N129UP

Service difficulty reports · 253

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 = 'N129UP' 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 IPXA2026091912039Cover · detachedCREW DOOR UPPER HANDLE COVER FELL OFF. INSTALLED CREW DOOR UPPER HANDLE COVER IAW AMM 52-11-11-27 THIS CLEARS DEFERRAL AND PLACARD REMOVEDSep 18, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026042808251Door · leakingSQUEALING NOISE FROM MAIN ENTRY DOOR WHEN PRESSURIZED. INSTALLED INNER DOOR HANDLE AND LINING PER MM 52-11-21.Apr 21, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2026042208251Shaft · looseSQUEALING NOISE FROM MAIN ENTRY DOOR WHEN PRESSURIZED. TIGHTENED MOUNTING HARDWARE FOR LOCKING SHAFT BLOCK, NOTED SLIGHT CHANGE IN SQUEALING SOUND IAW AMM 52-11-21.Apr 21, 2026 · N129UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025111955197Door · corrodedLAVATORY SERVICING PANEL ACCESS DOOR OPEN / CLOSE LATCH FROM CTR EXTERNAL FOUND DAMAGED ( UN SERVICEABLE ) LAVATORY SERVICE DOOR REMOVED IAW A300-600 SRM 51-40-21.FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS (DOUBLER AND SHIM) IAW A300-600 SRM 52-42-11/FINov 13, 2025 · N129UP · Airbus A300F4622R · Fluid Service DoorsSDR IPXA2025111053801Floorbeam · corrodedBULK CARGO PIT FR.#66 STRUCTURAL BEAM UNDER LH FLOOR PANEL #161GF HEAVY CORROSION. INSTALLED NUTPLATES AND CROSSBEAM IAW SRM 51-40-21.Nov 7, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025110746890Doubler · corrodedLAVATORY SERVICE PANEL 121DL BLANKING PLUG REINFORCEMENT DOUBLER IS CORRODED. REMOVED AND REPLACED BLANKING PLUG AT LAV SERVICE PANEL 121DL IAW SRM 51-40-21.Nov 6, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025103113680Floor Panel · damagedFLOOR PANEL 132AH IS BROKEN IN HALF. FLOOR PANEL 132AH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)). REVIEWEDOct 29, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025103171956Floor Panel · damagedMCD FLOOR PANEL 221EG IS BROKEN. FLOOR PANEL 221EG FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT MAIN CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).Oct 27, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025110149647Plate · crackedLEFT WING CENTER FLAP, METALIC PLATE ON TOP SURFACE LE SIDE HAS GOUGING AND SHOWS EVIDENCE OF A CRACK. REMOVED AND REMPLACED METALIC PLATE ON TOP SURFACE LE SIDE IAW SRM 51-40-21.Oct 19, 2025 · N129UP · Airbus A300F4622R · Wing Main, Frame StructureSDR IPXA2025111813903Frame · crackedAIR CONDITION BAY, FR 46RH, BASE FRAME FITTINGS HAS A CRACK. VERIFIED ACCOMPLISHED REPAIR IAW EO-46789-JIC008 REV1. BASE FRAME FITTING FR 46 R/H STRG 35.Oct 17, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2025111412206Support Fitting · crackedHORIZONTAL STAB, 2EA CRACKED BRACKETS ATTACHMENT FOR RH UPPER THS TO FUSELAGE FAIRING. DOT NO. 17-55. INSTALLED 2 EA BRACKETS AT RH UPPER THS TO FUSELAGE FAIRING IAW SRM 51-40-21.Oct 17, 2025 · N129UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2025111112361Bracket · crackedCRACKED BRACKET ATTACHMENT FOR LH UPPER THS TO FUSELAGE FAIRING FWD AREA. DOT NO. 17-57. INSTALLED BRAKET SUPPORT P/N: A5517155320451 AT L/H UPPER THS TO FUSELAGE FAIRING IAW A300-600 SRM 51-40-40 IAW A300-600 SRM 51-40-21.Oct 17, 2025 · N129UP · Airbus A300F4622R · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2025110405938Profile · brokenLEFT FRAME 82 THE CORNER ANGLE IS BROKEN. REMOVED PROFILE -T P/N: A53981401200 AT ZONE 200 L/H FR 82 I.A.W. A300-600 SRM 51-40-21. INSTALLED NEW PROFILE Z AT LH FR 82 IAW A300 SRM 51-40 21.Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025103198494Floor Panel · damagedUPPER MAIN CARGO FLOOR PANEL 232KH DELAMINATED AND BROKEN . FLOOR PANEL 232KH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C).Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025103195901Floor Panel · damagedUPPER MAIN CARGO FLOOR PANEL 222EG DAMAGED AND DELAMINATED. FLOOR PANEL 222EG FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C).Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025103198283Floor Panel · damagedUPPER MAIN CARGO FLOOR PANEL 231KH DAMAGED AND BROKEN . FLOOR PANEL 231KH FAB COMPLETED IAW SREO-16407-REQ002 ((APPX C) CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025103195609Floor Panel · brokenUPPER MAIN CARGO FLOOR PANEL # 222DG BROKEN . 89-1589. LOORBOARD PANEL 222DG FAB COMPLETED IAW SREO-16407-REQ002 ,APPX C A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION.Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025102805909Profile · brokenFAULT/STR/ZONE 200 R/H FR 82 THE CORNER ANGLE IS BROKEN. REMOVED PROFILE -T R/H FR 82 I.A.W. SRM 51-40-21. INSTALLED NEW PROFILE-T AT ZONE 200 R/H FR 82 I.A.W. A300-600 SRM 51-40-21.Oct 16, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025111380204Seat Track · corrodedMAIN DECK SEAT TRACK AT FR79/FR80, Y0 HAS CORROSION. INSTALLED SEAT TRACK AT Y '0' FR 79 TO FR 80 USING FASTNERS PN HL10VF8-6 B# 0004989789, NSA5075-8 38 EACH B# 0004145036, HL12-6-6 B# 0004304262 16 EACH, HL10VF6-5 B# 0004426225 6 EACH, NSA5075-6 B# 00042919Oct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025110470051Skin · crackedRH WING, UPPER SURFACE, CLOSE TO RIB 18, REAR SPAR, SKIN HAS A CRACK DOT 103-51. REMOVED RIVETS AND BOLTS AFFECTED BY THE REPAIR ON RH WING UPPER SURFACE CLOSE TO RIB 18 REAR SPAR IAW A300-600F SRM 57-51-12. INSTALLED BUTTSTRAP, PACKING STRIP, REINFORCEMENT PLOct 15, 2025 · N129UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025110570051Skin · crackedRIGHT WING, UPPER SURFACE, CLOSE TO RIB 18, REAR SPAR, SKIN HAS A CRACK.Oct 15, 2025 · N129UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2025110382369Floorbeam · bentMAIN DECK FLOOR STRUCTURE- CROSSBEAM BENT AT FR48 BETWEEN -Y450 AND -Y953, VERIFIED CROSSBEAM REPLACED ON SREO. COMPLIED WITH SREO-75878-REQ001.Oct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025102882408Floorbeam · crackedFAULT - STR - Z241 -MAIN DECK FLOOR STRUCTURE- CROSSBEAM CRACKED (BUCKLING) AT FR51 BETWEEN -Y450 AND -Y953, DOT 78-20. ACCOMPLISHED WITH SREO-75878-REQ001. REVIEWEDOct 15, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR IPXA2025103054985Support · crackedLH WING FIXED LEADING EDGE SUPPORT CRACKED AT LWR CORNER INSIDE ACCESS PANEL 524GB, INSTALLED PLATE P\N: R5724018520000 BATCH: 0004437520, LH WING FIXED LEADING EDGE SUPPORT IAW A300-600 SRM 57-41-11 PAGE 211 FIGURE 202 (SHEET 2) AND SRM 51-40-21.Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2025110362365Web · gougedLEFT WING T/E REAR SPAR UNDER #5 SPOILER O/B SUPPORT WEB GOUGED, REMOVED CRACKED SUPPORT WEB IAW A300-600 SRM 51-40-21. INSTALLED NEW SUPPORT WEB IAW A300-600 SRM 51-40-21.Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2025103146907Rib · crackedRH WING T/E UPPER SKIN CHANNEL BELOW THE NO.3 SPOILER I/B HINGE IS CRACKED. DOT NO. 17-22. INSTALLED WEB IAW A300-600 SRM 51-40-21.Oct 14, 2025 · N129UP · Airbus A300F4622R · Wing, Rib/BulkheadSDR IPXA2025111826351Floor Support · corrodedBULK CARGO RH FLOOR BRACKET HAS CORROSION. DOT 28-1180. INSTALLED NEW FLOOR BRACKET IAW SRM 51-40-21.Oct 12, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025102913554Bracket · crackedNLG WW LH WHEEL GUIDE STRUT UPPER ATTACHED SUPPORT MOUNT IS CRACKED, DOT 55-033. INSTALLED NEW BRACKET-GUIDE STRUT NLG IAW A300-600 SRM 51-40-21. REVIEWEDOct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025102812902Floor Support · crackedFAULT-Z120-STR-FLOOR STRUCTURE SUPPORT ANGLES CRACKED L/H, @ FR.38 FWD CARGO JUST BELOW MAIN DECK FLOOR. DOT 85/1095. REMOVED CRACKED SUPPORT ANGLE L/H AT FR.38 I.A.W. A300-600 SRM 51-40-21. ++INSTALLED NEW SUPPORT IAW A300-600 SRM 51-40-21.Oct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025102812925Floor Support · crackedFAULT-Z120-STR-FLOOR STRUCTURE SUPPORT ANGLES CRACKED R/H, @ FR.38 FWD CARGO JUST BELOW MAIN DECK FLOOR. DOT 85/1096. REMOVED SUPPORT ANGLE R/H AT FR.38 I.A.W. A300-600 SRM 51-40-21. ++INSTALLED NEW SUPPORT IAW A300-600 SRM 51-40-21.Oct 11, 2025 · N129UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2025111295291Adapter · corrodedMDC CLS ADAPTER AT FR26 Y0 RT IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR26 Y0 RH IAW A300-600 SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110895377Adapter · corrodedMAJOR REPAIR - MDC CLS ADAPTER AT FR65 Y0 LH IS CORRODED. ACCOMPLISHED STEP # 9 E.A#: 300-5317-27-A4193 PRELIMINARY 1: "RESTORE SURFACE PROTECTION AND PAINT SCHEME ACCORDING TO SRM 51-23-10 AND 51-75-10.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025111394837Rib · crackedMAJOR REPAIR, LEFT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 15. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-95517-REQ1 AND VT-MAE EA 300-5750-27-A4185, REV -.Oct 10, 2025 · N129UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025111295293Adapter · corrodedMDC CLS ADAPTER AT FR27 Y0 LH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR27 Y0 LH IAW SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025111295254Adapter · corrodedMDC CLS ADAPTER AT FR26 Y0 LH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR26 Y0 LH IAW SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025111295296Adapter · corrodedMDC CLS ADAPTER AT FR27 Y0 RH IS CORRODED. INSTALLED CLS ADAPTER AND FLOOR STRUCTURE AT FR27 Y0 RH IAW A300-600 SRM 51-40-21-001, SRM 51-75-10-201 SRM 51-76-00-001.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110895397Adapter · corrodedMAJOR REPAIR - MDC CLS ADAPTER AT FR38.2 Y0 LH IS CORRODED. COMPLIED WITH EO-95476-REQ1 AND EA300-5314-27-A418.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110995367Adapter · corrodedMAJOR REPAIR - MDC CLS ADAPTER AT FR38.2 Y0 RH IS CORRODED.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110895344Adapter · corrodedMAJOR REPAIR - MDC CLS ADAPTER AT FR30 Y0 LT IS CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-95477-REQ1 AND VT-MAE EA 300-5314-27-A4191 REV - .Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110895440Adapter · corrodedMAJOR REPAIR - MDC CLS ADAPTER AT FR61 Y0 RT IS CORRODED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-95478-REQ1 AND VT-MAE EA 300-5317-27-A4192 REV -. .Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025103193086Skin · dentedRIGHT WING INBD FLAP HAS A DENT ON OTBD TOP SKIN. ACCOMPLISHED IAW EO-95578-REQ1 REV. 2 AND VT-MAE EA 300-5751-27-A4197, REV -.Oct 10, 2025 · N129UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2025111094874Angle · crackedNR 2 ENG PYLON UPPER, ANGLE UNDER 423AL IS CRACKED IN TWO LOCATIONS, ACROSS BOLT HOLE AND FWD OF BOLTS. DOT #85/1018 CERTIFIED. REMOVED STRUCTURAL BEAM I.A.W. SRM 51-40-21.FABRICATED, LOCATED AND DRILLED NEW CROSSBEAM IAW A300-600 SRM 51-31-00 AND DWR# A53974Oct 10, 2025 · N129UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2025110895368Adapter · corrodedMDC CLS ADAPTER AT FR38.1 Y0 LH IS CORRODED. COMPLIED WITH UPS EO-95474-REQ1 AND VTMAE EA300-5314-27-A4189.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110895352Adapter · corrodedCLS ADAPTER AT FR33 Y0 LH IS CORRODED. COMPLIED WITH EO-95473-REQ1 AND VTMAE EA300-5314-27-A4190.Oct 10, 2025 · N129UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2025110373140Roller · excess playROLLER UPPER REW DOOR FWD HAS AXIAL PLAY. REPLACED BEARING AND SPACE , ROLLER UPPER DOOR FWD IAW A300 SRM 51-40-21.Oct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025110373123Roller · excess playCREW DOOR ROLLER AFT SIDE HAS AXIAL PLAY DOR ALEX-04. REPLACED ROLLER ,CREW DOOR AFT SIDE IAW A300 SRM 51-40-21.Oct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew DoorsSDR IPXA2025101881185Floor Panel · damagedFAULT-MXP-531625-01-1-153-JIC-INT-152KG FLOOR PANEL IS DAMAGED. FLOOR PANEL 152KG FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C).Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025101881141Floor Panel · damagedFAULT- MXP-531625-01-1-153-JIC-INT- 151UF FLOOR PANEL IS DAMAGED. FLOOR PANEL 151UF FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C).Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2025101881096Floor Panel · damagedFAULT-MXP-531625-01-1-153-JIC-INT-151KG FLOOR PLANEL IS DAMAGED. FLOOR PANEL 151KG FABRICATION IS COMPLETE IAW SREO-16407-REQ002 ((APPX C).Oct 9, 2025 · N129UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA72672Panel · brokenFWD CREW DOOR PANEL 831GZ BROKEN IN CORNER. REPAIRED CREW DOOR PANEL 831GZ IAW A300 AMM 25-00-00/801 USED 1/4 OF TUBE ADHESIVE P/N: 04-001-0176 BTCH: 4433029. REVIEWEDOct 9, 2025 · N129UP · Airbus A300F4622R · Passenger/Crew Doors
Back to N129UP