N146UP

Service difficulty reports · 339

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 = 'N146UP' 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 IPXA2026100240166Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT BTWN FR 56 - 57 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y450 TO -Y963.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240462Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 AT CROSSBEAM -Y1959 HAD A SCREW HOLE WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. AFTER REWORK FOUND WITHIN LIMITS IAW SRM 51-73-11, NEGLIGIBLE DAMAGE, TREATED, PRIMED AND TOPCSep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240510Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 57.1 AT CROSSBEAM -Y1959 HAD A SCREW HOLE CORRODED. REMOVED CORROSION FROM CEILING SUPPORT AT CEILING SUPPORT. RESTORED SURFACE PROTECTION IAW SRM 51-21-10, AND SRM 51-75-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240360Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 58 WITH SPOTS OF CORROSION AT CROSSBEAM -Y450 TO -Y963.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100241134Support Angle · corrodedAFT CARGO COMPARTMENT, SUPPORT ANGLE OF SMOKE DETECTOR BOX AT FR 62, CROSSBEAM Y0 CORRODED. RESTORED SURFACE PROTECTION ON THE AFT CARGO BAY, SUPPORT ANGLE AT FR 62 CROSSBEAM Y0 IAW SRM 51-21-10 AND SRM 51-75-10.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100241943Support · corrodedFWD CARGO FR 38.2, BTWN Y805 AND -Y805 CEILING,LINING SUPPORT HAD FIVE SPOTS OF CORROSION. INSPECTED APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001, AND APPLIED PAINT IAW SRM 51-75-10-201.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100242382Crossbeam · corrodedFWD CARGO FR 38.1, BTWN Y805 AND Y1407, CEILING SUPPORT BRACKET WAS CORRODED. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001 AND APPLIED PAINT IAW SRM 51-75-10-201. NO FURTHER ACTION REQUIRED.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100242390Crossbeam · corrodedFWD CARGO FR 34, BTWN -Y140 AND -Y805, CEILING SUPPORT WAS CORRODED.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100242469Crossbeam · corrodedFWD CARGO FR 34, BTWN Y140 - Y805, CEILING SUPPORT WAS CORRODED. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN Y140 AND Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOUND TO BESep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100240158Support · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR 54.2 WITH SPOTS OF CORROSION FROM CROSSBEAM -Y953 TO -Y1959, CEILING SUPPORT REMOVED AT FR 54.2 FROM CROSSBEAM -Y953 TO -Y1959 AFT CARGO COMPARTMENT IAW IAW A300-600 SRM 51-40-21.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026100240574Crossbeam · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR58 FROM CROSSBEAM -Y450 TO -Y953 HAS A SPOTS WITH CORROSION, PROFILE CROSS T26/1880702 AND LOCATED AND DRILLED PROFILE CROSS IAW SRM 51-40-44-001.Sep 8, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100217405Stiffener · crackedLH WING, FLAP KRUEGER HAS A CRACK UNDERNEATH TEFLON ROLLER BASE , STIFFENER REMOVED AT LH WING, FLAP KRUEGER UNDERNEATH TEFLON ROLLER BASE IAW SRM 51-40-21. INSTALLED NEW STIFFENER TRAVELER #T26/1882425 P/N #A53510288200 IN LH WING FLAP KRUEGER IAW SRM 51-40Sep 6, 2026 · N146UP · Airbus A300F4622R · Wing, Control Surface Attach FittingsSDR IPXA2026100217425Bracket · crackedLH WING, FIXED LEADING EDGE, INSIDE FLAP KRUEGER COMPARTMENT I/B SIDE HAS A BRACKET WITH CRACK (DOT 64-018)Sep 6, 2026 · N146UP · Airbus A300F4622R · Wing, Control Surface Attach FittingsSDR IPXA2026102993107Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 3 CRACKS ON RIB 12 NOTED. ACCOMPLISHED STEP #55E OF E.A.#: 300-5753-27-A4625 REV- PRELIMINARY 4.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993072Skin · crackedLH WING, CENTER FLAP, TOP SKIN RIB FLANGE. 2 EA CRACK NOTED AT RIB 27. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98608 AND STE PNA EA 300-5753-27-A4624, REV-.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993191Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 2 CRACKS ON RIB 25 NOTED. GIVEN OK TO INSTALL FOR STEP 81 (D) OF E.A.#: 300-5753-27-A4625 REV- PRELIMINARY 4 .REF RII UPS GMM 04-02 MAJOR REPAIR .Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993093Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 3 CRACKS ON RIB 11 NOTED. COMPLETED PRELIMINARY 4 STEP #58 (D) OF E.A.#: 300-5753-27-A4625 REV-.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993056Skin · crackedLEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE. 1 EA CRACK NOTED AT RIB 26. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-98608 AND STE PNA EA 300-5753-27-A4624, REV-.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993186Rib · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 1 CRACK ON RIB 15 NOTED. VERIFIED STEP 60D OF E.A.300-5753-27-A4625 REV- PRELIMINARY 4.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993140Rib · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 2 CRACKS ON RIB 13 NOTED AND MARKED IN RED. ACCOMPLISHED STEP #56E OF E.A 300-5753-27-A4625 REV- PRELIMINARY 4.Sep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026102993231Skin · crackedRIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES, FOUND 2 CRACKS ON RIB 26 NOTED AND MARKED IN RED. CONFIRMED ACCOMPLISHED STEP 80 OF E.A.#: 300-5753-27-A4625 REV- PRELIMINARY 4 "REINSTALL HOISTING BRACKET WITH FASTENERS PER DRAWING REQUIREMENTS. IF FASTENER HOSep 4, 2026 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026081072086Lamp · inoperativeEMERGENCY EXIT LIGHT HAS 2 EA LAMPS INOP. RELAMPED 2 EA EMER EXIT LIGHT LAMPS W/REF TO MM 33-51-13 PB 0401. OPS CK GOOD.Aug 7, 2026 · N146UP · Airbus A300F4622R · Emergency LightingSDR IPXA2026052778934Protector · damagedSDF UNLOAD REPORTED DAMAGE TO THE UPPER AFT FRAME PROTECTOR OF NEAR THE MAIN CARGO DOOR. ACCOMPLISHED PERMANENT REPAIR PER SREO-24849-REQ002 STEPS 1-3. THIS CLEARS DEFERRAL MOC 2878903.May 27, 2026 · N146UP · Airbus A300F4622R · Cargo/Baggage DoorsSDR IPXA2026052530789Skin · missingLEFT WING INBOARD SLAT HAS APPROX 8" X 6" SQ AREA OF THE SLAT HAS MISSING SKIN. COMPLETED ALL STEPS OF PRELIMINARY REQ 3 AS REQUIRED. VERIFIED ALL STEPS OF EO-97577REQ5 HAS BEEN COMPLETED. MAJOR REPAIR.May 23, 2026 · N146UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2026061520719Skin · dentedMAJOR REPAIR. FUSELAGE LOWER SKIN DENT AND GOUGE AFT OF TAIL BALL. C/W EO-94154-REQ4 REF BARCODE T3F18E0090DWFApr 15, 2026 · N146UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025051229229Battery · malfunctionedESCAPE SLIDE LIGHTING BATTERY FUNCTIONAL CHECK FAILED CAPACITY CHECK R&R EMERGENCY EVACUATION SLIDE IAW AMM 25-61-21. SLIDE LIGHTING FUNCTIONAL TEST GOOD.May 11, 2025 · N146UP · Airbus A300F4622R · Escape SlideSDR IPXA2025020720940Control Lever · malfunctionedLANDING GEAR DID NOT RETRACT ON DEPARTURE. SWITCHED POSITION DET FROM SYSTEM 1 TO SYSTEM 2. LANDING GEAR RAISED NORMALLY. REPLACED LANDING GEAR CONTROL SWITCH REF AMM 32-31-11, OPS CHECK GOOD. REPLACEMENT PROX UNIT BAD FROM STOCK, ORDERED ANOTHER REPLACEMEN. CFeb 7, 2025 · N146UP · Airbus A300F4622R · Landing Gear SelectorSDR IPXA2023072693741Door · inoperativeFWD CABIN DOOR AUDIO WARNING INOPERATIVE. DEFERRED IAW MEL 52-73-01-2. M810723 ASSIGNED. NO DMPS. PLACARD INSTALLED.FOUND BROKEN WIRE ON WARNING HORN. REPLACED TERMINAL END AND INSTALLED ON WARNING HORN IAW ESPM 20-48-11-01 AND OPS CK IAW AMM 52-73-12 PB 0401.Jul 25, 2023 · N146UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2022102787559Oil System · leakingINSPECTION TYPE:N/AON APPROACH TURNED ENG & WING ANTI-ICE ON. SHORTLY AFTER HAD A FAINT SMELL IN COCKPIT. ON FINAL APPROACH NOTICED A FAINT VISIBLE SMOKE IN COCKPIT OVERHEAD LIGHT. SEEMED TO START TO DISSIPATE AFTER ANTI-ICE OFF.T/S C/O IAW TSM 21-20-00 PG 117Oct 27, 2022 · N146UP · Airbus A300F4622R · APU Oil SystemSDR IPXA2022030279626None · noneINSPECTION TYPE:N/AFUMES WITH OILY SMELL BEING DISCHARGED IN VENTILATION SYSTEM. BOTH PACK OPERATING FROM APU BLEED SMELL IN BOTH COCKPIT AND MAIN CARGO AREASREPLACED BOTH COALESCER BAGS REF AMM 21-51-16 KR #5601439 3-1-22 OPERATED LH ENG REF AMM 71-00-00 STARMar 1, 2022 · N146UP · Airbus A300F4622R · Air Distribution SystemSDR IPXA2022021679063Unknown · odorINSPECTION TYPE:N/ASTRONG ODOR OF BREAD/ YEAST WETSOCKS FROM PACKS WHEN THROTTLES ADCANCED OUT OF IDLE THRUST FOR T/O ODOR REMAINED FOR ENTIRE FLIGHT.SUSPECT DE-ICD FLUID INGESTION LEADING TO UNSATISFACTORY CABIN AIR QUALITY PER A300 FIM 21-20-00 FIG. 210. RANFeb 16, 2022 · N146UP · Airbus A300F4622R · Air Distribution SystemSDR IPXA2021102475274Engine · noneINSPECTION TYPE:N/A**SUPPLEMENTAL SDR **REQUEST DMI TO COMPLY WITH EO 7100-53507 BETWEEN 10-20 FLIGHT CYCLES FOR RH ENGINE AFTER INSTALLATION.COMPLIED WITH EO-M-7100-53507COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760587Oct 23, 2021 · N146UP · Airbus A300F4622R · Powerplant SystemSDR IPXA2021102475273Engine · noneINSPECTION TYPE:N/A**SUPPLEMENTAL SDR**REQUEST DMI TO COMPLY WIT EO M-7100-53507 BETWENN 10 AND 20 FLIGHT CYCLES FOR LH ENG AFTER INSTALL. COMPLIED WITH EO M7100-53507 REF D760586COMPLIED WITH EO M-7100-53507 APPX A. NO LEAKS NOTED. THIS CLEARS M760586Oct 23, 2021 · N146UP · Airbus A300F4622R · Powerplant SystemSDR IPXA2021102475281Strap · crackedINSPECTION TYPE:CDURING CUSTOMER WALK THROUGH FOUND STIFFENER BETWEEN FR85 AND FR86 CRACKEDREMOVED AND REPLACED STIFFENER IAW SRM 51-40-21Oct 23, 2021 · N146UP · Airbus A300F4622R · Fuselage Structure (General)SDR IPXA2021102175183Bracket · brokenINSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.Oct 14, 2021 · N146UP · Airbus A300F4622R · Engine Cowling SystemSDR IPXA2021102175182Bracket · brokenINSPECTION TYPE:A300#2 ENG T/R I/B AND O/B CIRCUMFERENTIAL LATCH UPPER GUIDE BRACKETS ARE BROKEN.REMOVED AND REPLACED BRACKETS IAW SRM 51-40-21.Oct 14, 2021 · N146UP · Airbus A300F4622R · Engine Cowling SystemSDR IPXA2021100974769Flap · noneINSPECTION TYPE:A300RT WING O/B FLAP O/B STATIC WICK BASE DIBONDED. AFTER FURTHER INVESTIGATION FOUND FLAP SKIN WITH CORROSION. MATERIAL REMOVED DOWN TO 0.043' (78%) WITH SOME CORROSION STILL REMAINING.ACCOMPLISHED DOUBLER SKIN REPAIRED PER EA #300-5754-27-A27Oct 9, 2021 · N146UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2021102375250Washer · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 2 PER EA# A300-5710-81939-A , INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2021102375249Washer · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL WASHER 1 PER EA# A300-5710-81939-A , INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2021102375248Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IM MIDDLE HOLE.INSTALL BUSHING PER EA# A300-5710-81939-A, INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2021102375247Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENETER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EA3 A300-5710-81939-A,INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2021102375246Bushing · crackedINSPECTION TYPE:A300ROTO PROBE OF RH FR 40 CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION FOUND DAMAGE IN MIDDLE HOLE.INSTALL BUSHING PER EO# A300-5710-81939-A,INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2021102175186Shim · noneINSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR44 LH SIDE HAS CRACK.REPAIRED PER EO A300-5310-46789-G APPENDIX J INSTALL ONLY.Sep 29, 2021 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2021102175179Doubler · crackedINSPECTION TYPE:A300CENTER FUSELAGE BASE FRAME FITTING AT FR 46 R/H SIDE HAS CRACK.ACCOMPLISHED REPAIR PER EO# A300-5310-46789-G APPENDIX K. INSTALL ONLYSep 29, 2021 · N146UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2021101374922Support · crackedINSPECTION TYPE:CMDC LH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR 61 AND 62 CRACKEDREMOVED FABRICATED AND INSTALLED IAW SRM 51-40-21Sep 29, 2021 · N146UP · Airbus A300F4622R · Cargo CompartmentsSDR IPXA2021101374920Web · crackedINSPECTION TYPE:A300MDC RH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR 38 AND 38.1 CRACKED.REMOVED,FABRICATED,AND INSTALLED IAW SRM 51-40-21.Sep 29, 2021 · N146UP · Airbus A300F4622R · Cargo CompartmentsSDR IPXA2021101374918Support · crackedINSPECTION TYPE:A300MDC RH FLOOR LEVEL ANGLE WEB SUPPORT BTW FR36 AND 37 CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.Sep 29, 2021 · N146UP · Airbus A300F4622R · Cabin Equipment/FurnishingsSDR IPXA2021101374915Bracket · crackedINSPECTION TYPE:A300EXTERNAL LOWER FUSELAGE LH SIDE AR FR45 AFT AIRCON PANEL SUPPORT BRACKET CRACKED.REMOVED AND REPLACED IAW SRM 51-40-21.Sep 29, 2021 · N146UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2021100674646None · crackedINSPECTION TYPE:CMDC RH SIDE FLOOR LEVEL ANGLE WEB SUPPORT BTW FR38.1 AND 38.2 CRACKEDREMOVED AND REPLACED IAW SRM 51-42-21Sep 29, 2021 · N146UP · Airbus A300F4622R · Cargo CompartmentsSDR IPXA2021101374900Floor Panel · damagedINSPECTION TYPE:A300PNL 231LG BROKEN.FABBED IAW SREO A300-5320-40552-B.Sep 28, 2021 · N146UP · Airbus A300F4622R · Standard Practices/Structures
Back to N146UP