N461UP

Service difficulty reports · 326

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 = 'N461UP' 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 IPXA2024091245563Cover · damaged**SDR FILED OPEN** CAPT EVAS SPLASH GUARD COVER MISSING PART ON ORDER ZERO STOCK M-25-021-101Sep 11, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024091245662Cover · damaged**SDR FILED OPEN** F/O EVAS SPLASH GUARD COVER MISSING PART ON ORDER ZERO STOCK M-25-021-101.Sep 11, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024081487080Skin · corrodedNR 1 I/B FWD PYLON SKIN HAS CORROSION AT INTERNAL AND EXTERNAL SURFACE. JOB HAS BEEN ACCOMPLISHED PER UPS EO-91010-REQ1 AND VT MAE EA 757-5450-27-A3658 REV- WITHOUT ANY DEVIATIONS.Jul 24, 2024 · N461UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024080337732Angle · corrodedFAULT-STR ZONE 165 BODY AFT BULK CARGO COMPARTMENT ANGLE PLATE BETWEEN STA 1680 AND 1720 IS DELAMINATED AND HAS CORROSION. DOT 75-001.REMOVED FLOOR PANEL 252XUF AT MAIN CABIN TO F.O.M. I.A.W. SRM 51-40-02-0G.REMOVED ANGLE PLATE AT BODY BULK CARGO COMPARTMENT IJul 21, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080321068Structure · corrodedMID FUS - WTB STRUCTURE STA 1220 RH SIDE HAS CORROSION.EVALUATED T-CHORD FROM STA 1220 RH TO 1240 RH FOUND EXFOLIATION THEREFORE OUT LIMITS I.A.W SRM 53-00-71-1A-1 DETAIL IX. AND REMOVED T-CHORD I.A.W SRM 51-40-02-0G. RESTORED SURFACE PROTECTION I.A.W. SRM 51-Jul 20, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080218851Floor Support · corrodedMAIN CARGO CORROSION UNDER FLOOR PANEL 241XAF AFT AREA. INSTALLED NEW UPPER CHORD IAW B757 SRM 51-40-02.Jul 20, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080218877Floor Support · corrodedMAIN CABIN CORROSION UNDER FLOOR PANEL 241XFF AFT AREA.REMOVED 01 NUT DOME IAW SRM 51-40-02-0G, CLEAN AREA AND REMOVED CORROSION IAW SRM 51-10-02, AFTER EVALUATION T-CHORD FOUND TO BE OUT OF LIMITS IAW SRM53-00-51-1A-1 DETAIL III, MEASUREMENTS: ORIGINAL THICKNJul 20, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080318949Tee Fitting · corrodedFAULT: STR Z200, MAIN CABIN CORROSION UNDERFLOOR PANEL 242XDF AFT AREA INSTALLED UPPER CHORD IN MAIN CABIN UNDER FLOOR PANEL 242XDF AFT AREA, IAW 757-200PF SRM 53-00-51-2R-2. REVIEWED.Jul 20, 2024 · N461UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024081089013Tee Angle · corrodedWTB STRUCTURE T-CHORD STA 1180 HAS CORROSION FROM RBL 0 TO RBL 60.AFTER FURTHER INVESTIGATION T-CHORD STA 1180 FROM RBL 0 TO RBL 60 FOUND 100% MATERIAL LOSS BY CORROSION THEREFORE IT'S OUT LIMITS IAW B757 SRM 53-00-71-1A-1, AND REMOVED T-CHORD IAW B757 SRM 51-Jul 18, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080389031Tee Angle · corrodedFAULT: STR Z100, MID FUS - WTB STRUCTURE T-CHORD FROM STA 1180 TO 1240 RBL 60 HAS CORROSION INSTALLED T-CHORD FROM STA1180 TO 1240 RBL 60, RIVET P/N:BACR15FT6D5C BATCH:004298336, HI-LOK P/N:BACB30NX6K6 BATCH:0004288696, BACB30NX6K4 BATCH:0004286459, WASHER P/NJul 18, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080286954Tee Angle · corrodedFAULT: STR Z100, MID FUS -T-CHORD STA 900 HAS CORROSION AT RBL 10 INSTALLED T-CHORD MID FUS STA 900, IAW B757 SRM 51-40-02 AND SRM 51-70-12. MATERIAL USED: SOLID RIVETS P/N BACR15FT6KE10C BATCH NO: 0004254774, P/N BACB30NX6K6 BATCH NO: 0004288696, P/N BACC30M6Jul 18, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080386951Tee Fitting · corrodedFAULT: STR Z100, MID FUS -T-CHORD STA 1037 TO 1060 LH SIDE HAS CORROSION INSTALLED NEW T-CHORD IN STA 1037 TO 1060 LH IAW SRM 51-40-02 RIVET P/N BACR15FT6D7C BTCH: 0004201930 FASTENERS P/N BACB30MY6K5X BTCH: 0004279034 COLLAR P/N: BACC30M6 BTCH: 0004295539, PEJul 18, 2024 · N461UP · Boeing 75724APF · Fuselage Main, Attach FittingsSDR IPXA2024083060457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. COMPLETED REPAIR IAW EO-90940-REQ 1 AND EA 757-5450-27-A3651. REPAIRED #2 I/B SKIN IAW EO-90940 REQ1 & EA 757-5450-27-A3651A REV -. AUDIT COMPLETE.Jul 17, 2024 · N461UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024081860457Skin · corrodedNR 2 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION. DOT 8-006 AND IN RED. VERIFIED PARTS. OPENJul 17, 2024 · N461UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024081260701Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE FWD HINGE PANEL HAS EXFOLIATION CORROSION, DOT 8-004. AUDIT COMPLETE. OPENJul 17, 2024 · N461UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024081760669Skin · corrodedNR 1 ENGINE INBD PYLON INNER SKIN AFT OF THE SQUARE PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-003. ACCOMPLISHMENT OF E.O. AS PER UPS EO-90941-REQ1 AND VT-MAE EA 757-5450-27-A3650, REV. -. WITHOUT ANY DEVIATIONS.Jul 17, 2024 · N461UP · Boeing 75724APF · Nacelle/Pylon, Plate/SkinSDR IPXA2024081259225Stiffener · corrodedFAULT: STR Z600, RH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED.REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.INSTALLED NEW STIFFENER AND ATTACHING PARTS WITH FASTENERS PN: BACB30NY6K11, BT: 0004279074; BACB30NJul 17, 2024 · N461UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA2024080359746Tee Angle · corrodedWTB T-CHORD AT STA 1240 HAS CORROSION AT RBL 15. REMOVED CORROSION. AFTER EVALUATION AND LIMIT VERIFICATION THE WTB T-CHORD AT STA 1240 IS EXFOLIATED, OUT OF LIMITS. IAW SRM 53-00-71.RESTORED SURFACE PROTECCION T-CHORD AND SPLICES IAW SRM 51-20-01-0G-0Jul 17, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080359714Tee Angle · corrodedWTB T-CHORD BETWEEN STA 1180 TO 1240 RH SIDE HAS CORROSION (RAT AREA) REMOVED AND INSTALLED T-CHORD FROM STA1180 TO STA1240 B757 SRM 51-04-02-0G.Jul 17, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080359737Tee Angle · corrodedWTB T-CHORD AT STA 1200 RH SIDE HAS CORROSION AT WL 160.REMOVED T-CHORD AT STA 1200 RH SIDE, WL 160 IAW B757 SRM 51-40-02-0G.INSTALLED NEW T-CHORD AT STA 1200 RH IAW SRM 51-40-02-0G,Jul 17, 2024 · N461UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2024080159861Latch · inoperativeLOWER DOOR LATCH CAM GOUGED. DOT 59-003.BLENDED OUT GOUGE IAW SRM 51-10-02 ACCOMPLISHED STEP 1 SREO-14721-REQ001, T3F18E004V538.Jul 17, 2024 · N461UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024080159841Latch · inoperativeUPPER DOOR LATCH CAM GOUGED. DOT 59-002.BLENDED OUT GOUGE IN UPPER DOOR LATCH IAW SRM 51-10-02, ACCOMPLISHED STEP 1 SREO-14721-REQ001, T3F18E004V50.Jul 17, 2024 · N461UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024072259225Stiffener · corrodedRH WING - T/E STIFFENER PN: 113N1184-4 EXFOLIATED REF STEP 2. INSPECTED AND VERIFIED REMOVED STIFFENER EXFOLIATED P/N 113N1184-4 FROM RH WING TRAILING EDGE IAW SRM 51-40-02-0G-0.Jul 17, 2024 · N461UP · Boeing 75724APF · Wing Miscellaneous StructureSDR IPXA2024071859861Latch · gougedZONE 800 LOWER DOOR LATCH CAM GOUGED. DOT 59-003 APPROVED.Jul 17, 2024 · N461UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024071859841Latch · gougedSTR ZONE 800 UPPER DOOR LATCH CAM GOUGED. DOT 59-002 APPROVED.Jul 17, 2024 · N461UP · Boeing 75724APF · Passenger/Crew DoorsSDR IPXA2024011810140Door · warning lightON PREFLIGHT OBSERVED TWO IDENTATIONS IN THE FUSELAGE SKIN ABOVE THE COCKPIT ENTRY DOOR PER SRM 51-10-01-0G-0 SHEET 1 STA 309.5 & 311.0 0N STRINGER S2 LT SIDE. AERODYNAMIC SMOOTHNESS WITHIN ABOVE MENTIONED LIMITS. ACFT OK TO CONTINUE SERVICEJan 18, 2024 · N461UP · Boeing 75724APF · Fixed Inner DoorsSDR IPXA2023041492874Flap · unknownINSPECTION TYPE:NA*EMERGENCY DECLARED* TE FLAP ASYMPERFORMED FSEU BITE TEST PER FIM 27-51-00-815-805 STEP 1-33. FOUND CURRENT FAULT MSG LT FLAP XMTR WIRE ON FSEU1. T/S USING FSEU TESTS AND FOUND LH TE FLAP POS XMTR OUT OF ADJUSTMENT. ADJUSTED IAW AMM 27-58-01-Apr 14, 2023 · N461UP · Boeing 75724APF · Trailing Edge Flap Control SystemSDR IPXA2023010489582Warning Message · illuminatedAIR TURN BACK AFTER DEPARTURE, GOT STAB TRIM FOLLOWED BY MACH/SPD TRIM EICAS AUTOPILOT DISCONNECTED AND AIRPLANE PITCHED NOSE OVER.BRKERS STB TRM CONT RT POS P11 H20 POPPED & RST MACH/SPD TRM EICAS ADVISRY MSG GNE. DMP 27-41-2 RT STCM RT A/P CH INOP. 22-02-00Jan 1, 2023 · N461UP · Boeing 75724APF · Stabilizer Control SystemSDR IPXA2022071284113Skin · corrodedINSPECTION TYPE:SEG1#2 PYLON IB FWD SKIN PANEL (P/N: 311N5193-1) HAS CORROSION DAMAGE EXCEEDING 50% MATERIAL THICKNESS ON THE INSIDE OF THE FWD SKINACCOMPLISHED SKIN REPLACEMENT PER RCD 274051, BOEING DWG 311N5002, 757-200PF SRM 51-40-02-0GJul 1, 2022 · N461UP · Boeing 75724APF · Nacelle/Pylon, Main FrameSDR IPXA2022071284111Panel · dentedINSPECTION TYPE:SEG1DURING HIDDEN DAMAGE INSPECTION, FOUND TWO DENTS/POINTS OF IMPACT WITH A SCISSOR LIFTREPAIRED PANEL IAW B757 SRM 51-70-10-2R REPAIR 4 PER SRM 55-10-01-1A-1Jul 1, 2022 · N461UP · Boeing 75724APF · Horizontal Stabilizer StructureSDR IPXA2022071284089Torque Box · delaminatedINSPECTION TYPE:SEG1THE LOWER FWD TORQUE BOX PANEL ON THE L/H SIDE, HAS A DISBONDED DENT BY FSS 270.784REPAIRED PANEL IAW B757 SRM 51-70-10-2R REPAIR 2 PER SRM 55-30-01-2R-5Jul 1, 2022 · N461UP · Boeing 75724APF · Vertical StabilizerSDR IPXA2022071284112Skin · dentedINSPECTION TYPE:SEG1RH FUSELAGE SKIN FROM STA 1540-1580, S-28R TO S-29R HAS DENT FOUND TO BE OUT OF LIMITSACCOMPLISHED REPAIR IAW SRM 53-00-01-2R-29, PER SRM 53-60-01-2RJun 29, 2022 · N461UP · Boeing 75724APF · Fuselage Main, StructureSDR IPXA2022022579415None · activatedINSPECTION TYPE:NA**ATB** **EMERGENCY DECLARED** **LANDED UNEVENTFULLY** AT ROTATION FROM SDQ RW 35 THE FIRE BELL ACTIVATED WITH NO EICAS MSG OR RED HANDLE. IMPOSSIBLE TO SILENCER/R MODULES-WARNING ELECTRONIC UNIT (WEU) CARDS M619- M999- M1000 IAW AMM 31-51-04Feb 25, 2022 · N461UP · Boeing 75724APF · Detection SystemSDR IPXA2020082879545Sensor · out of adjustAIR TURN BACK AFTER TAKEOFF GOT STATUS MESSAGE NOSE A/G DISAGREE. NO EMERGENCY WAS DECLARED. FOUND THE LT NOSE LANDING GEAR NOT COMPRESSED, SENSOR OUT OF ADJUSTMENT. ADJUSTED LT NOSE LANDING GEAR NOT COMPRESSED SENSOR AS REQUIRED AND RETESTED SENSORS IAW AMMAug 26, 2020 · N461UP · Boeing 75724APF · Landing Gear Position and WarningSDR IPXA2020081749061Skin · crackedINSPECTION TYPE:SEG, CREASE FOUND WITH CRACK INDICATIONS ON RT SIDE OF TAILCONE AFT OF ELEVATOR. REPAIRED AREA IAW B757 SRM 51-70-10-2R-2 PER SRM 53-80-01-2R FIG 201Aug 14, 2020 · N461UP · Boeing 75724APF · Aerodynamic FairingsSDR IPXA2020060556194Unknown · odorINSPECTION TYPE:N/A STRONG FISH SMELL RETURNED WHILE ON DESCENT INTO PHL. CLEANED SOURCE OF ODOR PER AMM 25-00-00-701.Jun 4, 2020 · N461UP · Boeing 75724APF · Air Distribution SystemSDR IPXA2018081732917Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XCF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732916Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XBF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732915Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SERO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732914Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 221XCF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SERO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732913Floor Panel · damagedMAIN CARGO FLOOR PANEL 221XBF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9596-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732912Floor Panel · damagedMAIN CARGO FLOOR PANEL 221XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5310-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732927Floor Panel · damagedMAIN CARGO FLOOR PANEL 232XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732926Floor Panel · damagedMAIN CARGO FLOOR PANEL 222XCF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732925Floor Panel · damagedMAIN CARGO FLOOR PANEL 222XBF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732924Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XFF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732923Floor Panel · damagedMAIN CARGO FLOOR PANEL 222XAF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-KAug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732922Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XJF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-KAug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732921Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XHF WAS DAMAGED. FABRICATED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2018081732920Floor Panel · damagedMAIN CARGO FLOOR PANEL 231XGF WAS DAMAGED. FABRICTED A NEW FLOOR PANEL IAW SREO B757-5320-9692-K.Aug 17, 2018 · N461UP · Boeing 75724APF · Fuselage Floor Panel
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