# Service difficulty reports: N443UP A list on [N443UP](https://openairdocs.org/aircraft/N443UP.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 6 · 292 reports - [SDR IPXA2026022722165](https://openairdocs.org/sdr/IPXA2026022722165.md): Fuel Sys · out of balance · Feb 26, 2026 · N443UP · Boeing 75724APF · Aircraft Fuel Distribution System > *** DIVERSION *** RECEIVED FUEL CONFIG LIGHT & MESSAGE ON FINAL APPROACH WITH THE FUEL IMBALANCE OF 1800LBS. NOTICED FUEL TO BEGIN SLOW IMBALANCE FROM CRUISE THRU TOUCHDOWN. TOTAL FUEL USED AND TOTALIZER CORRECT. C/W FIM 28-21 TASK 801 AND EVERYTHING OPS CHEC - [SDR IPXA2026012925317](https://openairdocs.org/sdr/IPXA2026012925317.md): Window · cracked · Jan 29, 2026 · N443UP · Boeing 75724APF · Flight Compartment Windows > LT FWD WINDOW CRACKED. REMOVED AND REPLACED L1 WINDOW IAW B757 AMM 56-11-01 OPS AND LK CHECKS GOOD AT THIS TIME. PERFORMED RII OF L1 WINDSHIELD ELECTRICAL CONNECTION INSTALL AND TORQUE PER GMM 04-02. - [SDR IPXA2026012925306](https://openairdocs.org/sdr/IPXA2026012925306.md): Element · burned · Jan 29, 2026 · N443UP · Boeing 75724APF · Flight Compartment Windows > LEFT FWD WINDOW LOWER ELEMENT BURN OUT DURING FLIGHT. REPLACEED THE L1 WINDSHIELD. ALSO REPLACED M191 HEAT CONTROL UNIT PRECAUTIONARY PER AMM 30-41-01-004-001. OPS CHECK GOOD. REF BARCODE T3F18E0086B65 FOR RII SIGNOFF OF L1 WINDSHIELD REPLACEMENT. - [SDR IPXA2025041482306](https://openairdocs.org/sdr/IPXA2025041482306.md): Angle · corroded · Apr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors > FAULT: STR Z-300 APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 HAS CORROSION ( T3F18E006CECF) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA SUPPORT ANGLE + 1 PLATE IAW B757-200-SRM-51-40-02-OG. REVIEWED - [SDR IPXA2025041482337](https://openairdocs.org/sdr/IPXA2025041482337.md): Angle · corroded · Apr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors > FAULT: STR Z-300 APU INLET DOOR FWD UPPER CORNER ANGLE STA 1787.45 HAS CORROSION (T3F18E006CEBJ) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA CORNER ANGLE B757-200-SRM-51-40-02-OG. REVIEWED - [SDR IPXA2025041482229](https://openairdocs.org/sdr/IPXA2025041482229.md): Angle · corroded · Apr 12, 2025 · N443UP · Boeing 75724APF · Auxiliary Power Unit (APU) Doors > APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 (T3F18E006CEAL) TO REPLACE SUPPORT ANGLE. INSTALLED 1 EA UPPER ANGLE IAW B757-200-SRM-51-40-02-OG. REVIEWED - [SDR IPXA2025040873394](https://openairdocs.org/sdr/IPXA2025040873394.md): Floor Panel · damaged · Apr 7, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > FAULT MCD FLOOR PANEL 242XGF HAS SURFACE /EDGE DAMAGE DOT 103-17. FABRICATED / INSTALLED MCD FLOOR PANEL 242XGF, IAW / UPS SREO: B757-9692-REQ 001. REVIEWED - [SDR IPXA2025041502950](https://openairdocs.org/sdr/IPXA2025041502950.md): Floorbeam · corroded · Apr 2, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Floor Beam > STA900. SIGNS OF EXFOLIATION ON LOWER BSTA 900 T-CHORD BETWEEN LEFT BUTTOCK LINE10"L AND 10"R. INSTALLED 01 EA CHORD AND 08 EA REPAIRS PARTS IAW B757-200 SRM 51-70-12-0G-0 STEPS 8 TO 10 AND SRM 51-40-02. REVIEWED - [SDR IPXA2025041665509](https://openairdocs.org/sdr/IPXA2025041665509.md): Frame · cracked · Mar 31, 2025 · N443UP · Boeing 75724APF · Engine Thrust Reverser > #2 ENG, O/B T/R, FWD SIDE, LOWER ACTUATOR AREA WITH A BRACKET CRACKED DOT 23-038. INSTALLED REPAIR ANGLE AND BRACKET IAW B757-200PF SRM 51-40-02-0G-0 FOR ACCOMPLISH STEP 1 OF E.A.# 757-7831-27-A3895 PRELIMINARY 1.REPAIR ACCOMPLISHED PER UPS EO: EO-93450-REQ2 - [SDR IPXA2025041063102](https://openairdocs.org/sdr/IPXA2025041063102.md): Support Angle · corroded · Mar 31, 2025 · N443UP · Boeing 75724APF · Fuselage Miscellaneous Structure > STR ANGLE SUPPORT CORRODED A LOWER DECK PLATE STA 1720 BTW LBL30.00 AND LBL 40.00.REMOVED ANGLE SUPPORT CORRODED A LOWER DECK PLATE STA 1720 BTW LBL30 AND LBL 40 IAW B757 SRM 51-10-02.LOCATED AND DRILLED NEW ANGLE IAW B757-200 SRM 51-40-05-0G-0.INSTALLED ANGLE - [SDR IPXA2025041148311](https://openairdocs.org/sdr/IPXA2025041148311.md): Keelbeam · corroded · Mar 30, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Keel > KEEL BEAM, SEC 44, AFT STA 900, FITTING BEHIND 139AL PANEL HAS EVIDEN OF CORROSION AROUND NUTPLATE HOLE. DOT 23-023.REMOVED CORROSION ON THE CHANNEL OF KEEL BEAM, AFT STA 900, FITTING BEHIND 139AL PANEL, AROUND NUTPLATE HOLE IAW B757 SRM 51-10-02.REMOVED CHANN - [SDR IPXA2025041807322](https://openairdocs.org/sdr/IPXA2025041807322.md): Support Bracket · damaged · Mar 28, 2025 · N443UP · Boeing 75724APF · Fuselage Miscellaneous Structure > AFT CARGO (BULK CARGO AREA) BETWEEN STA.1701 TO STA.1720, UPPER SIDE, BRACKET SUPPORTS AND NUTPLATE HAS CORROSION (8PLACES) DOT 103-33 (ATTACHED PHOTOS). INSTALLED ANGLES 2EA AN NUTPLATES AT AFT CARGO (BULK CARGO AREA) BETWEEN STA.1701 TO STA.1720, UPPER SID - [SDR IPXA2025040822166](https://openairdocs.org/sdr/IPXA2025040822166.md): Angle · corroded · Mar 28, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Structure > APU INLET DOOR UPPER ANGLE FROM STA 1787.45 TO STA 1825.00 HAS CORROSION.REMOVED 1E ANGLE + 1 EA PLATE IAW B757-200-SRM-51-40-02-OG.FABRICATED 1 EA ANGLE WITH MATERIAL PN EXTRUSION BAC1490-2738 BTCH 0004378076.INSTALLED 1 EA UPPER ANGLE IAW B757-200-SRM-51-40- - [SDR IPXA2025040822320](https://openairdocs.org/sdr/IPXA2025040822320.md): Angle · corroded · Mar 28, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Structure > APU INLET DOOR FWD UPPER CORNER ANGLE AT STA 1787.45 HAS CORROSION.REMOVED 1 EA CORRODED ANGLE IAW B757-200-SRM-51-40-02-OG.FABRICATED 1 EA ANGLE WITH MATERIAL PN EXTRUSION BAC1490-2738 BTCH 0004378076.INSTALLED 1 EA CORNER ANGLE B757-200-SRM-51-40-02-OG. - [SDR IPXA2025040822408](https://openairdocs.org/sdr/IPXA2025040822408.md): Angle · corroded · Mar 28, 2025 · N443UP · Boeing 75724APF · Fuselage Miscellaneous Structure > APU INLET DOOR FWD LOWER CORNER ANGLE AT STA 1787.45 HAS CORROSION. INSTALLED 1 EA SUPPORT ANGLE + 1 PLATE IAW B757-200-SRM-51-40-02-OG. - [SDR IPXA2025041298764](https://openairdocs.org/sdr/IPXA2025041298764.md): Skin · corroded · Mar 27, 2025 · N443UP · Boeing 75724APF · Nacelle/Pylon, Plate/Skin > # 2 PYLON OUTBD SIDE BETWEEN ACCESS PANELS SHOWS CORROSIONN AT INSIDE SKIN AREA. (RED DOT OUTSIDE). FABRICATED EXTERNAL REPAIR DOUBLER FOR ACCOMPLISHED STEP 19 OF EA # 757-5450-27-A3873 PRELIMINARY 3. VERIFIED FABRICATED EXTERNAL REPAIR DOUBLER FOR ACCOMPLISH - [SDR IPXA2025040892422](https://openairdocs.org/sdr/IPXA2025040892422.md): Floor Panel · damaged · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XDF HAS EDGES DAMAGED. DOT 103-26. FABRICATED MCD FLOOR PANEL 242XDF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED MCD FLOOR PANEL 242XDF FABRICATED. AUDIT COMPLETE - [SDR IPXA2025041492405](https://openairdocs.org/sdr/IPXA2025041492405.md): Floor Panel · damaged · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XEF HAS CORNER AND EDGES DAMAGED. DOT 103-23. FABRICATED MCD FLOOR PANEL 242XEF, IAW UPS SREO: B757-9692-REQ 001.VERIFIED MCD FLOOR PANEL 242XEF FABRICATED. - [SDR IPXA2025040287996](https://openairdocs.org/sdr/IPXA2025040287996.md): Floorbeam · corroded · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Floor Beam > FAULT: STR-200-MCC FLOOR STA.1200, LBL 0-62.225 HAS CORROSION.REMOVED NUTPLATE (11EA) ON STR-200-MCC FLOOR STA.1200, LBL 0-62.225 IAW B757-200 SRM 51-40-02-0G-0.REMOVED CORROSION IN THE AREA PER SRM 51-10-02.ACCOMPLISHED HFEC SURFACE ON FLOOR STA. 1200, LBL 0- - [SDR IPXA2025040892155](https://openairdocs.org/sdr/IPXA2025040892155.md): Floor Panel · damaged · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XKF HAS EDGE DAMAGED. DOT 103-07.FABRICATED MCD FLOOR PANEL 242XKF, IAW UPS SREO: B757-9692-REQ 001.AUDIT COMPLETE - [SDR IPXA2025040998346](https://openairdocs.org/sdr/IPXA2025040998346.md): Frame · cracked · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > NLG W/W FRAME ON THE LANDING GEAR DOOR, RIGHT SIDE AFT OF THE HINGE N2 WITH A CRACK DOT 07-043.REMOVED FRAME ON THE LANDING GEAR DOOR, RIGHT SIDE AFT OF THE HINGE N2 IAW B757-200 SRM 51-40-02-0G-0.INSTALLED NEW FRAME ON LANDING GEAR RH SIDE AFT OF THE HINGE N2 - [SDR IPXA2025040791891](https://openairdocs.org/sdr/IPXA2025040791891.md): Floor Panel · damaged · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XLF HAS EDGE DAMAGED. DOT 103-06. FABRICATED MCD FLOOR PANEL 242XLF, IAW UPS SREO: B757-9692-REQ 001 - [SDR IPXA2025040892043](https://openairdocs.org/sdr/IPXA2025040892043.md): Floor Panel · dented · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XMF HAS EDGE DAMAGED. FABRICATED MCD FLOOR PANEL 242XMF, IAW UPS SREO: B757-9692-REQ 001. - [SDR IPXA2025040892417](https://openairdocs.org/sdr/IPXA2025040892417.md): Floor Panel · dented · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XDF, INNER SURFACE HAS DENTS (3EA). FABRICATED / INSTALLED MCD FLOOR PANEL 242XDF, IAW UPS SREO: B757-9692-REQ 001. - [SDR IPXA2025040892390](https://openairdocs.org/sdr/IPXA2025040892390.md): Floor Panel · dented · Mar 27, 2025 · N443UP · Boeing 75724APF · Fuselage Floor Panel > MCD, FLOOR AREA, PANEL 242XFF, INNER SURFACE HAS DENTS (10EA). DOT 103-22. FABRICATED MCD FLOOR PANEL 242XFF, IAW UPS SREO: B757-9692-REQ 001 USING MATERIALS, PNL PN: 5024N400001SS-G BAT: 0004055277, PLUG PN: G2001B-3P, BAT: 0004365510, SLEEVE PN: G2002B-3S, - [SDR IPXA2025041681038](https://openairdocs.org/sdr/IPXA2025041681038.md): Frame · dented · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > AFT CARGO COMPARTMENT BS1500 / S25L-S27L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-27, ENRIQUE BARREIRO. INSTALLED J SECTION REPAIR PER SRM 53-00-07-2R-5 DETAIL I. REVIEWED - [SDR IPXA2025041680829](https://openairdocs.org/sdr/IPXA2025041680829.md): Frame · dented · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > AFT CARGO COMPARTMENT BS1600 / S26L-S25L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-25, ENRIQUE BARREIRO. INSTALLED STRIGER CLIP (2EA) AND REPAIR SPLICE ON AFT CARGO COMPARTMENT BS1600 / S26L-S25L FUSELAGE FRAME IAW B757-200 SRM 53-00-07-2R-5 MATERIAL US - [SDR IPXA2025041380768](https://openairdocs.org/sdr/IPXA2025041380768.md): Angle · corroded · Mar 26, 2025 · N443UP · Boeing 75724APF · Aerodynamic Fairings > -WING/BODY STRUCTURE ON PANEL 192DR NUTPLACE BRACKET WITH CORROSION DOT 07-036. INSTALLED (BRACKET) AND NUT PLATES AT WING/BODY STRUCTURE ON PANEL 192DR IAW B757-200 SRM 51-40-02. REVIEWED - [SDR IPXA2025041480002](https://openairdocs.org/sdr/IPXA2025041480002.md): Frame · corroded · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > FAULT - STR - Z162- AFT CARGO COMPARTMENT BS1300 / S26R FRAME HAS A DENT. DOT 95-22, ENRIQUE BARREIRO. INSTALLED NEW J SECTION. IAW SRM 51-40-02. MATERIAL USED 21EA BOLT P/N BACB30MY6K4X BATCH 0004365542, 21EA COLLAR P/N BACC30AC6 BATCH 0004198709 AND SEAL P/ - [SDR IPXA2025041580671](https://openairdocs.org/sdr/IPXA2025041580671.md): Frame · dented · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > FAULT - STR - Z162 - AFT CARGO COMPARTMENT BS1480 / S25R FUSELAGE FRAME HAS A DENT. DOT 95-24, ENRIQUE BARREIRO. INSTALLED SUPPORT PANEL AT AFT CARGO COMPARTMENT BS1480 FUSELAGE FRAME IAW B757-200 SRM 51-40-02-0G MATERIAL USED P/N:BAC330NX6K3 BTCH:0004325741 - [SDR IPXA2025041580950](https://openairdocs.org/sdr/IPXA2025041580950.md): Frame · dented · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Frame > FAULT - STR - Z161 - AFT CARGO COMPARTMENT BS1580 / S26L-S25L FUSELAGE FRAME HAS 2 EA DENTS AS MARKED. DOT 95-26, ENRIQUE BARREIRO. INSTALLED 1EA REPAIR SPLICE AND 2EA STRINGER CLIPS IAW B757-200PF SRM 51-40-02-0G FOR ACCOMPLISH REPAIR IAW SRM 53-00-07-2R-5 D - [SDR IPXA2025041180978](https://openairdocs.org/sdr/IPXA2025041180978.md): Bracket · corroded · Mar 26, 2025 · N443UP · Boeing 75724APF · Aerodynamic Fairings > RH WING/BODY STRUCTURE IN PANEL 196AR NUTPLACE HAVE CORROSION DOT 07-038. REMOVED BRACKET ON WING BODY 196AR IAW B757-200 SRM 51-40-02-0G-0 BRACKET P/N 149N7550-50.LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-05-0G-0.TRETATED AND PRIMED NEW BRACKET IAW SRM 51 - [SDR IPXA2025041380559](https://openairdocs.org/sdr/IPXA2025041380559.md): Angle · corroded · Mar 26, 2025 · N443UP · Boeing 75724APF · Fuselage, Wing Attach Fittings > LEFT WING ROOT ON PANEL 191DL NUTPLACE BRACKET HAVE EEVIDENCE OF CORROSION DOT 07-034.REMOVED 4EA NUTPLATES ON BRACKET AT 191DL PANEL IAW B757-200 SRM 51-40-02-0G-0.BLENDED CORROSION ON BRACKET AT 191DL PANEL IAW B757-200 SRM 51-10-02-0G-0.REMOVED BRACKET ON 1 - [SDR IPXA2025041053539](https://openairdocs.org/sdr/IPXA2025041053539.md): Support Channel · cracked · Mar 25, 2025 · N443UP · Boeing 75724APF · Fuselage Miscellaneous Structure > FAULT-STR-Z100-RH MLG W/W IN FRONT FRAME IN RETAINER SEAL HAVE A CRACK DOT 07-011. INSTALLED SUPPORT CHANNEL AND RETEINER. IAW B757-200 SRM 51-40-02. REVIEWED - [SDR IPXA2025041452165](https://openairdocs.org/sdr/IPXA2025041452165.md): Angle · corroded · Mar 25, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Structure > APU INLET DOOR LOWER ANGLE CORRODED BETWEEN STA 1787.45 TO STA 1825.00. R/H.REMOVED 1E ANGLE + 1 EA PLATE IAW B757-200-SRM-51-40-02-OG.FABRICATED 1 EA ANGLE WITH MATERIAL PN EXTRUSION BAC1490-2738 BTCH 0004378076.INSTALLED 01EA ANGLE + 01EA PLATE.IAW B757-200- - [SDR IPXA2025030911672](https://openairdocs.org/sdr/IPXA2025030911672.md): Mount · bent · Mar 1, 2025 · N443UP · Boeing 75724APF · Fuselage Main, Attach Fittings > EVAS MOUNTING BRACKET DETACHED INSTALLED NEW MOUNT PLATE WRT EO B757-2560-45127-H, INSTALLED ORIGINAL SERVICEABLE EVAS UNIT FROM PFM IAW AMM 25-69-00. THIS ACTION CLEARS MEL 25-60-1, DMP REVERSED. PLACARD REMOVED. - [SDR IPXA2023033092438](https://openairdocs.org/sdr/IPXA2023033092438.md): Shear Web · corroded · Mar 18, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3CORROSION FOUND UNDER DRAIN PAN AT STA 324 RBL 0 TO RBL 24.75REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023033092437](https://openairdocs.org/sdr/IPXA2023033092437.md): Shear Web · corroded · Mar 18, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3CORROSION FOUND UNER DRAIN PAN AT STA 324 RBL 24.5 TO RBL 45.5REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023040192492](https://openairdocs.org/sdr/IPXA2023040192492.md): Shear Web · corroded · Mar 17, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG346 AREAS OF CORROSION UNDER FLOOR PANEL 222XCF RBL 45.5 TO RBL 67.5 STA 324 TO STA 436REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023040192488](https://openairdocs.org/sdr/IPXA2023040192488.md): Shear Web · corroded · Mar 17, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG334 AREAS OF CORROSION UNDER FLOOR PANEL 221XCF LBL 45.5 TO LBL 67.5 STA 324 TO STA 436REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023032592238](https://openairdocs.org/sdr/IPXA2023032592238.md): Floor Panel · cracked · Mar 17, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Plate/Skin > INSPECTION TYPE:SEG3PNL 232NF CRACKEDFABRICATED PNL 232NF PER SREO B757-5320-9692-K - [SDR IPXA2023040192490](https://openairdocs.org/sdr/IPXA2023040192490.md): Shear Web · corroded · Mar 16, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG316 AREAS OF CORROSION UNDER FLOOR PANEL 221XBF LBL 24.75 TO LBL 45.5 STA 324 TO STA 418REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023033092440](https://openairdocs.org/sdr/IPXA2023033092440.md): Shear Web · corroded · Mar 16, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG314 AREAS OF CORROSION MAIN CARGO BAY UNDER FLOOR PANEL 221XAF BL0 TO LBL 24.75 STA 340 TO STA 377.7REMOVED CORROSION AND FOUND TO BE IN LIMITS IAW SRM 53-10-51-1A-2 - [SDR IPXA2023040292508](https://openairdocs.org/sdr/IPXA2023040292508.md): Skin · dented · Mar 15, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3*MAJOR REPAIR* AFT LEFT FUSELAGE SKIN AT STA 1360 S-24L HAS A DENT DAMAGE ON SKIN WITH CREASING AND INTO FRAME WITH PULLING RIVETSREPAIRED SKIN PER EA 757-5360-27-A3175 - [SDR IPXA2023033192479](https://openairdocs.org/sdr/IPXA2023033192479.md): Skin · dented · Mar 14, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3*MAJOR REPAIR* AFT CARGO DOOR SKIN HAS A DENT AT STA 1410 BELOW STRINGER 21REPAIRED SKIN PER SRM 53-30-01-2R-4 - [SDR IPXA2023040192494](https://openairdocs.org/sdr/IPXA2023040192494.md): Frame · dented · Mar 14, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3*MAJOR REPAIR* AFT CARGO FRAME 1460 LH SIDE, HAS A DENT ON TOP OF THE FRAME FLANGE BY S-26LREPAIRED FRAME PER SRM 53-00-07-2R REPAIR 5 - [SDR IPXA2023033192478](https://openairdocs.org/sdr/IPXA2023033192478.md): Frame · dented · Mar 14, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3*MAJOR REPAIR* AFT CARGO FRAME 1600 R/H SIDE, HAS A DENT ON TOP OF THE FRAME FLANGE BY S-26RREPAIRED FRAME PER SRM 53-00-07-2R-D DETAIL 3 - [SDR IPXA2023032992410](https://openairdocs.org/sdr/IPXA2023032992410.md): Frame · none · Mar 13, 2023 · N443UP · Boeing 75724APF · Fuselage Main, Structure > INSPECTION TYPE:SEG3DURING INSPECTION OF EO (B757-5310-73926-A) FOUND AN EXISTING REPAIR AT STA 1300 LH STR 23L-28LCOMPLETED WORK PER UPS EO B757-5310-43353-D AND VT MAE EA 757-5360-27-A3165 REV - AND UPS RCD 275237 - [SDR IPXA2022120188606](https://openairdocs.org/sdr/IPXA2022120188606.md): Bracket · not reported · Nov 30, 2022 · N443UP · Boeing 75724APF · Accessory Compartment > CREW DOOR INDICATION INOPERATIVE. REPLACED CREW ENTRY DOOR SENSOR BRACKET, OPS CHECK NORMAL IAW AMM 52-71-00-825-223. ORIG SUB DATE: 12/1/2022 - [SDR IPXA2022112288365](https://openairdocs.org/sdr/IPXA2022112288365.md): Elt · inoperative · Nov 19, 2022 · N443UP · Boeing 75724APF · Emergency Locator Beacon > INSPECTION TYPE:N/AELT FAILED TEST (PORTABLE)R&R PORTABLE ELT IAW TC 0101 STEP 19A, B, C, ON PS2AF Next page: https://openairdocs.org/aircraft/N443UP/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 = 'N443UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N443UP/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.