N412UP

Service difficulty reports · 248

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N412UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA2026092882672Evas Unit · dislodgedCAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED. INSTALLED CAPTAIN (LEFT) SIDE EVAS PER AMM 25-60-00.Sep 23, 2026 · N412UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2026092382672Evas Unit · dislodgedCAPTAIN (LEFT) SIDE EVAS CONTAINER LID DISLODGED AND EVAS EXPOSED, DEFERRAL REMAINSSep 23, 2026 · N412UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2026060280694Skin · damagedAFTER REMOVAL OF DME ANTENNA, FOUND SIGNS OF CORROSION. CHECKED LIMITS AT FUSELAGE SKIN AREA ORIGINAL THICKNESS .080 IAW DWG# 143N3471 BLENDED DIMENSIONS L=5.500'', W=2'', X=.004'' MAXIMUM ALLOWABLE X=15%=.012'' AREA FOUND TO BE WITHIN LIMITS IAW B757-200PF SMay 20, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026052180694Skin · corrodedAFTER REMOVAL OF DME ANTENNA,, FOUND SIGNS OF CORROSION.May 20, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2026053022584Attach Fitting · corrodedUPON REMOVAL OF UPPER AND LOWER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND TRAILING EDGE TIP FAIRING ASSEMBLY WITH EVIDENCE OF CORROSION, INSTALLED ELEVATOR ATTACHMENT FITTING, ELEVATOR TIP AND STATIC WICK BASE AT LH ELEVATOR T/E, TIP AREA IAW SRM 51-4May 16, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2026052622502Frame · corrodedUPON REMOVAL OF UPPER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND UPPER CONDUCTIVE FRAME CORRODED. INSTALLED NEW UPPER CONDUCTIVE FRAME P/N:183N2007Y8 BATCH:0004487190 AT LH ELEVATOR TIP OTBD END IAW B757-200PF SRM 51-40-02-0G-0 AND SRM 51-40-04-0G-0.May 16, 2026 · N412UP · Boeing 75724APF · Elevator, Spar/RibSDR IPXA2026052622562Frame · corrodedUPON REMOVAL OF LOWER SPLICE PLATE AT LH ELEVATOR T/E, TIP AREA, FOUND LOWER CONDUCTIVE FRAME CORRODED, INSTALLED NEW LOWER CONDUCTIVE FRAME IAW SRM 51-40-02-0G-0 AND SRM 51-40-04-0G-0.May 16, 2026 · N412UP · Boeing 75724APF · Elevator, Spar/RibSDR IPXA2026060328065Support Angle · damagedAFT CARGO COMPARTMENT AFT BULKHEAD ACCESS PANEL UPPER SUPPORT ANGLE HAS CORROSION AND 2 EA ELONGATED HOLE APPROX AT BS 1640 BTW RBL 50 AND LBL 50, INSTALLED UPPER SUPPORT ANGLE AT AFT CARGO COMPARTMENT AFT BULKHEAD AT BS 1640 BTW RBL 50 AND LBL 50 IAW B757-200May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060226363Skin · crackedNR 2 PYLON UPPER SKIN 12 HOLE HAS CRACK AT 12 O'CLOCK POSITION AT LOWER LAYER. ACCOMPLISHED REPAIR PER EO-97524-REQ1 AND VT-SAA EA 757-5700-01-B0750, REV I/R.May 11, 2026 · N412UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2026052629850Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 45.50, INSTALLED FABRICATED STABILIZATION STRAP, REPAIR SPLICE AND 9EA NUT PLATES AT AFT CARGO COMP STA 1540-1610, LBL 45.50 CEILING PANEL IAW May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052629952Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 24.75, INSTALLED 01EA STABILIZATION STRAP CEILING PANEL AT RBL 24.75 BETWEEN FS 1360-1440 IAW SRM 51-40-02-0G-0 AND SRM 51-70-11-0G-0.May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052629852Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 24.75, INSTALLED FABRICATED STABILIZATION STRAP, 01EA SPLICE AND 5EA NUT PLATES AT AFT CARGO COMP STA 1540-1610, LBL 24.75 IAW B757-200PF SRM May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052629933Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 45.50, INSTALLED 01EA SECTION OF STABILIZATION STRAP @ RBL 45.50 BETWEEN FS 1360-1470 REF SRM 51-40-02-0G-0 AND 51-70-11-0G-0.May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060232065Mount · gougedNR 2 ENG AFT MOUNT HAS CHIPPED MATERIAL ON UPPER SURFACE, FLL-0035, ATA 71. ACCOMPLISHED REPAIR PER EO-97541-REQ1 AND VT-SAA EA 757-7121-01-B0744 REV I/R.May 11, 2026 · N412UP · Boeing 75724APF · Engine Mount SectionSDR IPXA2026052627817Floorbeam · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR BEAM ASSY UPPER FLANGE HAS 4 EA NUT PLATE CORRODED APPROX AT BS 1681.8, BTW BL 0 AND RBL 50, ID STICKER NUM. (085-015) ATA 53-10. INSTALLED 2EA NEW NUT PLATE STRAPS ASSY AT AFT OF BULK CARGO COMPARTMENT FLOOR BEAM ASSY UPPEMay 11, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026052129933Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 45.50,May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026052129850Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, BTW BS 1560 AND BS 1580, LBL 45.50,May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026052129952Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 24.75,May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052129852Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1560 AND BS 1580, LBL 24.75,May 11, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026051619006Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 12.50, ID STICKER NUM. (085-005) ATA 53-20 INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, RBL 12.50. May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026051619025Nut Plate · corrodedSTR, AFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 5, ID STICKER NUM. (085-006) ATA 53-20 INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, RBL 5. IAWMay 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026052419140Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 23, ID STICKER NUM. (085-009) ATA 53-20 INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, LBL 23. IAW B7May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026051619223Nut Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1710, RBL 51, ID STICKER NUM. (085-011) ATA 53-20 INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1710, RBL 51. IAW B75May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026052414678Bracket · corrodedRIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 ES-046. INSTALLED 2 EA WTB FAIRING BRACKETS, P/N: 149N7210-70SAAU AND P/N: 149N7210-76SAAU AT RIGHT WING TO BODY FARING AT B.S. 906.5 IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 149N7210.May 10, 2026 · N412UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026052418871Deck Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 23, I INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, RBL 23, IAW B757-200 SRM 51-40-02-OG-0.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026060214234Crossbeam · damagedMAIN DECK WING CENTER SECTION FLOOR PANEL 241XBF STA 900 BTW LBL 24.75 AND LBL 45.5 HAS FLOOR PANEL FRAME SUPPORT BROKEN, FLL-003, ATA 53. INSTALLED 01 EA NEW STRAP SUPPORT AT MAIN DECK WING CENTER SECTION STA 900 BTW LBL 24.75 AND LBL 45.5 IN REF SRM 51-40-0May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026052419117Strap · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 12.50. INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, LBL 12.50 IAW SRM 51-40-02-OG-0.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060219107Nut Plate · damagedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 36.50, INSTALLED NUT PLATE STRAP AT FLOOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, LBL 36.50 IAW B757-200 SRM 51-40-02-OG-0.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026060219038Nut Plate · damagedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 5, ID STICKER NUM. (085-007) ATA 53-20. INSTALLED NUT PLATE STRAP AT FLOR DECK PLATE SUPPORT ANGLE ASSY APPROX AT BS 1715, LBL 5 IAW B757-2May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026052118868Support Angle · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY HAS CORROSION APPROX AT BS 1715, RBL 36.50. INSTALLED NEW SUPPORT ANGLE AND NUTPLATE STRAP ASSY AT AFT OF BULK CARGO COMPLARTMENT FLOOR DECK PLATE APPROX AT BS 1715, RBL 36.50 IAW SRM 51-40-0May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052114678Bracket · corrodedRIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 OUT OF LIMITSMay 10, 2026 · N412UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026052114234Floor Support · brokenMAIN DECK WING CENTER SECTION FLOOR PANEL 241XBF STA 900 BTW LBL 24.75 AND LBL 45.5 HAS FLOOR PANEL FRAME SUPPORT BROKEN, C/W SRM 51-20-01-0G-0.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026051619038Support Angle · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 5,May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026051618871Deck Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, RBL 23. QC AUDIT C/W.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026051619107Nut Plate · damagedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 36.50.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2026051619117Plate · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR DECK PLATE, SUPPORT ANGLE ASSY NUT PLATE STRAP HAS CORROSION APPROX AT BS 1715, LBL 12.50.May 10, 2026 · N412UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026052405432Control Wheel · corrodedCOPILOTS CONTROL WHEEL OUTER SKIN CORRRODED RH SIDE. INSTALLED SERVICEABLE COPILOTS AILERON CONTROL WHEEL AND ADAPTER IAW AMM 27-11-02-424-010 TW ID:19-983 DD:09/03/2026May 9, 2026 · N412UP · Boeing 75724APF · Aileron Control SystemSDR IPXA2026060205494Skin · crackedNR 2 ENG FIRE LOOP ACCESS PANEL L/E SKIN CRACKED . INSTALLED EXTERNAL REPAIR DOUBLER AT #2 ENG FIRE LOOP ACCESS PANEL IAW E.A.# 757-5741-01-B0742 REV P1 STEP 7. ACCOMPLISHED PERMANENT REPAIR PER EO-97550-REQ1 AND VT-SAA EA 757-5741-01-B0742, REV. I/R.May 9, 2026 · N412UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2026060178921Angle · corrodedL/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STRAP) AT L/H HORZ STAB TO ELEVATOR OTBD IAW SRM 51-40-02-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Elevator Miscellaneous StructureSDR IPXA2026060378913Bracket · damagedR/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STRAP) AT R/H HORZ STAB TO ELEVATOR OTBD IAW B757-200PF SRM 51-40-02-0G-0. REVIEWEDMay 8, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2026052478794Frame · corrodedRT ELEVATOR OTBD END UPPER CONDUCTIVE FRAME DISBONDED AT AREA UNDER CORRODED STATIC WICK BASE. RL003. INSTALLED CONDUCTIVE FRAME , AND INSTALLED STATIC WICK BASE ASSY AT R/H ELEVATOR IAW 51-40-02-0G-0 , SRM 51-40-04-0G-0 , AMM TASK 23-61-01-402-028 AND AMM May 8, 2026 · N412UP · Boeing 75724APF · Elevator, Spar/RibSDR IPXA2026052478671Skin · corrodedL/H ELEVATOR TO TIP (UPPER AND LOWER) SPLICE PLATE HAVE CORROSION WITH POPPED RIVET. RL013. INSTALLED UPPER SPLICE PLATE P/N 183N2007-5SAAU AND LOWER SPLICE PLATE P/N 183N2007-6SAAU AT L/H ELEVATOR TO TIP IAW B757-200PF SRM 51-40-02-0G-0 AND SRM 51-40-04-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2026052793693Support Angle · crackedNR 1 PYLON HYD BAY O/B SIDE ACCESS PNL CUT-OUT HAS LOWER, FWD SUPPORT ANGLE WITH CRACKS. 83-017. ATA 54-40. INSTALLED ANGLE (SPRING CLIP) AT NR 1 PYLON HYD BAY O/B SIDE ACCES PANEL CUT-OUT IAW SRM 51-40-02-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026052793074Support Angle · crackedNR 1 PYLON HYD BAY FWD, UPPER SUPPORT ANGLE HAS A CRACK AT OTBD END. PRODUCTION AUDIT C/W. INSTALLED SUPORT ANGLE (BEAM) AT #1 PYLON HYD BAY FWD UPPER IAW B757-200PF SRM 51-40-02-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026052178671Structure · corrodedLEFT ELEVATOR TO TIP (UPPER AND LOWER) SPLICE PLATE HAVE CORROSION WITH POPPED RIVET. C/W SRM 51-40-02-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2026052178794Frame · debondedRIGHT ELEVATOR OTBD END UPPER CONDUCTIVE FRAME DISBONDED AT AREA UNDER CORRODED STATIC WICK BASE.May 8, 2026 · N412UP · Boeing 75724APF · Elevator Miscellaneous StructureSDR IPXA2026051678913Bracket · corrodedR/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. INSTALLED WEB, NEW ANGLE (BRACKET) AND NEW BONDING JUMPER (STRAP) IAW SRM 51-40-05-0G-0.May 8, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2026051678921Attach Angle · corrodedL/H HORZ STAB TO ELEVATOR OTBD END BONDING STRAP ATTACH BRACKETS APPEARS TO HAVE LIGHT CORROSION. RL014 VERIFIED STEP 1 AND 2.May 8, 2026 · N412UP · Boeing 75724APF · Elevator StructureSDR IPXA2025022013683Proximity Switch · out of adjustON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY SWITCH OUT OF PROPER ADJUSTMENT. ADJUSTED PER AMM 52-71-00. OPS CHECK NORMAL. REMOVED ICE AND SNOW CFeb 18, 2025 · N412UP · Boeing 75724APF · Door Warning SystemSDR IPXA2025021913683Proximity Switch · out of adjustON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY SWITCH OUT OF PROPER ADJUSTMENT. ADJUSTED PER AMM 52-71-00. OPS CHECK NORMAL. REMOVED ICE AND SNOW CFeb 18, 2025 · N412UP · Boeing 75724APF · Door Warning System
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