknown · unknown · Sep 20, 2023 · N425UP · Boeing 75724APF · Fuselage Structure (General)
  > FAULT: EXTERNAL SKIN BULGING AT STA.1600 AND BETWEEN STR.29L AND STR.30L INSTALLED NEW INTERCOSTAL AT STA.1600 BETWEEN STRG.29L AND 30L I.A.W. 51-40-02-0G. JOB COMPLETE
- [SDR IPXA2023102494081](https://openairdocs.org/sdr/IPXA2023102494081.md): Skin · dented · Sep 18, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Plate/Skin
  > *SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT-A GOUGE AT STA730, BTWN STR26R-STR25R; DOT 117-011. JOB WAS ACCOMPLISHED IAW UPS EO 88312-REQ1 AND VT MAE EA 757-5330-27-A3385 REV- WITHOUT ANY DEVIATION. REVIEWED
- [SDR IPXA2023102391597](https://openairdocs.org/sdr/IPXA2023102391597.md): Frame · dented · Sep 18, 2023 · N425UP · Boeing 75724APF · Fuselage Main, Frame
  > *** MAJOR REPAIR *** FAULT: AFT CARGO PIT, FRAME STA 1600 LH SIDE HAS A DENT ON UPPER FLANGE BETWEEN STR 25L AND STR 26L VERIFIED INSTALLATION OF NEW STRAP. VERIFIED JOB WAS ACCOMPLISHED PER UPS EO-88259-REQ1 AND VTMAE EA 757-5360-27-A3379 REV-. REVIEWED
- [SDR IPXA2023101791584](https://openairdocs.org/sdr/IPXA2023101791584.md): Shear Tie · dented · Sep 18, 2023 · N425UP · Boeing 75724APF · Fuselage Internal Mounting Structure
  > MAJOR REPAIR, AFT CARGO PIT, FRAME STA 1300 RH SIDE HAS A DENT ON UPPER FLANGE AT STR 26R. JOB WAS ACCOMPLISHED IAW UPS EO 88264-REQ1 AND VTMAE EA 757-5360-27-A3384 REV-, WITHOUT ANY DEVIATION.
- [SDR IPXA2023101291585](https://openairdocs.org/sdr/IPXA2023101291585.md): Unknown · unknown · Sep 18, 2023 · N425UP · Boeing 75724APF · Fuselage Structure (General)
  > *MAJOR REPAIR* FAULT: AFT CARGO PIT, FRAME STA 1240 RH SIDE HAS A DENT ON UPPER FLANGE BETWEEN STR 25R AND STR 26R VERIFIED JOB ACCOMPLISHED PER UPS EO/88263-REQ1 AND VTMAE EA 757-5360-27-A3383 REV-. JOB COMPLETE
- [SDR IPXA2023081633505](https://openairdocs.org/sdr/IPXA2023081633505.md): Flap System · inoperative · Aug 9, 2023 · N425UP · Boeing 75724APF · Trailing Edge Flap Control System
  > *SUPPLEMENTAL SDR* *ATB* FLAP DISAGREE R+R FLAP INDICATOR IAW/AMM 27-58-02 OPS CKD GOOD, DMI 2503945 CLEARED PLACARD REMOVED
- [SDR IPXA2023080933505](https://openairdocs.org/sdr/IPXA2023080933505.md): Unknown · unknown · Aug 9, 2023 · N425UP · Boeing 75724APF · Flight Control System
  > *SDR FILED OPEN* *ATB* FLAP DISAGREE DEFERRED FLAP POSITION INDICATOR SYSTEM POSITION NEEDLES IAW MEL 27-08-2-1. PLACARD INSTALLED
- [SDR IPXA2021112376297](https://openairdocs.org/sdr/IPXA2021112376297.md): Warning Message · false activation · Nov 23, 2021 · N425UP · Boeing 75724APF · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A**EMERGENCY DECLARED**A/C LANDED W/OUT INCIDENT** NO HAZMAT**TE FLAP ASYM EICAS MESSAGE DISPLAYED FL 330 FLAP POS INDICATOR INDICATES FLAPS UP.REMOVED & REPLACED # 1 FSEU ALL OPS NORMAL IAW AMM 27-51-01.
- [SDR IPXA2021112376287](https://openairdocs.org/sdr/IPXA2021112376287.md): Connector · loose · Nov 22, 2021 · N425UP · Boeing 75724APF · Trailing Edge Flap Control System
  > EMERGENCY DECLARED, LANDED W/OUT INCIDENT, NO HAZMAT. TRAILING EDGE TE FLAP ASSY EICAS MESSAGE DISPLAYED FL 400 POS IND. DISPLAYED UP POSITION.PERFORMED FSEU BITE PROCEDURE PER FIM 27-51-00-815-805 FOUND MSG 221 CHECKED RT FLAP POS. XMITR FOUND LOOSE CANNON
- [SDR IPXA2021092174139](https://openairdocs.org/sdr/IPXA2021092174139.md): Shear Tie · corroded · Sep 20, 2021 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEGBS STA 879 BETWEEN STRINGERS 28L AND 28R THE 140N2002-1150 SHEAR TIE JUST AFT OF STA 879 IS EXFOLIATED BEYOND REPAIRREMOVED CORRODED SHEAR TIE AND INSTALLED REPLACEMENT PER SRM 51-40-02 AND 51-10-02 PR 9.
- [SDR IPXA2021092374179](https://openairdocs.org/sdr/IPXA2021092374179.md): Skin · corroded · Sep 17, 2021 · N425UP · Boeing 75724APF · Trailing Edge Flaps
  > INSPECTION TYPE:SEGRH WING IB FLAP TE TRACK SUPPORT IS HEAVILY CORRODED AROUND FASTENER HOLES.REMOVED AND INSTALLED REPLACEMENT 113N2322-24 PER DWG 113N2322 AND SRM 51-40-02
- [SDR IPXA2021092174138](https://openairdocs.org/sdr/IPXA2021092174138.md): Bracket · cracked · Sep 15, 2021 · N425UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG#1 ENGINE AFT FAIRING FRAME STA 272 RH SIDE BRACKET IS CRACKED.REMOVED CRACKED BRACKET AND INSTALLED REPLACEMENT PER SRM 51-40-02 AND 51-10-02 PR 9.
- [SDR IPXA2021093074430](https://openairdocs.org/sdr/IPXA2021093074430.md): Support · cracked · Sep 14, 2021 · N425UP · Boeing 75724APF · Nacelle/Pylon Structure
  > INSPECTION TYPE:SEG#2 PYLON OB SIDE AFT FAIRING FWD SUPPORT AFTER REMOVING CORROSION FOUND A.422" CRACK AT BOTTOM HOLE OF SUPPORTREPAIRED SUPPORT PER EO# B757-5450-27-A2700
- [SDR IPXA2021092174137](https://openairdocs.org/sdr/IPXA2021092174137.md): Shear Tie · corroded · Sep 14, 2021 · N425UP · Boeing 75724APF · Fuselage Main, Structure
  > INSPECTION TYPE:SEGBS STA 879 LOWER LOBE BETWEEN STR 28L AND 28R BOTTOM IML OF SKIN SHEAR TIE IS EXFOLIATED OUT OF LIMITSREMOVED CORRODED SHEAR TIE AND INSTALLED REPLACEMENT PER SRM 51-40-02 AND 51-10-02 PR 9.
- [SDR IPXA2021041368144](https://openairdocs.org/sdr/IPXA2021041368144.md): Elt · no test · Apr 11, 2021 · N425UP · Boeing 75724APF · Emergency Locator Beacon
  > INSPECTION TYPE:NAELT TRANSMITTER FAILS TEST.R & R'D ELT PER MM 25-60-00. TEST OK.
- [SDR IPXA2019103088411](https://openairdocs.org/sdr/IPXA2019103088411.md): Floor Support · corroded · Oct 28, 2019 · N425UP · Boeing 75724APF · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C1FLOOR SUPPORT CHANNEL IN AFT CARGO PIT HAS CORROSION & DELAMINATION RH SIDE STA 1540FABRICATED REPAIR PARTS PER SRM 51-70-13-OG AND UPS SREO B757-5320-3220-N
- [SDR IPXA2019102878351](https://openairdocs.org/sdr/IPXA2019102878351.md): Skin · punctured · Oct 27, 2019 · N425UP · Boeing 75724APF · Trailing Edge Flaps
  > INSPECTION TYPE:M4L/H WING OB AFT FLAP HAS A PUNCTURED HOLE IN FLAP DOT 33-11REPAIRED PUNCTURED FLAP IAW B757 SRM 57-53-01-2R-1 (TABLE 2) AND 51-70-04 350F CURE
- [SDR IPXA2019102548246](https://openairdocs.org/sdr/IPXA2019102548246.md): Skin · delaminated · Oct 24, 2019 · N425UP · Boeing 75724APF · Leading Edge Devices
  > INSPECTION TYPE:SEG4#5 SLAT UPPER WEDGE HAS NINE DENTS DOT 8-003 AND MARKED IN RED.FURTHER INSPECTION IDENTIFIED 13 DELAMINATIONS, REPAIRED DELAMINATIONS IAW B757 SRM 57-43-02-2R1 AND SRM 51-70-10 250F CURE PER UPS / RECD 129831.
- [SDR IPXA2019101877999](https://openairdocs.org/sdr/IPXA2019101877999.md): Floor Panel · damaged · Oct 17, 2019 · N425UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG4FLOOR PANEL 242XEF HAS EDGE DAMAGEFABRICATED NEW FLOOR PANEL 242XEF IAW B757-5320-9692-K
- [SDR IPXA2019101877998](https://openairdocs.org/sdr/IPXA2019101877998.md): Floor Panel · damaged · Oct 17, 2019 · N425UP · Boeing 75724APF · Fuselage Floor Panel
  > INSPECTION TYPE:SEG4FLOOR PANEL 241XFF REQUIRES FABRICATIONFABRICATED NEW PANEL 241XFF IAW SREO 757-5320-9692-K
- [SDR IPXA2019032740525](https://openairdocs.org/sdr/IPXA2019032740525.md): Warning System · false activation · Mar 23, 2019 · N425UP · Boeing 75724APF · Trailing Flap Position Indicating System
  > INSPECTION TYPE:N/A ON APPROACH FROM FLAPS 20 TO FLAPS 25 FLAP "TE FLAP DISAGREE" EICAS MSG & TRAILING EDGE LIGHT FLAPS STUCKED BETWEEN 20(DEG)-25(DEG) ACCOMPLISHED NON NORMAL CHECKLIST LANDED FLAPS 20 VREF. EMERGENCY DECLARED. ACCOMPLISHED FIM 27-51-00-815-80
- [SDR IPXA2018100534713](https://openairdocs.org/sdr/IPXA2018100534713.md): Stringer · corroded · Oct 5, 2018 · N425UP · Boeing 75724APF · Fuselage Main, Longeron/Stringer
  > FASTENERS PULLED THROUGH SKIN STA 1450-1460 STRINGER 29L. REPAIR IAW EO B757-5310-70134-A.
- [SDR IPXA2018040528220](https://openairdocs.org/sdr/IPXA2018040528220.md): Oil System · overserviced · Apr 4, 2018 · N425UP · Boeing 75724APF · Turbine Engine Oil System
  > FAINT OIL BURNING OR PNUMATIC BURNING ODOR EMERGED ENROUTE, CONDITION BECAME WORSE DURING DESCENT. NO SMOKE PRESENT IN COCKPIT. PERFORMED AIR CONDITIONING CONTAMINATION TASK SUGGEST ODOR POS ORIGINATING FROM OVER FILLED ENGINE OIL SYSTEM 23QTS IAW FIM 21-00

Next page: https://openairdocs.org/aircraft/N425UP/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 = 'N425UP' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N425UP/reports

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