N140UP

Service difficulty reports · 341

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 = 'N140UP' 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 IPXA2025080695532Skin · crackedRT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94787-REQ1 AND VT-MAE EA 300-5750-27-A4063, REV. -.Jul 18, 2025 · N140UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025091682895Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 6 FROM LOWER APPEAR TO HAVE GOUGES . 89-830 CLEANED AREA AT FWD CREW DOOR STOPS (FROM FWD FACE OF THE DOOR) # 6, AFTHER FURTHER EVALUATION AND REMOVED DAMAGE, ORIGINAL THICKNESS 0.135", REMOVED THICKNESS 0.003Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025091682988Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 7 FROM LOWER APPEAR TO HAVE GOUGES . 89-831 REMOVED AND REPLACED FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 7 FROM LOWER IAW A300/600 AMM 52-10-31/401.Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025091682897Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 5 FROM LOWER APPEAR TO HAVE GOUGES . 89-829 REMOVED AND REPLACED FWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 5 FROM LOWER IAW A300/600 AMM 52-10-31/401.Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025091683055Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 8 FROM LOWER APPEAR TO HAVE GOUGES . 89-832 REMOVED AND REPLACED ADJUSTABLE BOLT FOR DOOR FITTING IAW A300 AMM 52-10-31/401 STEP 2B(2) AND 2D(2). ADJUSTED FWD PASSENGER/CREW DOORS STOP FITTINGS IAW A300 AMM 52Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025090881604Adapter · corrodedCLS ADAPTER AT FR43 Y0 LH HAS CORROSION. COMPLIED WITH EO-94969-REQ1 AND VT-MAE EA 300-5315-27-A4057 REV.-.Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025090881678Adapter · corrodedCLS ADAPTER AT FR40 Y0 RH HAS CORROSION. .COMPLIED WITH EO-94969-REQ1 AND VT-MAE EA 300-5315-27-A4057 REV.-. CASS FEEDBACK REPORT COMPLETED AND FORWARDED TO CASS@UPS.COM. JOB COMPLETEJul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081681730Adapter · corrodedCLS ADAPTER AT FR38.1 RT OTBD IS BROKEN. COMPLIED WITH REMOVED AND REPLACED CLS ADAPTER IAW PRODUCTION DWR REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTSJul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025090172198Adapter · corrodedCLS ADAPTER AT FR71 IB OF Y1580 HAS CORROSION. REMOVED AND REPLACED CLS ADAPTER IAW PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQUIREMENTS.Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081681753Adapter · brokenCLS ADAPTER AT FR38 LH OB IS BROKEN. COMPLIED WITH REMOVE AND REPLACED 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND SRM CHAPTER 51 REQIREMENTS.Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025082275437Adapter · wornCLS ADAPTER AT FR57.1 Y0 LH HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025082275244Adapter · wornCLS ADAPTER AT FR57.1 Y0 RH HAS CORROSION. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025082275003Adapter · wornADAPTER AT FR56 Y0 RH HAS CORROSION COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025082273957Adapter · wornCLS ADAPTER AT FR54.2 Y0 RH HAS WEAR DOT 5612-15 COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94652-REQ1 AND VT-MAE EA 300-5316-27-A4065 REV. - .Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025082274190Adapter · wornCLS ADAPTER AT FR62 Y0 LH HAS WEAR DOT 5612-16 COMPLIED ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94688-REQ1 AND VT-MAE EA 300-5317-27-A4067 REV. - .Jul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081681965Adapter · brokenCLS ADAPTER AT FR34 RH OB IS BROKEN. COMPLIED WITH REMOVE AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTSJul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025081681917Adapter · brokenCLS ADAPTER AT FR37 RH OB IS BROKEN. COMPLIED WITH REMOVED AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTSJul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025081281580Adapter · crackedCLS ADAPTER AT FR38.1 LH OB IS BROKEN DOT 5612-28 COMPLIED WITH REMOVE AND REPLACE 1(EA) CLS ADAPTER P/N B53774136204 PER PRODUCTION DRAWING REQUIREMENTS AND A300-600F SRM CHAPTER 51 REQUIREMENTSJul 17, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA202507183055Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) # 8 FROM LOWER APPEAR TO HAVE GOUGES . 89-832 APPROVED.Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA202507182988Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 7 FROM LOWER APPEAR TO HAVE GOUGES .Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA202507182897Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 5 FROM LOWER APPEAR TO HAVE GOUGES .Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA202507182895Stop Fitting · gougedFWD CREW DOOR STOP ( FROM FWD FACE OF THE DOOR ) NR 6 FROM LOWER APPEAR TO HAVE GOUGES.Jul 17, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081455436Vertical Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y953 RH IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y953 RH APPLIED IAW A300-600, SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081455420Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y953 LH IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y953 LH APPLIED IAW A300-600, SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081455411Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y-1959 IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y-1959 APPLIED IAW A300-600, SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081455380Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y0 IS CRACKED INSTALLED VERTICAL SUPPORT AT AFT CARGO FR 54 Y 0 APPLIED IAW A300-600, SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080855589Support · corrodedFAULT - STR - Z100 - AFT CARGO FR 54.2 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 IAW A300-600 SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080855568Support · corrodedFAULT - STR - Z100 - AFT CARGO FR 54.2 LH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 L/H. IAW A300-600 SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080855599Support · corrodedFAULT - STR - Z100 - AFT CARGO FR 54.2 RH HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT AT AFT CARGO FR54.2 R/H. IAW A300-600 SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025081555780Support · corrodedAFT CARGO FR 62 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT FASTENER HOLES INSTALLED CEILING SUPPORT ON AFT CARGO FR 62 IAW SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA202508155380Vertical Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y0 IS CRACKED VERIFIED STEP 13 C/W, TASK IS COMPLETEJul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA202508155420Vertical Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y953 LH IS CRACKED VERIFIED STEP14 C/W, TASK IS COMPLETE.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA202508155411Vertical Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y-1959 IS CRACKED VERIFIED STEP 14 C/W, TASK IS COMPLETE.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA202508155436Vertical Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y953 RH IS CRACKED VERIFIED STEP 13 C/W, TASK IS COMPLETE.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080956334Seal · crackedAFT CARGO FR 65 RH DOOR LANDING UPPER CORNER IS CRACKED INSTALLATION OF SECTION CEILING ANGLE SUPPORT. JOB COMPLETE.Jul 16, 2025 · N140UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025081255450Support · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y1959 IS CRACKED.REMOVED SUPPORT AT AFT CARGO FR 54 VERTICAL Y 1959 IAW - SRM 51-40-21.LOCATED AND DRILL SUPPORT AT AFT CARGO FR54 Y 1959 IAW SRM 51-40-21.INSTALED NEW PART P/N: A5341076522200 IAW SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080655454Support · corrodedAFT CARGO FR 54 CENTER HORIZONTAL CEILING SUPPORT IS CORRODED AT ATTACHING POINT. INSTALLED EXTRUSION SUPPORT STRUCTURE AT THE FR54 IN THE AFT CARGO PIT IAW SRM 51-40-21-001. REVIEWEDJul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025080755399Angle · crackedAFT CARGO FR 54 VERTICAL SUPPORT AT Y-953 IS CRACKED. INSTALED NEW PART IAW SRM 51-40-21.Jul 16, 2025 · N140UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025082823227Skin · dentedMAJOR REPAIR, LEFT SIDE FUSELAGE SKIN DENT REPAIR BETWEEN FR0-FR1 REQUIRES PERMANENT REPAIR. COMPLIED WITH ACCOMPLISH PERMANENT REPAIR IAW EO-79250-REQ1 AND VT-MAE EA 300-5311-27-A4048, REV. -.Jul 14, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025081650158Skin · dentedMAJOR REPAIR, DENT WITH GAUGE FWD OF TAIL STAND ON RIGHT HAND SIDE. ACCOMPLISHED REPAIR DAMAGE IAW SRM 53-10-12-201, PARAGRAPH 11 AND FIGURE 208 (SHEET 1).Jun 21, 2025 · N140UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA2025031178271Indication Sys · faultedREF. MEL 52-11-01-2-4. MAIN ENTRY DOOR/SLIDE INOP "CREW SIGN OFF" VERIFIED MAIN ENTRY DOOR (L1) CLOSED, AND LOCKED. MEL/ DMP 52-11-01-2-4.Mar 11, 2025 · N140UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025031175551Indication Sys · faultedAFTER DIS-ARMING CABIN DOOR AND PUSHING TEST BUTTON. DOOR SHOWS DISARMED UNTIL THE DOOR IS OPENED. WARNING IS CONTINUOUS. DOOR SHOWS SLIDE ARMED AFTER OPENING DOOR.SLIDE DIDN€™T DEPLOY INSTALLED NEW SLIDE W/REF TO AMM 25-61-21/401. OPS NORMAL.Mar 11, 2025 · N140UP · Airbus A300F4622R · Door Warning SystemSDR IPXA2025012405142Window · fireDURING CLIMBOUT NOTICED/HEARD A WHEEZING NOISE: FOLLOWED BY ARCING-SMALL FLAMES IN LOWER CORNER OF FO€™SWINDOW: A CRACK FROM THAT CORNER TO MIDWAY DEVELOPED- AFTER LEVELING OFF AT 14,000 THE CRACK DOUB ACCOMPLISHED AMM 56-11-11/401 F, ATBJan 21, 2025 · N140UP · Airbus A300F4622R · Flight Compartment WindowsSDR IPXA2024072949044Floor Panel · damagedHOLE FOUND IN MAIN CARGO FLOOR AT 4R. REMOVED THE NO-SLIP MATERIAL FROM THE SURFACE OF THE FLOOR PANEL. SECURED THE LOWER PATCH WITH EPOXY ADHESIVE IN THE HOLE LOCATEDIN THE LOWER SKIN PER A300-600F SRM 51-77-10-201Jul 28, 2024 · N140UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2023092094209Sign · inoperativeINSPECTION TYPE:NACREW DOOR EXIT SIGN EMERGENCY LIGHT INOP OPENED SAFETIED AND TAGGED CIRCUIT BREAKERS E28M 22VU AND P80 M 132VU FOR REMOVAL / INSTALLATION OF EXIT MODULE REF AMM 33-51-13-0401REMOVED AND REPLACED DOOR EXIT SIGN MODULE PER A300 AMM 33-51-13-040Sep 20, 2023 · N140UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023090794102Cover · looseL1 DOOR SLIDE PACK COVER LOOSE. REMOVED SLIDE, SLIDE COVER, & GIRT BAR IAW AMM 25 61 21. REMOVED & REPLACED L1 DOOR ESCAPE SLIDE IAW AMM 25-61-21.Sep 7, 2023 · N140UP · Airbus A300F4622R · Escape SlideSDR IPXA2023051693242Panel · inoperativeINSPECTION TYPE:NAEMER EXT LT PANEL ABOVE CREW ENTRY DOOR IS FALLING OFF.RESECURED EMERGENCY EXIT LT PANEL IN REF TO AMM 33-50-00.May 16, 2023 · N140UP · Airbus A300F4622R · Emergency LightingSDR IPXA2023031691901Damper · unserviceableINSPECTION TYPE:N/A*MAJOR REPAIR* EMERGENCY DOOR DAMPNER WILL NOT HOLD PRESSUEREMOVED AND REPLACE WITH SERVICEABLE UNIT AMM 52-10-14-0401Mar 15, 2023 · N140UP · Airbus A300F4622R · Emergency ExitsSDR IPXA2023020490607Fitting · crackedINSPECTION TYPE:CK1CCRACK INDICATION AT FR47 UPPER RADIUS 3MMREPEAT INSPECTIONS AT 1400 FC INTERVALS PER EO A300-5310-18290-RFeb 4, 2023 · N140UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2023020490604Fitting · corrodedINSPECTION TYPE:CK1CHOLE 5 CORROSION INDICATION IN FR22A FORK FITTINGREPAIRED PER EA 300-5231-27-A3131Feb 4, 2023 · N140UP · Airbus A300F4622R · Cargo/Baggage Doors
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