N411UP

Service difficulty reports · 199

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 = 'N411UP' 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 IPXA2026080363542Duct · warning messageLEFT BLD DUCT LEAK EICAS MSG AT F340. QRH CHECKLIST COMPLETED AND L BLD DUCT LEAK MESSAGE WENT AWAY. PERFORMED FIM 26-90-15-00 SHEET 1 FIG 103 STEPS 1,10,2, SHEET 2 FIG 103 STEPS 3,4,11,12,13, & 14, HAD A FAULT CODE 14, PERFORMED STEP 15 FIG 103, SHEET 3. CARAug 1, 2026 · N411UP · Boeing 75724APF · Pneumatic Distribution SystemSDR IPXA2026012304472Web · damagedSTA 1200 UPPER WEB HAS A DAMAGED HOLE. AFTER FURTHER EVALUATION FOUND 4 DOUBLE HOLE AT THE TOP OF THE WEB. FOUND OUT OF LIMITS IAW B757-200 SRM 53-00-71-1A-1 AD1. CUT AND REMOVE DAMAGED SECTION OF WEB. IAW B757-200 SRM 51-70-13-0G-0 STEP 1. ++INSTALLED REPAIRSJan 14, 2026 · N411UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026011963930Seat Track · corrodedCAP SEAT TRACKS HAVE EVIDENCE OF CORROSION (AFT I/B EXFOLIATED) MARKED AREAS. REMOVED CORROSION LOCATED ON MAIN DECK FLOOR SHEAR UNDER SEAT TRACK. LBL13.0 AND 20'' UPPER STA278.0 O.T: .050''. MAT LOSS:0.035''. L:0.7'', W:0.7'' REWORK WAS FOUND OUT OF LIMITS IJan 12, 2026 · N411UP · Boeing 75724APF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026020462981Stringer · corrodedFUSELAGE SKIN IS BULDGING AROUND TWO FASTNER HEADS, JUST FORWARD OF THE AFT LOWER FUSELAGE MAJOR REPAIR AT AFT VHF ANTENNA. REMOVED 3 BULDGING RIVETS FORWARD OF THE AFT LOWER FUSELAGE MAJOR DOUBLER REPAIR AT STATION 1460 AND FRAME 1480 OF AFT VHF ANTENNA, NOJan 12, 2026 · N411UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026013069167Tee Angle · corrodedWING TO BODY FAIRING STRUCTURE LOWER T-CHORD EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO 1240 AT RBL 57.50. DOT 21-40. EVALUATED TEE FITTING BETWEEN STA 1180-1240 AT RBL 57.5 AND FOUND TO BE EXFLOIATED WITH 100% MATERIAL LOSS AND ISJan 12, 2026 · N411UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026012869037Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE UPPER TEE FITTING EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO BS 1240, RBL 57.50. REMOVED AFT WTB PANEL 198LR TO FOM IAW AMM 53-66-01-004-001. INSTALLED THE TEE FITTING IAW SRM 51-40-02.Jan 12, 2026 · N411UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026012868936Channel · corrodedWING TO BODY FAIRING SUPPORT STRUCTURE WITH EXFOLIATED CORROSION AT BS 1219 RBL 6. INSTALLED NEW CHANNEL, 2EA SUPPORT PLATES, 1EA ANGLE, IN WING TO BODY, BS 1219 RBL 6, IAW B757 SRM 51-40-02-0G-0.Jan 12, 2026 · N411UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026012869140Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE, VERTICAL T-FITTING EXFOLIATED AT LWR END AT BS 1200 RBL 57.50. INSTALLED T-FITTING IAW SRM 51-40-02.Jan 12, 2026 · N411UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026011955833Skin Panel · corrodedAPU BAY, INTERNAL STRUCTURE RT SIDE, BTWN BS 1885.2 & 1918.9, ALUMINUM HONEYCOMB SKIN HAD CORROSION. TRIMMED OUT LOWER FWD SECTION OF HONEYCOMB ONLY ON SKIN BOND ASSY. PANEL TO REMOVE EXFOLIATED CORROSION, ACCOMPLISHED AND INSPECTION OF THE STRINGER AND SURROJan 11, 2026 · N411UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026013056128Longeron · corrodedAPU BAY, INTERNAL STRUCTURE RT LONGERON, BS 1885.2 CORRODED. REMOVED CORROSION ON THE RT APU LONGERON, ORIGINAL THICKNESS 0.050", MATERIAL REMOVED 0.008". INSTALLED NEW LONGERON, SERVICABLE SEAL RETAINER, SERVICABLE SUPPORT PLATES, SERVICABLE HINGE ASSY, SJan 11, 2026 · N411UP · Boeing 75724APF · APU Cowling/ContainmentSDR IPXA2026013056154Intercostal · crackedMDC DOOR INTERNAL STRUCTURE, AN INTERCOSTAL FOUND CRACKED AT FWD LWR SECTION. REMOVED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AFTER EVALUATION FOUND CRACK TO BE OUT OF LIMITS, FLANGE 1.095", LENGTH 0.940", IAW 52-30-02-1A-1, DETAIL II, NOTE B. INSTALLED NEW IJan 11, 2026 · N411UP · Boeing 75724APF · Cargo/Baggage DoorsSDR IPXA2026012234008Skin · crackedLEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE HAS A GOUGE, AREA BY SLAT NR 1 OTBD END. PERFORMED CUT OUT OF THE AFFECTED PANEL FROM THE CENTER LINE OF THE MAIN TRACK AT OSS 809.46 TO THE OTBD END OF PANEL, IAW EA 757-5741-27-A4274 PRELIMINARY 1, STEP 3. INJan 9, 2026 · N411UP · Boeing 75724APF · Wing, Plate/SkinSDR IPXA2026012833721Tee Fitting · corrodedLEFT WING TO BODY FAIRING STRUCTURE WITH TEE FITTINGBEAM EXFOLIATED BTWN STA 1200 AND 1220 AT BL 57.50. INSTALLED NEW T-FITTING P/N: UP-149N7630-37 BETWEEN STA 1180-1240 LBL 57.50 I.A.W B757-200 SRM 51-40-02-OG.Jan 9, 2026 · N411UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2026011209109Floorbeam · corrodedSTR Z100 FAULT: FRETTING CORROSION ON T-ANGLE AT STA 1037, LBL 5 TO LBL 15 INSTALLED T-CHORD. IAW B757-200 SRM 51-40-02.Jan 8, 2026 · N411UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026012709232Floorbeam · corrodedFRETTING CORROSION ON FLOORBEAM T-ANGLE AT BS 900 BETWEEN LBL 7 TO LBL 12. REVIEWED.Jan 8, 2026 · N411UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026012110991Angle · corrodedANGLE AT BS 1037, LBL 60 HAD CORROSION. INSTALLED NEW ANGLES 2EA IAW SRM 51-40-02.Jan 8, 2026 · N411UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026013096567Tee Fitting · corrodedTEE FITTING AT BS 1147, RBL 65 SHOWS SIGNS OF LIGHT CORROSION. REMOVED THE DAMAGED TEE FITTING IAW SRM 51-40-02. INSTALLED NEW TEE FITTING P/N: UP-149N7222-69 BETWEEN BS 1147 RBL 65 IAW SRM 51-40-02-OG.Jan 7, 2026 · N411UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026013096671Tee Fitting · corrodedTEE FITTING, BS 1037 - 1060, LBL 37, HAD EXFOLIATING CORROSION. REMOVED FLOOR PANEL 198CR AT EXHAUST AREA BTWN BS 1037 TO 1060, RBL 65 TO FACILITATE THE EVALUATION IAW SRM 51-40-02-0G. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.Jan 7, 2026 · N411UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2026012896589Tee Fitting · corrodedTHE OTBD T-FITTING FOR ECS EXHAUST, STA 1037-1060, RBL 60 HAS CORROSION. INSTALLED T-FITTING IN STA 1037-1060, RBL 60 PER B757-200 SRM 51-40-02.Jan 7, 2026 · N411UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026010996688Tee Fitting · corrodedTEE FITTING, BS 1037 - 1060, LBL 60, EXFOLIATING CORROSION. REMOVED THE TEE FITTING IAW SRM 51-40-02. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.Jan 7, 2026 · N411UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2025032894505Bleed Air Sys · oscillatesRIGHT BLEED AIR OSCILLATING RAPIDLY AT FL 390. THIS WAS CAUSING ENG TO SURGE FROM 1.17 TO 1.34 EPR ALONG WITH A YAWING MOTION TO AIRCRAFT. AFTER BLEED VALVE SHUT OFF, ENG BEHAVED NORMALLY. R/R R/H ENG PRSOV IAW AMM 36-11-09-401. BLEED PRESSURE NORMAL. NO FLUCTMar 27, 2025 · N411UP · Boeing 75724APF · Engine Bleed Air SystemSDR IPXA2025032794505Bleed Valve · faulted**SDR FILED OPEN** **DIVERSION**RIGHT BLEED AIR OSCILLATING RAPIDLY AT FL 390. THIS WAS CAUSING ENG TO SURGE FROM 1.17 TO 1.34 EPR ALONG WITH A YAWING MOTION TO AIRCRAFT. AFTER BLEED VALVE SHUT OFF, ENG BEHAVED NORMALLY.Mar 27, 2025 · N411UP · Boeing 75724APF · Compressor Bleed ValveSDR IPXA2024020680118Skin · damagedR/H ELEVATO AFT TIP HAS EXFOILATION ON TO AND BOTTOM MARKED IN RED. DOT 140-1 INSTALLED R/H ELEVATOR IAW AMM 27-31-01-424-028. REPLACED ROD END OF POSITION TRANSMITER IAW AMM 27-38-02-424-018. PERFORMED ELEVATOR OP CHECK, TEST PASS IAW AMM 27-31-00-715-331 REVFeb 2, 2024 · N411UP · Boeing 75724APF · Elevator, Plate/SkinSDR IPXA2024021625858Skin · corrodedFAULT: #2 ENG O/B CORE COWL HAS CORROSION I/B UP TOP IN THE MIDDLE. DOT 33-010 INSTALLED #2 ENG O/B CORE COWL IAW AMM 71-11-06-404-036-P00 UNTILL STEP G (4).Jan 31, 2024 · N411UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024020936216Angle · corrodedANGLE WITH CORROSION IN LH RUDDER PEDAL ASSY. DOT 07308-001 INSTALLED NEW ANGLE I.A.W. SRM 51-40-02-0G.Jan 31, 2024 · N411UP · Boeing 75724APF · Rudder Control SystemSDR IPXA2023101658163Bulkhead · cracked*SUPPLEMENTAL SDR* R\H PYLON, HYD BAY, AFT SIDE OF PYLON BULKHEAD, UPPER SUPPORT ANGLE, I\B SIDE, HAS AN 1 1\2 INCH CRACK. VERIFIED HEAT TREATMENT PER NDTM, PART 4, 51-00-10. COMPLETED INSTALLATION PER DRAWING 313N3052Oct 12, 2023 · N411UP · Boeing 75724APF · Nacelle/Pylon, Bulkhead/FirewallSDR IPXA2023101358163Unknown · unknown*SDR FILED OPEN* R\H PYLON, HYD BAY, AFT SIDE OF PYLON BULKHEAD, UPPER SUPPORT ANGLE, I\B SIDE, HAS AN 1 1\2 INCH CRACKOct 12, 2023 · N411UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2022090185804None · noneINSPECTION TYPE:**SDR FILED OPEN** L FWD ENTRY DOOR EICAS AFTER LANDING \, DURING TAXI, ILLUMINATED. WENT OUT AFTER 1 MINUTE. DEFERRED LEFT FWD ENTRY DOOR INDICATION SYSTEM IAW MEL 52-71-1.. DMP C/W. PLACARD INSTALLED.Sep 1, 2022 · N411UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2020052255632Fitting · crackedINSPECTION TYPE:SEG3UPPER SKIN FITTING RH PYLON #3 HOLE HAD REJECTABLE CRACK INDICATIONS AT BOTTOM OF HOLEREAMED HOLE TO REMOVED INDICATION PER E.O. B757-5720-76605-A.May 22, 2020 · N411UP · Boeing 75724APF · Wing Main, Frame StructureSDR IPXA2020052255631Fitting · damagedINSPECTION TYPE:SEG3UPPER SKIN DRAG FITTING RH PYLON #1 HOLE HAS VISUAL DAMAGEREAMED HOLE TO REMOVED DAMAGE PER E.O. B757-5720-76605-A.May 22, 2020 · N411UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA2020052255627Skin · crackedINSPECTION TYPE:SEG3UPPER SKIN RH PYLON #8 HOLE HAS CRACK INDICATIONSREPAIRED PER EO BY REMAINING HOLE TO REMOVED DAMAGE B757-5720-76605-AMay 22, 2020 · N411UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2020052055527Angle · corrodedINSPECTION TYPE:SEG3ANGLE SUPPORT FWD RAT CUTOUT BEAM HAS CORROSION ON THE IB SIDE STA 1180REPLACED ANGLE IAW DWG 149N7734May 19, 2020 · N411UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2020022875537Warning Message · false activationINSPECTION TYPE:N/AEMERGENCY DECLARED - TRAILING EDGE FLAP DISAGREE MESSAGE AFTER T/O. ASSOCIATED TRAILING EDGE LIGHT ILLUMINATED. ACCOMPLISHED QRH TRAILING EDGE FLAP DISAGREE PROCEDURE. RETRACTED & EXTENDED LE & TE FLAPS WITH ALTERNATE FLAP SELECTOR.PERFORMEDFeb 26, 2020 · N411UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2020011350866Rotary Actuator · faultyINSPECTION TYPE:N/A**EMERGENCY DECLARED** IN PATTERN AT SDF @ 3000FT AND 210 KNOTS WE SELECTED FLAPS 1 AND GOT LE SLAT DISAGREE EICAS AND LEADING EDGE ANNEMERATOR THE FLAP INDICATOR READ HALFWAY BETWEEN "UP & "1" WE ACCOMPLISHED LE SLAT DISAGREE CHECK LIST ANDJan 10, 2020 · N411UP · Boeing 75724APF · Leading Edge Slat ActuatorSDR IPXA2018051409532Floor Panel · tornINSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 231XJF FOUND TORN. FABRICATED A NEW FLOOR PANEL, AND INSTALLED IAW SREO B757-5320-9692-K.May 2, 2018 · N411UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018051409531Floor Panel · delaminatedINSPECTION TYPE: SEG2, MAIN DECK FLOOR PANEL 231XFF FOUND DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K, AND INSTALLED.May 2, 2018 · N411UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018052189757Skin · dentedINSPECTION TYPE: SEG2,M UPPER MID FUSELAGE EXTERNAL SKIN HAD ONE DENT AT BS 1180 STRINGER 7R. REPAIRED IAW EA 757-5361-27-A2298.Apr 30, 2018 · N411UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2017053117742Smoke Goggles · crackedSUPERNUMERARY SEAT SMOKE GOGGLES CRACKED. REPLACED THE SMOKE GOGGLES.May 25, 2017 · N411UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2016102709939Cable · misroutedINSPECTION TYPE: N/A, EMER DECENT REELS CABLES IMPROPERLY ROUTED BACKWARDS. REROUTED CABLES PER AMM 25-61-02-201.Oct 26, 2016 · N411UP · Boeing 75724APF · Emergency EquipmentSDR IPXA2016052303769Skin · corrodedINSPECTION TYPE:C-17, EXTERNAL FUSELAGE BS 1473 VHF ANTENNA SUPPORT HAS SURFACE CORROSION, MATERIAL THICKNESS DOES NOT MATCH S/O 757-53A0053 REQUIREMENTS, SHOULD BE .063 FOR BOTH -1 AND -4 HAV .080 AND .071 COMPLIED WITH REO-G19929, REV B.May 23, 2016 · N411UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2016052203664Shear Tie · crackedINSPECTION TYPE:C-17, AFT PIT BS 1480, SHEAR TIE CRACKED BETWEEN S-25L AND S-26L. R & R SHEAR TIE IAW SRM 51-40-02.May 17, 2016 · N411UP · Boeing 75724APF · Fuselage Internal Mounting StructureSDR IPXA2016052203673Skin · dentedINSPECTION TYPE:C-17, FUSELAGE SKIN DENT AT BS 1475, BETWEEN STR 25L- 26L. REPAIRED IAW REO-G19910.May 1, 2016 · N411UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR IPXA2015101694858Shaft · looseON LANDING MAIN ENTRY DOOR EICAS MESS AND OVERHEAD LT, CAME ON AND STAYED ON DOOR WAS CLOSED AND LATCHED. TIGHTENED ATTACHING HARDWARE ON HANDLE SHAFT IAW MM 52-12-00, OPS CK OK.Oct 14, 2015 · N411UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2015082892818Bulb · inoperativeINSPECTION TYPE:IN, EMERGENCY LIGHTS "UNARMED" AND HAS ONE BULB OUT. REPLACED THE ANNUNCIATOR. , OK FOR SERVICE.Aug 27, 2015 · N411UP · Boeing 75724APF · Emergency LightingSDR IPXA2015020985675Bulb · inoperativeEMERGENCY LIGHT HAS SIX INOPERATIVE BULBS. REPLACED THE BULBS IAW AMM 33-51-01-2.Feb 6, 2015 · N411UP · Boeing 75724APF · Emergency LightingSDR IPXA2014061183260Frame · dentedC16 INSPECTION, AFT CARGO BAY BS 1560, S26L FRAME DENTED. REPAIRED IAW SRM 53-00-07-2R REPAIR 5, DETAIL II.May 16, 2014 · N411UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2014060683213Frame · dentedC16 INSPECTION, AFT CARGO BAY FRAME BS 1540, STR 25L DENTED. REPAIRED IAW SRM 53-00-07-2R, REPAIR 5, DETAIL II.May 16, 2014 · N411UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2014060683212Stringer · corrodedC16 INSPECTION, AFT CARGO BAY STRINGER 25L BS 1460 IS CORRODED. REPAIRED IAW SRM 53-00-03-2R, REPAIR 1, DETAIL II.May 16, 2014 · N411UP · Boeing 75724APF · Fuselage Main, Longeron/StringerSDR IPXA2014060683200Frame · dentedC16 INSPECTION, AFT CARGO BAY FRAME BS 1280, S26L DENTED. INSTALLED REPAIR IAW SRM 53-00-07-2R, REPAIR 6, DETAIL IV.May 16, 2014 · N411UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2014060483199Frame · dentedC16 INSPECTION, AFT CARGO BAY BS 1460, S26L FRAME DENTED. REPAIRED IAW SRM 53-00-07-2R-5 FIG 201, DETAIL I.May 16, 2014 · N411UP · Boeing 75724APF · Fuselage Main, Frame
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